US3910269A - Integrated helmet and mask structure - Google Patents

Integrated helmet and mask structure Download PDF

Info

Publication number
US3910269A
US3910269A US449777A US44977774A US3910269A US 3910269 A US3910269 A US 3910269A US 449777 A US449777 A US 449777A US 44977774 A US44977774 A US 44977774A US 3910269 A US3910269 A US 3910269A
Authority
US
United States
Prior art keywords
mask
face
helmet
sealing tube
shell
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US449777A
Inventor
William K Ansite
Jr John J Mitchell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Scott Technologies Inc
Original Assignee
CAPTECH Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US00255838A external-priority patent/US3833935A/en
Application filed by CAPTECH Inc filed Critical CAPTECH Inc
Priority to US449777A priority Critical patent/US3910269A/en
Application granted granted Critical
Publication of US3910269A publication Critical patent/US3910269A/en
Assigned to TEXACE CORPORATION A CORP. OF TEX. reassignment TEXACE CORPORATION A CORP. OF TEX. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). 11-10-78 Assignors: CAPTECH INC.
Assigned to SCOTT AVIATION-SIERRA PRODUCTS, INC., reassignment SCOTT AVIATION-SIERRA PRODUCTS, INC., CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). 11-10-78 Assignors: TEXACE CORPORATION
Assigned to CAPTECH INC. reassignment CAPTECH INC. NUNC PRO TUNC ASSIGNMENT (SEE DOCUMENT FOR DETAILS). 7-31-69 Assignors: SIERRA ENGINEERING CO.
Assigned to TEXACE CORPORATION, A CORP. OF TX reassignment TEXACE CORPORATION, A CORP. OF TX MERGER (SEE DOCUMENT FOR DETAILS). TEXAS, EFFECTIVE SEPT. 20, 1978 Assignors: CAPTECH INC., A CORP. OF CA., TEXACE CORPORATION, A CORP. OF TX
Assigned to FIGGIE INTERNATIONAL INC., A CORP. OF OHIO reassignment FIGGIE INTERNATIONAL INC., A CORP. OF OHIO ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: SCOTT AVIATION-SIERRA PRODUCTS, INC.
Assigned to FIGGIE INTERNATIONAL INC. reassignment FIGGIE INTERNATIONAL INC. MERGER (SEE DOCUMENT FOR DETAILS). EFFECTIVE DATE: DECEMBER 31, 1986 Assignors: FIGGIE INTERNATIONAL INC., (MERGED INTO) FIGGIE INTERNATIONAL HOLDINGS INC. (CHANGED TO)
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • AHUMAN NECESSITIES
    • A42HEADWEAR
    • A42BHATS; HEAD COVERINGS
    • A42B3/00Helmets; Helmet covers ; Other protective head coverings
    • A42B3/04Parts, details or accessories of helmets
    • A42B3/28Ventilating arrangements
    • A42B3/288Ventilating arrangements with means for attaching respirators or breathing masks
    • AHUMAN NECESSITIES
    • A42HEADWEAR
    • A42BHATS; HEAD COVERINGS
    • A42B3/00Helmets; Helmet covers ; Other protective head coverings
    • A42B3/04Parts, details or accessories of helmets
    • A42B3/18Face protection devices
    • A42B3/22Visors
    • A42B3/228Visors for military or aviation applications
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D10/00Flight suits

Definitions

  • ABSTRACT For flying personnel there is provided a hard shell helmet suitably padded and held out of close contact with the head.
  • An integrated visor assembly has an articulated attachment to the helmet movable between an operative position over the wearers face and a lifted position extending over the top of the helmet removed from the face.
  • Compound leverage elements making up the attachment determine a path of movement for the visor assembly such that it travels an irregular path allowing it to first lift clear of contact with the face and then travel upwardly to its lifted position.
  • An inflatable seal extends around the perimeter of the visor assembly, the seal being inflated with air from the oxygen supply for the breathing mask when in operation over the face of the wearer and being collapsed when deflated providing additional clearance for ease of removal from the face and for storage in its lifted position.
  • Personal flight equipment can be said to comprise chiefly of a flight protection helmet equipped with oxygen mask, head-set or ear phones and a smokeprotective visor.
  • Another object of the invention is to provide a new and improved helmet and mask integrated structure which is low in profile despite the need for a leverage or related mechanism to permit the mask assembly to be removed from the face.
  • Still another object of the invention is to provide a new and improved helmet and mask integrated structure provided with an inflatable seal between the mask assembly and the face of the wearer which can, when desired, be inflated automatically by oxygen pressure normally supplied to the mask and which provides for sufficient mask clearance of the face during donning.
  • Still further among the objects of the invention is to provide a mask assembly including an inflatable seal which is of such design and construction that it can be readily fitted to faces of different shape and size without need for changing the shape and size of the mask assembly and associated helmet shell.
  • the invention consists in the construction, arrangement, and combination of the various parts of the device, whereby the objects contemplated are attained, hereinafter set forth, pointed out in the appended claims and illustrated in the accompanying drawings.
  • FIG. 1 is a side elevational view of one form of the helmet and mask integrated structure shown in operating position on the head of a wearer. 7
  • FIG. 2 is a longitudinal sectional view of the structure of FIG. I.
  • FIG. 3 is a fragmentary cross sectional view taken on the circular line 3 of FIG. 2 with the seal inflated.
  • FIG. 4 is a fragmentary sectional view similar to FIG. 3 but with the seal deflated.
  • FIG. 5 is a side elevational view similar to FIG. I but with the visor assembly lifted into inoperative position.
  • FIG. 6 is a fragmentary cross sectional view on the line 6-6 of FIG. 1.
  • FIG. 7 is a fragmentary longitudinal sectional view on the line 77 of FIG. 5.
  • FIG. 8 is a side elevational view of a second form of the invention shown in position on the head of a wearer.
  • FIG. 9 is a side elevational view of the same form of the device as in FIG. 8 but with the visor assembly lifted into inoperative position.
  • FIG. 10 is a side elevational view of another form of the device shown in operative position.
  • FIG. 11 is a side elevational view of the device of FIG. 10 but with the visor assembly lifted into inoperative position.
  • FIG. 12 is a front perspective view of a modified form of the invention as shown in operative position on the head of a wearer.
  • FIG. 13 is a front perspective view similar to FIG. 12 but with the visor assembly lifted into inoperative position.
  • a hard helmet shell 10 equipped with a visor assembly indicated generally by the reference character 11 shown mounted on the head 12 of a wearer with the visor assembly in operative position applied to the wearers face 13.
  • a visor cover 14 is fixed in position at the crown of the helmet shell and provides a pocket 15. Extending through the helmet shell is a series of .ventillating perforations l6, and perforations 17 in the visor cover assist the perforations 16 which open into the pocket 15. Perforations serve two functions; to provide for ventilation; to reduce weight, yet still provide protection.
  • a shock or energy absorbing liner 18 extends around the entire inner surface of the helmet shell, the liner being of some appropriate foam cushion.
  • a sling 20 For supporting the helmet shell and perforce the he]- met and mask integrated structure on the crown of the head 12, there is provided a sling 20 extending fore and aft and to which are applied a forehead cross-web 21, a crown cross web 22, a rear cross-web 23 and a nape cross-web 24 attached to the sling at the junctions shown.
  • the sling and cross-webs are provided with elastomer pads 25, 26, 27 and 28 of appreciable depth sufficient to support the helmet shell in a position removed from contact with the head of the wearer providing a space from which heat, from the wearers head can pass outwardly through the perforations 16.
  • a chin strap 29 serves to hold the sling and cross-webs in position, the chin strap and the cross-webs being all attached to a lateral webbing 30 surrounding the wearers ears.
  • the lining of the helmet shell normally is spaced clear of the head of the wearer and that this spacing may vary to some extent depending upon the shape of the wearers head and the height of the elastomer pads.
  • the pads moreover, are yieldable and the sling and cross-webs are likewise yieldable so that should there be an impact on the helmet shell sufficient to compress the pads at one location or another, the wearers head will strike the liner.
  • the liner is of a character capable of absorbing the impact and the energy is dissipated, thereby protecting the head of the wearer.
  • the attachment of the ear cups to the helmet is flexible to allow lateral spreading to clear the ears for rapid donning. These flexible attachments facilitate folding ear cups into the inside of helmet shell for minimum storage volume.
  • the visor assembly 11 in this embodiment consists of two parts, namely, an eye area shell section 31 at a location surrounding the eyes of the wearer and an oralnasal area shell section 32 which is the portion usually identified as a breathing mask and upon which is mounted a regulator 33 capable of accommodating appropriate valving (not shown) for an air or oxygen line 34 and a microphone (not shown) supplied by a microphone line 35.
  • a seal indicated generally by the reference character 40 which in the chosen embodiment is a hollow tube, as indicated in FIGS. 3 and 4.
  • the tube extends around the lower and side edges of the oral-nasal area shell section 32, the side edges of the eye area shell section 31 and across the upper or forehead portion of the eye area shell section 31 at a location slightly removed from an upper edge 41.
  • the seal is continuous and endless.
  • there is a transverse section 42 of the seal which extends across the eye area shell section near the line 43 of junction between the eye area shell section and the oral-nasal area shell section.
  • thetransverse section 42 is actually attached to a web 44 which lies inside of the eye area shell section 31.
  • the transverse section moreover, is in communication with the seal 40 at the point ofjunction.
  • an air line 45 shown in FIG. 1, which extends from an air switch 46 supplied in turn from the mask regulator 33.
  • an air valve 47 on which is an actuator button 48 which normally tends to move to a shutoff position. As shown in FIG. 1, the actuator button is moved to an on position by engagement therewith of a portion of a composite arm 50.
  • a microphone switching arrangement also might be incorporated to switch off an external microphone (boom microphone) and switch on the microphone inside the mask.
  • the composite arm consists of a plunger 51, an outer end of which is attached to a bracket 52 which, in turn, has a pivotal attachment 53 to the side of the oral-nasal area shell section 32.
  • a telescoping sleeve 54 forms a connection between the plunger 51 and a hollow cylinder 55.
  • the cylinder is in turn attached by means of a screw 56 to a bracket 57, the bracket being part of an arm 58 which has a pivotal attachment 59 to the helmet shell 10.
  • a spring 60 has one end 61 secured by a spring keeper 62 to the plunger 51 and has its other end 63 secured to a keeper 64 which is anchored to the bracket 57.
  • the spring under tension is biased to draw the visor assembly in a direction from left to right as viewed in FIG. 1 so that the seal 40 is drawn into engagement with the face 13 of the wearer.
  • a slot 65 in the visor cover 14 within which travels the shank 66 of a knob 67, the shank 66 being riveted at 68 to an adjacent edge 69 of the eye area shell section 31.
  • the visor assembly and helmet shell are an integrated structure in that, except for the upward and downward motion about the pivot joints, the visor assembly is firmly held in a fixed relationship with respect to the helmet shell.
  • the mask regulator protruding as it does, can be made use of in a sense as a handle when the visor assembly is lifted upwardly or counter clockwise as viewed in FIG. 5.
  • the arm 58 is moved from its position of engagement with the actuator button 48 and the air valve 47 then closes off the air line 34 so that no air flows either to the mask regulator 33 or to the seal 40 through the air line 45.
  • a sealing face 70 has a seal 40, which is the portion of the seal which actually engages the skin on the face 13 and draws away from the skin an appreciable distance, namely, about half the inflated height of the seal as shown in FIGS. 3 and 4.
  • This providesjade quate clearance so that when the mask assembly is lifted progressively from the position of FIG. 1 to the position of FIG. 5, there will be no resistance to its lifting.
  • the composite arm 50 then in an over-center position functions to pull the visor assembly toward the visor cover 14 until the eye area shell section is drawn into the pocket 15.
  • the mask regulator 33 and visor assembly is swung downwardly or counter-clockwise as viewed in FIG. 5, initially extending the spring 60 as it swings, until the positions of FIG. 1 are then accomplished.
  • the arm 58 engages the actuator button 48 thereby to admit automatically air from the air or oxygen line 34 to the mask regulator 33 and thence into the mask.
  • air under pressure passes through the air switch 46 and air line 45 into the seal 40 causing it to be inflated to the position of FIG. 3.
  • the sealing face 70 will be drawn gently into engagement with the face of the wearer thereby sealing all of that portion of the visor assembly which is defined by the perimeter of the seal as shown in FIGS. 1, 2 and 5.
  • FIGS. 8 and 9 there is substituted for the composite arm 50 a compound lever assembly consisting of a lever arm and lever arm 76.
  • the lever arm 75 has a bent end section 77 extending at right angle to the lever arm, the end section 77 having a pivot connection 78 to the edge of the oral-nasal area shell section 32.
  • the lever arm 76 has a pivot connection 79 to an ear receptacle 80 which is'an integral part of the helmet shell 10.
  • An extension 81 of the lever arm 76 protrudes below the ear receptacle and there is a pivot connection 82 between the lever arm 75 and the lever arm 76 at a location not far removed from the pivot connection 79.
  • An actuator button 83 on an air valve 84 serves to automatically open the air valve when the extension 81 is in the position shown in FIG. 8 thereby to inflate the seal 40 while the visor assembly is in a position against the face 13 of the wearer.
  • an air line 85 extends from the air valve 84 to a side portion ofthe seal 40 as shown in FIG. 8.
  • the extension 81 can be employed to help tighten the seal by pushing rearwardly against the extension.
  • a locking button 86 of substantially conventional construction, can be turned to tighten engagement of a corner tab 87 of the eye area shell section 31 to the visor cover 14 which is immediately adjacent the end of the slot 65.
  • the locking button 86 When the visor assembly is to be lifted clear of the face the locking button 86 is loosened. The visor assembly can then be lifted to the position of FIG. 9. Meanwhile the locking button and its attached shank 88 move to the opposite end of the slot 65 and there again can be tightened so as to be capable of holding the visor assembly in-the elevated position until it is to be released.
  • the visor cover 14' is cut away at 90 and the slot 65 dispensed with.
  • a lever system of three lever arms is made use of for holding and guiding the visor assembly relative to the helmet shell.
  • the lever system consists of a lever arm 91 having a bent section 92 at one end which by means of a pivot connection 93 is attached to a corner 94 of a transparent visor 95.
  • a lever arm 96 has a pivot conection 97 to an ear receptacle 98 which is an integral part of the helmet shell 10.
  • a pivot connection 99 interconnects the lever arm 91 with the lever arm 96.
  • Another lever arm 100 has a pivot connection 101 at one end to the visor 95 about midway between the top and the bottom. At the other end of the lever arm is a pivot connection 102 which connects the lever arm 100 to the lever arm 96 at a location farther away from the pivot connection 97 than the pivot connection 99 previously described. An extension 103 of the lever arm 96 protrudes to a position below the ear receptacle 98.
  • An actuator button 104 on an air valve 105 serves a function similar to the previously described actuator button 83 in that in the lowered or operative position of FIG. 10, the actuator button 104 is tripped by the lever arm 100 and causes the air valve to open thereby to inflate a seal 40.
  • the lever arm 100 is moved free of the actuator button 104 causing it to shut off the supply of air whereupon to collapse the seal 40'.
  • the visor is substantially a single piece transparent visorwhich covers the surface of the wearers face 13 both above and around the eyes and around and below the nose and mouth.
  • a single perimetrical seal 40' extending around the edge of the visor 95 forms a seal between the visor and the face of the wearer.
  • An air line 106 communicates between the air valve and the seal 40' so that air from an air or oxygen line 34' can be made to supply both air pressure for the seal 40 and air to the mask regulator 33 which communicates with the area beneath the visor 95 in a substantially conventional manner.
  • FIGS. 12 and 13 A somewhat different form of helmet and mask integrated structure is shown in FIGS. 12 and 13.
  • a visor cover 110 mounted on a helmet shell 111 is provided with a pair of forwardly extending extensions 112 in each of which is a track 113.
  • a shoe 114 on either side of an eye area shell section 115 is curved to match the curvature of the track 113 and is adapted to slide with respect to the track as the eye area shell section is moved upwardly from the position in FIG. 12 to the position of FIG. 13.
  • a mask section 116 adapted to extend around the nose and mouth of the wearer is integrally attached to the eye area shell section along the line 117.
  • the mask regulator is in turn supplied by anjair line 120.
  • a pair of lift arms 121 one on each side, one only being shown in FIGS. 12 and 13.
  • the lift arm 121 is pivoted beneath a pivot connection 122, the pivot connection being mounted upon and anchored to an ear receptacle 123.
  • the ear receptacle 123 is made to act substantially integrally with the helmet shell 110 by employment of a rear strap 124 and an upper strap 125.
  • the straps may be either a synthetic plastic resin material or a spring metal material which by flexing in the direction of the flat areas permits the ear receptacles to be easily moved upwardly away from the head and ears of the wearer when the helmet is to be donned and which, upon release, will cause the ear receptacles to be sprung inwardly into contact with the area around the ears of the wearer by virtue of the return acting spring effect of the straps 124 and 125.
  • a chin strap 126 helps hold the assembly in place.
  • the helmet shell and the visor and mask combination have only very limited movement in any other direction thereby making them a substantially integrated structure, which fits under the visor cover 110 when elevated to the position of FIG. 13, and which snugly seals around the face of the wearer in the position of FIG. 12.
  • An integrated helmet and mask structure for the head and face of a wearer comprising a hard helmet shell, a visor assembly including a mask shell and having an articulated attachment on each side to the helmet shell and valve means on the mask shell including a supply of breathing gas for directing such gas to the mask structure, said mask shell having an inner surface adapted to face the face of the wearer, means for moving the mask shell toward and away from a position adjacent the face of a wearer, a hollow sealing tube extending around the edge of the mask shell on the side thereof facing the face, said sealing tube having a fixed sealed attachment to said mask shell, a hose in communication between the valve means and the sealing tube for introducing breathing gas from the supply for the valve means into said tube, said tube having a normally collapsed condition in a direction perpendicular with respect to the inner surface of the mask shell at all locations of attachment, said sealing tube being withdrawn from the adjacent face of the wearer when not subject to gas under pressure and an inflated condition when subject to gas under pressure, the tube when in inflated condition under
  • valve means is mounted on the helmet shell and includes a mask supply line and a seal supply line, and a valve actuator in operative relationship with theseal supply line.
  • valve actuator has an open condition when out of engagement with a portion of said articulated attachment wherein there is an open connection for gas under mask pressure to said sealing tube, said valve actuator having a closed condition when said articulated attachment is at a position of engagement with said valve actuator wherein there is a closed connection shutting off gas under mask pressure to the sealing tube whereby the tube is deflated.
  • sealing tube is an endless tube extending around the perimeter of said mask shell.
  • An integrated helmet and mask structure as in claim 4 wherein there is a transverse section of sealing tube extending across the interior of said mask shell at a location intermediate an eye surrounding area and an oral-nasal surrounding area, and wherein said trans verse section is connected to the sealing tube and subject to respectively inflated and collapsed conditions when the remainder of the sealing tube is subject to respectively inflated and collapsed conditions.
  • sealing tube has a long dimension substantially perpendicular to said inner surface and a substantially short dimension at right angles thereto, said sealing tube having a normally collapsed condition in the direction of said long dimension to which it returns when not subject to internal air pressure.

Abstract

For flying personnel there is provided a hard shell helmet suitably padded and held out of close contact with the head. An integrated visor assembly has an articulated attachment to the helmet movable between an operative position over the wearer''s face and a lifted position extending over the top of the helmet removed from the face. Compound leverage elements making up the attachment determine a path of movement for the visor assembly such that it travels an irregular path allowing it to first lift clear of contact with the face and then travel upwardly to its lifted position. An inflatable seal extends around the perimeter of the visor assembly, the seal being inflated with air from the oxygen supply for the breathing mask when in operation over the face of the wearer and being collapsed when deflated providing additional clearance for ease of removal from the face and for storage in its lifted position.

Description

United States Patent 191 Ansite et al.
[ Oct. 7, 1975 INTEGRATED HELMET AND MASK STRUCTURE [73] Assignee: Sierra Engineering Co., Sierra Madre, Calif.
22 Filed: Mar. 11, 1974 [211 Appl. No.: 449,777
Related US. Application Data [62] Division of Ser. No. 255,838, May 22, 1972, Pat. No.
[52] US. Cl 128/142; 128/142.7 [51] Int. Cl. A6213 7/00 [58] Field of Search..... 128/141, 142, 146.7, 142.3, 128/142.7, 142.2, 142.5; 2/6
FOREIGN PATENTS OR APPLICATIONS France United Kingdom Primary Examiner-Richard A. Gaudet Assistant Examiner-Lee S. Cohen [5 7] ABSTRACT For flying personnel there is provided a hard shell helmet suitably padded and held out of close contact with the head. An integrated visor assembly has an articulated attachment to the helmet movable between an operative position over the wearers face and a lifted position extending over the top of the helmet removed from the face. Compound leverage elements making up the attachment determine a path of movement for the visor assembly such that it travels an irregular path allowing it to first lift clear of contact with the face and then travel upwardly to its lifted position. An inflatable seal extends around the perimeter of the visor assembly, the seal being inflated with air from the oxygen supply for the breathing mask when in operation over the face of the wearer and being collapsed when deflated providing additional clearance for ease of removal from the face and for storage in its lifted position.
7 Claims, 13 Drawing Figures US. Patent Oct. 7,1975 shw 1 of5 3,910,269
w a m a y M /II 5 7 r w t r m w 0 US. Patent US. Patent 0a. 7,1975 Sheet 3 of5 3,910,269
Oct. 7,1975 Sheet 4 of 5 3,910,269
US, Pamnt U.S. Patesnt Oct. 7,1975 Sheet 5 of5 3 910369 mi w INTEGRATED HELMET AND MASK STRUCTURE This is adivision of application Ser. No. 255,838, filed'May 22, 1972.
As aircraft capabilities continuously involve in creased speeds, demands upon the men who fly them experience a change which, in part, adds greatly to the mentaland physical stresses experienced. Physical discomforts are variable in nature and additive. Movement within the cockpit is confined and restricted. Added to this is the weight and restrictiveness of equipment worn by the pilot and crew and the heat generated within his personal flight safety equipment which, over long periods of flight duty, create extensive discomfort. Personal flight equipment can be said to comprise chiefly ofa flight protection helmet equipped with oxygen mask, head-set or ear phones and a smokeprotective visor.
Respecting currently available personal equipment, a complaint and consequently a defect in addition to being too hot, too heavy, excessively cumbersome and too restrictive, is that the equipment has too many nonintegrated components. Whatever remedy may be offered, however, the protection must still include protection against head injury as a result of buffeting or turbulence upon ejection, cabin or cockpit decompression, eitherexplosive or otherwise, and eye protection from the smoke of cabin or cockpit tires as well from spalling.
It is therefore among the objects of the invention to provide a new and improved helmet and mask integrated structure wherein the mask and communication equipment are so connected to the helmet itself to present a more integrated combination which, at the same time, is cool and comfortable when worn.
Another object of the invention is to provide a new and improved helmet and mask integrated structure which is low in profile despite the need for a leverage or related mechanism to permit the mask assembly to be removed from the face.
Still another object of the invention is to provide a new and improved helmet and mask integrated structure provided with an inflatable seal between the mask assembly and the face of the wearer which can, when desired, be inflated automatically by oxygen pressure normally supplied to the mask and which provides for sufficient mask clearance of the face during donning.
Still further among the objects of the invention is to provide a mask assembly including an inflatable seal which is of such design and construction that it can be readily fitted to faces of different shape and size without need for changing the shape and size of the mask assembly and associated helmet shell.
With these and other objects in view, the invention consists in the construction, arrangement, and combination of the various parts of the device, whereby the objects contemplated are attained, hereinafter set forth, pointed out in the appended claims and illustrated in the accompanying drawings.
In the drawings:
FIG. 1 is a side elevational view of one form of the helmet and mask integrated structure shown in operating position on the head of a wearer. 7
FIG. 2 is a longitudinal sectional view of the structure of FIG. I.
FIG. 3 is a fragmentary cross sectional view taken on the circular line 3 of FIG. 2 with the seal inflated.
FIG. 4 is a fragmentary sectional view similar to FIG. 3 but with the seal deflated.
FIG. 5 is a side elevational view similar to FIG. I but with the visor assembly lifted into inoperative position.
FIG. 6 is a fragmentary cross sectional view on the line 6-6 of FIG. 1.
FIG. 7 is a fragmentary longitudinal sectional view on the line 77 of FIG. 5.
FIG. 8 is a side elevational view of a second form of the invention shown in position on the head of a wearer.
FIG. 9 is a side elevational view of the same form of the device as in FIG. 8 but with the visor assembly lifted into inoperative position.
FIG. 10 is a side elevational view of another form of the device shown in operative position.
FIG. 11 is a side elevational view of the device of FIG. 10 but with the visor assembly lifted into inoperative position.
FIG. 12 is a front perspective view of a modified form of the invention as shown in operative position on the head of a wearer.
FIG. 13 is a front perspective view similar to FIG. 12 but with the visor assembly lifted into inoperative position.
In an embodimentpf the invention chosen for the purpose of illustration, there is shown a hard helmet shell 10 equipped with a visor assembly indicated generally by the reference character 11 shown mounted on the head 12 of a wearer with the visor assembly in operative position applied to the wearers face 13. A visor cover 14 is fixed in position at the crown of the helmet shell and provides a pocket 15. Extending through the helmet shell is a series of .ventillating perforations l6, and perforations 17 in the visor cover assist the perforations 16 which open into the pocket 15. Perforations serve two functions; to provide for ventilation; to reduce weight, yet still provide protection. A shock or energy absorbing liner 18 extends around the entire inner surface of the helmet shell, the liner being of some appropriate foam cushion.
For supporting the helmet shell and perforce the he]- met and mask integrated structure on the crown of the head 12, there is provideda sling 20 extending fore and aft and to which are applied a forehead cross-web 21, a crown cross web 22, a rear cross-web 23 and a nape cross-web 24 attached to the sling at the junctions shown. The sling and cross-webs are provided with elastomer pads 25, 26, 27 and 28 of appreciable depth sufficient to support the helmet shell in a position removed from contact with the head of the wearer providing a space from which heat, from the wearers head can pass outwardly through the perforations 16. A chin strap 29 serves to hold the sling and cross-webs in position, the chin strap and the cross-webs being all attached to a lateral webbing 30 surrounding the wearers ears.
It will be understood that the lining of the helmet shell normally is spaced clear of the head of the wearer and that this spacing may vary to some extent depending upon the shape of the wearers head and the height of the elastomer pads. The pads, moreover, are yieldable and the sling and cross-webs are likewise yieldable so that should there be an impact on the helmet shell sufficient to compress the pads at one location or another, the wearers head will strike the liner. The liner is of a character capable of absorbing the impact and the energy is dissipated, thereby protecting the head of the wearer.
It should be noted that the attachment of the ear cups to the helmet is flexible to allow lateral spreading to clear the ears for rapid donning. These flexible attachments facilitate folding ear cups into the inside of helmet shell for minimum storage volume.
The visor assembly 11 in this embodiment consists of two parts, namely, an eye area shell section 31 at a location surrounding the eyes of the wearer and an oralnasal area shell section 32 which is the portion usually identified as a breathing mask and upon which is mounted a regulator 33 capable of accommodating appropriate valving (not shown) for an air or oxygen line 34 and a microphone (not shown) supplied by a microphone line 35.
In this embodiment there is also provided a compensated exhalation valve 36 and a relief valve 37 of substantially conventional construction.
For sealing the perimeter of the visor assembly to the face 13 of the wearer, use is made of a seal indicated generally by the reference character 40 which in the chosen embodiment is a hollow tube, as indicated in FIGS. 3 and 4. As shown in FIGS. 1 and 2, the tube extends around the lower and side edges of the oral-nasal area shell section 32, the side edges of the eye area shell section 31 and across the upper or forehead portion of the eye area shell section 31 at a location slightly removed from an upper edge 41. To the extent described, the seal is continuous and endless. In addition, there is a transverse section 42 of the seal which extends across the eye area shell section near the line 43 of junction between the eye area shell section and the oral-nasal area shell section. As shown in FIG. 2, thetransverse section 42 is actually attached to a web 44 which lies inside of the eye area shell section 31. The transverse section, moreover, is in communication with the seal 40 at the point ofjunction.
For inflating the seal, use is made of an air line 45, shown in FIG. 1, which extends from an air switch 46 supplied in turn from the mask regulator 33.
In the air or oxygen line 34 is interposed an air valve 47 on which is an actuator button 48 which normally tends to move to a shutoff position. As shown in FIG. 1, the actuator button is moved to an on position by engagement therewith of a portion of a composite arm 50. A microphone switching arrangement also might be incorporated to switch off an external microphone (boom microphone) and switch on the microphone inside the mask.
As shown in FIG. 7 in company with FIG. 1, the composite arm consists of a plunger 51, an outer end of which is attached to a bracket 52 which, in turn, has a pivotal attachment 53 to the side of the oral-nasal area shell section 32.
A telescoping sleeve 54 forms a connection between the plunger 51 and a hollow cylinder 55. The cylinder is in turn attached by means of a screw 56 to a bracket 57, the bracket being part of an arm 58 which has a pivotal attachment 59 to the helmet shell 10.
As shown in FIG. 7, a spring 60 has one end 61 secured by a spring keeper 62 to the plunger 51 and has its other end 63 secured to a keeper 64 which is anchored to the bracket 57. The spring under tension is biased to draw the visor assembly in a direction from left to right as viewed in FIG. 1 so that the seal 40 is drawn into engagement with the face 13 of the wearer.
To assist in shifting the visor assembly 11 from the operative position shown in FIG. 1 to the withdrawn position of FIG. 5, use is made of a slot 65 in the visor cover 14 within which travels the shank 66 of a knob 67, the shank 66 being riveted at 68 to an adjacent edge 69 of the eye area shell section 31.
Although only one side of the visor assembly is shown in FIG. 1, it will be understood that the other side is identical except for being a right-hand side counterpart of the composite arm 50 and the slot 65 containing the shank 66. Connected as described, the visor assembly and helmet shell are an integrated structure in that, except for the upward and downward motion about the pivot joints, the visor assembly is firmly held in a fixed relationship with respect to the helmet shell.
When the visor assembly is to be moved from the operative position of FIG. 1 to the elevated position of FIG. 5, the mask regulator, protruding as it does, can be made use of in a sense as a handle when the visor assembly is lifted upwardly or counter clockwise as viewed in FIG. 5.
When this occurs, the arm 58 is moved from its position of engagement with the actuator button 48 and the air valve 47 then closes off the air line 34 so that no air flows either to the mask regulator 33 or to the seal 40 through the air line 45.
When this circumstance prevails, the seal 40 will collapse to the position shown in FIG. 4 by reason of the fact that the seal initially is given the collapsed form of FIG. 4 when molded. Collapsing as described, a sealing face 70 has a seal 40, which is the portion of the seal which actually engages the skin on the face 13 and draws away from the skin an appreciable distance, namely, about half the inflated height of the seal as shown in FIGS. 3 and 4. This providesjade quate clearance so that when the mask assembly is lifted progressively from the position of FIG. 1 to the position of FIG. 5, there will be no resistance to its lifting. Additionally, when the mask assembly is elevated, the composite arm 50 then in an over-center position functions to pull the visor assembly toward the visor cover 14 until the eye area shell section is drawn into the pocket 15.
Conversely when the mask assembly is to be lowered into operating position, the mask regulator 33 and visor assembly is swung downwardly or counter-clockwise as viewed in FIG. 5, initially extending the spring 60 as it swings, until the positions of FIG. 1 are then accomplished. At this point the arm 58 engages the actuator button 48 thereby to admit automatically air from the air or oxygen line 34 to the mask regulator 33 and thence into the mask. At the same time, air under pressure passes through the air switch 46 and air line 45 into the seal 40 causing it to be inflated to the position of FIG. 3. In this position the sealing face 70 will be drawn gently into engagement with the face of the wearer thereby sealing all of that portion of the visor assembly which is defined by the perimeter of the seal as shown in FIGS. 1, 2 and 5.
In the form of invention of FIGS. 8 and 9, there is substituted for the composite arm 50 a compound lever assembly consisting of a lever arm and lever arm 76. The lever arm 75 has a bent end section 77 extending at right angle to the lever arm, the end section 77 having a pivot connection 78 to the edge of the oral-nasal area shell section 32.
The lever arm 76 has a pivot connection 79 to an ear receptacle 80 which is'an integral part of the helmet shell 10. An extension 81 of the lever arm 76 protrudes below the ear receptacle and there is a pivot connection 82 between the lever arm 75 and the lever arm 76 at a location not far removed from the pivot connection 79. An actuator button 83 on an air valve 84 serves to automatically open the air valve when the extension 81 is in the position shown in FIG. 8 thereby to inflate the seal 40 while the visor assembly is in a position against the face 13 of the wearer.
Conversely when the visor assembly is lifted to the position of FIG. 9, the extension 81 moves out of engagement with the actuator button 83 thereby permitting the air valve to close and cut off the air supply whereupon the seal 40 collapses in the manner previously described. in this form of invention, an air line 85 extends from the air valve 84 to a side portion ofthe seal 40 as shown in FIG. 8.
When the visor assembly is in the operating position of FIG. 8 and the wearer wishes to press it more snugly against his face, the extension 81 can be employed to help tighten the seal by pushing rearwardly against the extension. When it has been pushed far enough, a locking button 86, of substantially conventional construction, can be turned to tighten engagement of a corner tab 87 of the eye area shell section 31 to the visor cover 14 which is immediately adjacent the end of the slot 65.
When the visor assembly is to be lifted clear of the face the locking button 86 is loosened. The visor assembly can then be lifted to the position of FIG. 9. Meanwhile the locking button and its attached shank 88 move to the opposite end of the slot 65 and there again can be tightened so as to be capable of holding the visor assembly in-the elevated position until it is to be released.
Additionally, this engagement of the extension 81 from the actuator button 83 causes the air valve 84 to shut off the supply of air and the seal 40 thereupon will collapse.
In the form of invention of FIGS. and 11, the visor cover 14' is cut away at 90 and the slot 65 dispensed with. A lever system of three lever arms is made use of for holding and guiding the visor assembly relative to the helmet shell. The lever system consists of a lever arm 91 having a bent section 92 at one end which by means of a pivot connection 93 is attached to a corner 94 of a transparent visor 95. A lever arm 96 has a pivot conection 97 to an ear receptacle 98 which is an integral part of the helmet shell 10. A pivot connection 99 interconnects the lever arm 91 with the lever arm 96.
Another lever arm 100 has a pivot connection 101 at one end to the visor 95 about midway between the top and the bottom. At the other end of the lever arm is a pivot connection 102 which connects the lever arm 100 to the lever arm 96 at a location farther away from the pivot connection 97 than the pivot connection 99 previously described. An extension 103 of the lever arm 96 protrudes to a position below the ear receptacle 98.
An actuator button 104 on an air valve 105 serves a function similar to the previously described actuator button 83 in that in the lowered or operative position of FIG. 10, the actuator button 104 is tripped by the lever arm 100 and causes the air valve to open thereby to inflate a seal 40. When the visor assembly is lifted to the position of FIG. 11, the lever arm 100 is moved free of the actuator button 104 causing it to shut off the supply of air whereupon to collapse the seal 40'.
In this form of the invention the visor is substantially a single piece transparent visorwhich covers the surface of the wearers face 13 both above and around the eyes and around and below the nose and mouth. In this way a single perimetrical seal 40' extending around the edge of the visor 95 forms a seal between the visor and the face of the wearer. An air line 106 communicates between the air valve and the seal 40' so that air from an air or oxygen line 34' can be made to supply both air pressure for the seal 40 and air to the mask regulator 33 which communicates with the area beneath the visor 95 in a substantially conventional manner.
A somewhat different form of helmet and mask integrated structure is shown in FIGS. 12 and 13. There a visor cover 110 mounted on a helmet shell 111 is provided with a pair of forwardly extending extensions 112 in each of which is a track 113. A shoe 114 on either side of an eye area shell section 115 is curved to match the curvature of the track 113 and is adapted to slide with respect to the track as the eye area shell section is moved upwardly from the position in FIG. 12 to the position of FIG. 13. A mask section 116 adapted to extend around the nose and mouth of the wearer is integrally attached to the eye area shell section along the line 117.
A seal 40 of the same general character as the seals 40 and 40 heretofore described, extends around the perimeter of the eye area shell section 115 and the mask section 116, the seal being supplied with air through an air line 118 fed from a m'ask'regulator 119. The mask regulator is in turn supplied by anjair line 120. i
To additionally hold and guide the'ieye area shel l'section and hence what constitutes a mask assembly,'there is provided a pair of lift arms 121, one on each side, one only being shown in FIGS. 12 and 13. The lift arm 121 is pivoted beneath a pivot connection 122, the pivot connection being mounted upon and anchored to an ear receptacle 123.
The ear receptacle 123 is made to act substantially integrally with the helmet shell 110 by employment of a rear strap 124 and an upper strap 125. The straps may be either a synthetic plastic resin material or a spring metal material which by flexing in the direction of the flat areas permits the ear receptacles to be easily moved upwardly away from the head and ears of the wearer when the helmet is to be donned and which, upon release, will cause the ear receptacles to be sprung inwardly into contact with the area around the ears of the wearer by virtue of the return acting spring effect of the straps 124 and 125. A chin strap 126 helps hold the assembly in place.
Here, again, except for the movement up and down of the visor and mask combination relative to the helmet shell, the helmet shell and the visor and mask combination have only very limited movement in any other direction thereby making them a substantially integrated structure, which fits under the visor cover 110 when elevated to the position of FIG. 13, and which snugly seals around the face of the wearer in the position of FIG. 12.
While the invention has herein been shown and described in what is conceived to be a practical and effective embodiment, it is recognized that departures may be made therefrom within the scope of the invention, which is not to be limited to the details disclosed herein but is to be accorded the full scope of the claims so as to embrace any and all equivalent devices.
Having described the invention, what is claimed as new in support of Letters Patent is:
1. An integrated helmet and mask structure for the head and face of a wearer, said structure comprising a hard helmet shell, a visor assembly including a mask shell and having an articulated attachment on each side to the helmet shell and valve means on the mask shell including a supply of breathing gas for directing such gas to the mask structure, said mask shell having an inner surface adapted to face the face of the wearer, means for moving the mask shell toward and away from a position adjacent the face of a wearer, a hollow sealing tube extending around the edge of the mask shell on the side thereof facing the face, said sealing tube having a fixed sealed attachment to said mask shell, a hose in communication between the valve means and the sealing tube for introducing breathing gas from the supply for the valve means into said tube, said tube having a normally collapsed condition in a direction perpendicular with respect to the inner surface of the mask shell at all locations of attachment, said sealing tube being withdrawn from the adjacent face of the wearer when not subject to gas under pressure and an inflated condition when subject to gas under pressure, the tube when in inflated condition under pressure of gas from said gas supply being adapted to have a sealing relationship with the face of the wearer.
2. An integrated helmet and mask structure as in claim 1 wherein said valve means is mounted on the helmet shell and includes a mask supply line and a seal supply line, and a valve actuator in operative relationship with theseal supply line.
3. An integrated helmet and mask structure as in claim 2 wherein said valve actuator has an open condition when out of engagement with a portion of said articulated attachment wherein there is an open connection for gas under mask pressure to said sealing tube, said valve actuator having a closed condition when said articulated attachment is at a position of engagement with said valve actuator wherein there is a closed connection shutting off gas under mask pressure to the sealing tube whereby the tube is deflated.
4. An integrated helmet and mask structure as in claim 1 wherein the sealing tube is an endless tube extending around the perimeter of said mask shell.
5. An integrated helmet and mask structure as in claim 4 wherein there is a transverse section of sealing tube extending across the interior of said mask shell at a location intermediate an eye surrounding area and an oral-nasal surrounding area, and wherein said trans verse section is connected to the sealing tube and subject to respectively inflated and collapsed conditions when the remainder of the sealing tube is subject to respectively inflated and collapsed conditions.
6. An integrated helmet and mask structure as in claim 5 wherein there is a flexible web between said transverse section of the sealing tube and said oralnasal surrounding area of the visor, said web compris ing a flexible attachment for the sealing tube to the visor.
7. An integrated helmet and mask structure in claim 1 wherein said sealing tube has a long dimension substantially perpendicular to said inner surface and a substantially short dimension at right angles thereto, said sealing tube having a normally collapsed condition in the direction of said long dimension to which it returns when not subject to internal air pressure.

Claims (7)

1. An integrated helmet and mask structure for the head and face of a wearer, said structure comprising a hard helmet shell, a visor assembly including a mask shell and having an articulated attachment on each side to the helmet shell and valve means on the mask shell including a supply of breathing gas for directing such gas to the mask structure, said mask shell having an inner surface adapted to face the face of the wearer, means for moving the mask shell toward and away from a position adjacent the face of a wearer, a hollow sealing tube extending around the edge of the mask shell on the side thereof facing the face, said sealing tube having a fixed sealed attachment to said mask shell, a hose in communication between the valve means and the sealing tube for introducing breathing gas from the supply for the valve means into said tube, said tube having a normally collapsed condition in a direction perpendicular with respect to the inner surface of the mask shell at all locations of attachment, said sealing tube being withdrawn from the adjacent face of the wearer when not subject to gas under pressure and an inflated condition when subject to gas under pressure, the tube when in inflated condition under pressure of gas from said gas supply being adapted to have a sealing relationship with the face of the wearer.
2. An integrated helmet and mask structure as in claim 1 wherein said valve means is mounted on the helmet shell and includes a mask supply line and a seal supply line, and a valve actuator in operative relationship with the seal supply line.
3. An integrated helmet and mask structure as in claim 2 wherein said valve actuator has an open condition when out of engagement with a portion of said articulated attachment wherein there is an open connection for gas under mask pressure to said sealing tube, said valve actuator having a closed condition when said articulated attachment is at a position of engagement with said valve actuator wherein there is a closed connection shutting off gas under mask pressure to the sealing tube whereby the tube is deflated.
4. An integrated helmet and mask structure as in claim 1 wherein the sealing tube is an endless tube extending around the perimeter of said mask shell.
5. An integrated helmet and mask structure as in claim 4 wherein there is a transverse section of sealing tube extending across the interior of said mask shell at a location intermediate an eye surrounding area and an oral-nasal surrounding area, and wherein said transverse section is connected to the sealing tube and subject to respectively inflated and collapsed conditions when the remainder of the sealing tube is subject to respectively inflated and collapsed conditions.
6. An integrated helmet and mask structure as in claim 5 wherein there is a flexible web between said transverse section of the sealing tube and said oral-nasal surrounding area of the visor, said web comprising a flexible attachment for the sealing tube to the visor.
7. An integrated helmet and mask structure as in claim 1 wherein said sealing tube has a long dimension substantially perpendicular to said inner surface and a substantially short dimension at right angles thereto, said sealing tube having a normally collapsed condition in the direction of said long dimension to which it returns when not subject to internal air pressure.
US449777A 1972-05-22 1974-03-11 Integrated helmet and mask structure Expired - Lifetime US3910269A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US449777A US3910269A (en) 1972-05-22 1974-03-11 Integrated helmet and mask structure

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US00255838A US3833935A (en) 1972-05-22 1972-05-22 Integrated helmet and mask structure
US449777A US3910269A (en) 1972-05-22 1974-03-11 Integrated helmet and mask structure

Publications (1)

Publication Number Publication Date
US3910269A true US3910269A (en) 1975-10-07

Family

ID=26944989

Family Applications (1)

Application Number Title Priority Date Filing Date
US449777A Expired - Lifetime US3910269A (en) 1972-05-22 1974-03-11 Integrated helmet and mask structure

Country Status (1)

Country Link
US (1) US3910269A (en)

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3971368A (en) * 1975-08-13 1976-07-27 Puritan Equipment, Inc. Combined oxygen mask and smoke goggle apparatus with automatic flush valve
US4116237A (en) * 1977-02-07 1978-09-26 Norman Birch Emergency breathing apparatus
US4136403A (en) * 1976-09-10 1979-01-30 Dragerwerk Aktiengesellschaft Head guard assembly comprising a protective helmet and a protective breathing mask
US4172455A (en) * 1976-12-28 1979-10-30 Intertechnique Breathing equipment for high altitude flights
US4174710A (en) * 1977-04-28 1979-11-20 Auergesellschaft Gmbh Connection between two different parts of a person's protective covering
US4227520A (en) * 1978-02-10 1980-10-14 Canadian Patents & Development Ltd. Safety helmet for miners
US4336799A (en) * 1980-09-03 1982-06-29 Banyaszati Aknamelyito Vallalat Apparatus for supplying oxygen to a user
US5078130A (en) * 1988-07-14 1992-01-07 Gentex Corporation Personnel headgear enabling free breathing of ambient air or selective breathing from various sources
US5291880A (en) * 1990-08-16 1994-03-08 Cairns & Brother Inc. Protective helmet with protective facepiece connection and adjustment provision
GB2271285A (en) * 1992-10-09 1994-04-13 Michael Beard Automatic tensioner for a face mask harness
US5355878A (en) * 1990-06-26 1994-10-18 Cam Lock (Uk) Ltd. Breathing equipment for aircrew
US5538001A (en) * 1992-06-12 1996-07-23 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Northern Ireland And Great Britain Oxygen masks
FR2732865A1 (en) * 1995-04-12 1996-10-18 Gentex Corp INTEGRATED HELMET SYSTEM
US5687713A (en) * 1991-11-29 1997-11-18 Bahr; Erik W. Breathing mask
US5758639A (en) * 1992-09-08 1998-06-02 Ikonen; Alpo Combination of a helmet and a respiratror and a method for using it
WO1999008556A1 (en) * 1997-08-15 1999-02-25 Honeywell Inc. Headgear having an articulated mounting mechanism for a visor
US20030047185A1 (en) * 2001-09-13 2003-03-13 Olsen Gregory James Breathing assistance apparatus
WO2003005765A3 (en) * 2001-07-02 2003-03-20 Be Intellectual Pty Inc Multi-phase headset for pilots
US20040035428A1 (en) * 2000-06-14 2004-02-26 Fisher & Paykel Healthcare Limited Breathing assistance apparatus
US20040244801A1 (en) * 2002-09-30 2004-12-09 Hannah Gary R. Full face flexible oxygen mask for use with flight helmets
US20050028820A1 (en) * 2001-11-05 2005-02-10 Smith Nicholas Charles Alan Nasal masks
US6997178B1 (en) * 1998-11-25 2006-02-14 Thomson-Csf Sextant Oxygen inhaler mask with sound pickup device
US20060060193A1 (en) * 2002-09-27 2006-03-23 Richardson Grant S Respirator
US20060277665A1 (en) * 2005-05-27 2006-12-14 Drager Safety Ag & Co. Kgaa Safety helmet with a breathing mask
US20070107727A1 (en) * 2005-11-14 2007-05-17 Brichetto David Mr Aviator emergency oxygen system
AU2007202982B2 (en) * 2001-07-02 2009-10-01 Be Intellectual Property, Inc. Multi-phase headset for pilots
US20100229288A1 (en) * 2009-03-16 2010-09-16 Danny Higgins Helmet having a guiding mechanism for a compatible visor
US7934497B1 (en) * 2001-11-19 2011-05-03 The United States Of America As Represented By The Secretary Of The Army Modular helmet-mask assembly
ITUB20153701A1 (en) * 2015-09-17 2017-03-17 Caberg Spa JET TYPE HELMET STRUCTURE WITH INCORPORATED VISOR
US20190008228A1 (en) * 2016-12-30 2019-01-10 David Francis Ramey Integrated non-conflicting headgear platform system and method
US20190350301A1 (en) * 2017-02-21 2019-11-21 Unit 1 Gear, Inc. Headphone and helmet assembly
US11507056B1 (en) * 2020-04-06 2022-11-22 Lockheed Martin Corporation System and method for three-dimensional (3D) computer-aided manufacturing (CAM) of an ensemble of pilot equipment and garments

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1960544A (en) * 1932-06-06 1934-05-29 Malcom Robert Mask
US2005072A (en) * 1934-10-15 1935-06-18 William H Lea Breathing mask
US2882896A (en) * 1955-07-18 1959-04-21 Henry W Seeler Breathing apparatus
US3128469A (en) * 1959-08-06 1964-04-14 Ml Aviation Co Ltd Flying helmets
US3149632A (en) * 1961-02-01 1964-09-22 Goodrich Co B F Head covering assembly with face and visor seals
US3330273A (en) * 1964-10-15 1967-07-11 Puritan Compressed Gas Corp Oro-nasal face mask with improved sealing cuff
US3473166A (en) * 1968-01-29 1969-10-21 Eric Noel Mobbs Helmets
US3680555A (en) * 1969-03-20 1972-08-01 Draegerwerk Ag Protective mask with annular flushing chamber

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1960544A (en) * 1932-06-06 1934-05-29 Malcom Robert Mask
US2005072A (en) * 1934-10-15 1935-06-18 William H Lea Breathing mask
US2882896A (en) * 1955-07-18 1959-04-21 Henry W Seeler Breathing apparatus
US3128469A (en) * 1959-08-06 1964-04-14 Ml Aviation Co Ltd Flying helmets
US3149632A (en) * 1961-02-01 1964-09-22 Goodrich Co B F Head covering assembly with face and visor seals
US3330273A (en) * 1964-10-15 1967-07-11 Puritan Compressed Gas Corp Oro-nasal face mask with improved sealing cuff
US3473166A (en) * 1968-01-29 1969-10-21 Eric Noel Mobbs Helmets
US3680555A (en) * 1969-03-20 1972-08-01 Draegerwerk Ag Protective mask with annular flushing chamber

Cited By (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3971368A (en) * 1975-08-13 1976-07-27 Puritan Equipment, Inc. Combined oxygen mask and smoke goggle apparatus with automatic flush valve
US4136403A (en) * 1976-09-10 1979-01-30 Dragerwerk Aktiengesellschaft Head guard assembly comprising a protective helmet and a protective breathing mask
US4172455A (en) * 1976-12-28 1979-10-30 Intertechnique Breathing equipment for high altitude flights
US4116237A (en) * 1977-02-07 1978-09-26 Norman Birch Emergency breathing apparatus
US4174710A (en) * 1977-04-28 1979-11-20 Auergesellschaft Gmbh Connection between two different parts of a person's protective covering
US4227520A (en) * 1978-02-10 1980-10-14 Canadian Patents & Development Ltd. Safety helmet for miners
US4336799A (en) * 1980-09-03 1982-06-29 Banyaszati Aknamelyito Vallalat Apparatus for supplying oxygen to a user
US5078130A (en) * 1988-07-14 1992-01-07 Gentex Corporation Personnel headgear enabling free breathing of ambient air or selective breathing from various sources
US5355878A (en) * 1990-06-26 1994-10-18 Cam Lock (Uk) Ltd. Breathing equipment for aircrew
US5291880A (en) * 1990-08-16 1994-03-08 Cairns & Brother Inc. Protective helmet with protective facepiece connection and adjustment provision
US5687713A (en) * 1991-11-29 1997-11-18 Bahr; Erik W. Breathing mask
US5538001A (en) * 1992-06-12 1996-07-23 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Northern Ireland And Great Britain Oxygen masks
US5758639A (en) * 1992-09-08 1998-06-02 Ikonen; Alpo Combination of a helmet and a respiratror and a method for using it
GB2271285A (en) * 1992-10-09 1994-04-13 Michael Beard Automatic tensioner for a face mask harness
FR2732865A1 (en) * 1995-04-12 1996-10-18 Gentex Corp INTEGRATED HELMET SYSTEM
WO1999008556A1 (en) * 1997-08-15 1999-02-25 Honeywell Inc. Headgear having an articulated mounting mechanism for a visor
US5901369A (en) * 1997-08-15 1999-05-11 Honeywell Inc. Headgear having an articulated mounting mechanism for a visor
US6997178B1 (en) * 1998-11-25 2006-02-14 Thomson-Csf Sextant Oxygen inhaler mask with sound pickup device
US7017576B2 (en) 2000-06-14 2006-03-28 Fisher & Paykel Healthcare Limited Breathing assistance apparatus
US20040035428A1 (en) * 2000-06-14 2004-02-26 Fisher & Paykel Healthcare Limited Breathing assistance apparatus
US6886559B2 (en) 2001-07-02 2005-05-03 Be Intellectual Property, Inc. Multi-phase headset for pilots
AU2002354766B2 (en) * 2001-07-02 2007-08-09 Be Intellectual Property Inc Multi-phase headset for pilots
EP1418985A2 (en) * 2001-07-02 2004-05-19 BE Intellectual Property, Inc. Multi-phase headset for pilots
WO2003005765A3 (en) * 2001-07-02 2003-03-20 Be Intellectual Pty Inc Multi-phase headset for pilots
AU2007202982B2 (en) * 2001-07-02 2009-10-01 Be Intellectual Property, Inc. Multi-phase headset for pilots
EP1418985A4 (en) * 2001-07-02 2007-10-03 Be Intellectual Pty Inc Multi-phase headset for pilots
US7905232B2 (en) 2001-09-13 2011-03-15 Fisher & Paykel Healthcare Limited Breathing assistance apparatus
US20030047185A1 (en) * 2001-09-13 2003-03-13 Olsen Gregory James Breathing assistance apparatus
US20060266362A1 (en) * 2001-11-05 2006-11-30 Smith Nicholas C A Nasal masks
US20050028820A1 (en) * 2001-11-05 2005-02-10 Smith Nicholas Charles Alan Nasal masks
US7096867B2 (en) * 2001-11-05 2006-08-29 Fisher & Paykel Healthcare Limited Nasal masks
US7934497B1 (en) * 2001-11-19 2011-05-03 The United States Of America As Represented By The Secretary Of The Army Modular helmet-mask assembly
US20060060193A1 (en) * 2002-09-27 2006-03-23 Richardson Grant S Respirator
US20070289594A1 (en) * 2002-09-30 2007-12-20 Be Intellectual Property, Inc. Full face flexible oxygen mask for use with flight helmets
US8028700B2 (en) 2002-09-30 2011-10-04 Be Intellectual Property, Inc. Full face flexible oxygen mask for use with flight helmets
US7278421B2 (en) * 2002-09-30 2007-10-09 Be Intellectual Property, Inc. Full face flexible oxygen mask for use with flight helmets
US20040244801A1 (en) * 2002-09-30 2004-12-09 Hannah Gary R. Full face flexible oxygen mask for use with flight helmets
US7770240B2 (en) * 2005-05-27 2010-08-10 Dräger Safety AG & Co. KGaA Safety helmet with a breathing mask
US20060277665A1 (en) * 2005-05-27 2006-12-14 Drager Safety Ag & Co. Kgaa Safety helmet with a breathing mask
US7694680B2 (en) * 2005-11-14 2010-04-13 Nevada Aviation Safety Consultants, Inc. Aviator emergency oxygen system
US20070107727A1 (en) * 2005-11-14 2007-05-17 Brichetto David Mr Aviator emergency oxygen system
US8286270B2 (en) * 2009-03-16 2012-10-16 Danastem Sports Enr. Helmet having a guiding mechanism for a compatible visor
US20100229288A1 (en) * 2009-03-16 2010-09-16 Danny Higgins Helmet having a guiding mechanism for a compatible visor
ITUB20153701A1 (en) * 2015-09-17 2017-03-17 Caberg Spa JET TYPE HELMET STRUCTURE WITH INCORPORATED VISOR
US20190008228A1 (en) * 2016-12-30 2019-01-10 David Francis Ramey Integrated non-conflicting headgear platform system and method
US20190350301A1 (en) * 2017-02-21 2019-11-21 Unit 1 Gear, Inc. Headphone and helmet assembly
US10791788B2 (en) * 2017-02-21 2020-10-06 Unit 1 Gear, Inc. Headphone and helmet assembly
US11507056B1 (en) * 2020-04-06 2022-11-22 Lockheed Martin Corporation System and method for three-dimensional (3D) computer-aided manufacturing (CAM) of an ensemble of pilot equipment and garments
US20220390921A1 (en) * 2020-04-06 2022-12-08 Lockheed Martin Corporation System and method for three-dimensional (3d) computer-aided manufacturing (cam) of an ensemble of pilot equipment and garments
US11822312B2 (en) * 2020-04-06 2023-11-21 Lockheed Martin Corporation System and method for three-dimensional (3D) computer-aided manufacturing (CAM) of an ensemble of pilot equipment and garments

Similar Documents

Publication Publication Date Title
US3910269A (en) Integrated helmet and mask structure
US3833935A (en) Integrated helmet and mask structure
US3362403A (en) Unified helmet and oxygen breathing assembly
US5655527A (en) Respiratory mask with floating seal responsive to pressurized gas
US5492116A (en) Respiratory mask with floating seal responsive to pressurized gas
US4059852A (en) Inflatable suit for cyclists
US2935985A (en) Airtight helmet
CA1180629A (en) Respirator hood
US5630412A (en) Protective equipment for the head comprising a breathing mask and an optical screen
US3860966A (en) Safety helmet
US4116237A (en) Emergency breathing apparatus
US3991423A (en) Helmet with actuated neck pad
US5410757A (en) Face shield
US3234939A (en) Quick-donning mask suspension
US4484575A (en) Loose fitting supplied air respirator hood
US4698856A (en) Ventilated helmet
EP1400262B1 (en) High G oxygen mask for aircrew
GB1581218A (en) Portable breathing apparatus
US2642574A (en) Helmet for protection against low-temperatures
CN104023798B (en) Store the method for breathing mask and the breathing equipment including breathing mask and storage element
US3307202A (en) Faceband equipped headwear
US2597764A (en) Crash helmet
US4173220A (en) Facemask
US3130415A (en) Helmet assembly with face seal and adjustment means therefor
US4671775A (en) Survival hood

Legal Events

Date Code Title Description
AS Assignment

Owner name: TEXACE CORPORATION A CORP. OF TEX.

Free format text: CHANGE OF NAME;ASSIGNOR:CAPTECH INC.;REEL/FRAME:003996/0930

Effective date: 19781110

Owner name: SCOTT AVIATION-SIERRA PRODUCTS, INC.,

Free format text: CHANGE OF NAME;ASSIGNOR:TEXACE CORPORATION;REEL/FRAME:003996/0919

Effective date: 19781110

Owner name: TEXACE CORPORATION, A CORP. OF TX

Free format text: MERGER;ASSIGNORS:CAPTECH INC., A CORP. OF CA.;TEXACE CORPORATION, A CORP. OF TX;REEL/FRAME:003950/0653

Effective date: 19781110

Owner name: CAPTECH INC.

Free format text: NUNC PRO TUNC ASSIGNMENT;ASSIGNOR:SIERRA ENGINEERING CO.;REEL/FRAME:003996/0923

Effective date: 19690728

AS Assignment

Owner name: FIGGIE INTERNATIONAL INC., 4420 SHERWIN RD. WILLOU

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:SCOTT AVIATION-SIERRA PRODUCTS, INC.;REEL/FRAME:003961/0236

Effective date: 19811105

AS Assignment

Owner name: FIGGIE INTERNATIONAL INC.

Free format text: MERGER;ASSIGNOR:FIGGIE INTERNATIONAL INC., (MERGED INTO) FIGGIE INTERNATIONAL HOLDINGS INC. (CHANGED TO);REEL/FRAME:004767/0822

Effective date: 19870323