US20070235169A1 - Military Electronic Apparatus - Google Patents
Military Electronic Apparatus Download PDFInfo
- Publication number
- US20070235169A1 US20070235169A1 US11/562,356 US56235606A US2007235169A1 US 20070235169 A1 US20070235169 A1 US 20070235169A1 US 56235606 A US56235606 A US 56235606A US 2007235169 A1 US2007235169 A1 US 2007235169A1
- Authority
- US
- United States
- Prior art keywords
- electronic apparatus
- military
- heat insulation
- heat
- detection
- 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.)
- Abandoned
Links
- 238000001514 detection method Methods 0.000 claims abstract description 37
- 238000009413 insulation Methods 0.000 claims abstract description 19
- 239000011248 coating agent Substances 0.000 claims description 9
- 238000000576 coating method Methods 0.000 claims description 9
- 239000012774 insulation material Substances 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 6
- 239000003973 paint Substances 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J2/00—Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic or acoustic waves
- F41J2/02—Active targets transmitting infrared radiation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H3/00—Camouflage, i.e. means or methods for concealment or disguise
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L23/00—Details of semiconductor or other solid state devices
- H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2924/00—Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
- H01L2924/0001—Technical content checked by a classifier
- H01L2924/0002—Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
Definitions
- the present invention relates to a military electronic apparatus that may not be detected by a thermal detection signal and more particularly to use a shell or a coating to achieve the goal of stealth.
- FIG. 1 a schematic diagram illustrates an electronic apparatus for use in the military environment.
- a heat energy generated by the electronic apparatus 13 may be sensed by a thermal detection signal 12 generated from a thermal detection apparatus 11 .
- the position of the electronic apparatus 13 may be further detected to endanger the safety of users. Therefore, insulating a heat source within the electronic apparatus to prevent the electronic apparatus from being detected by the thermal detection apparatus, and further absorbing the thermal detection signal generated from the thermal detection apparatus are very important issues for military electronic apparatuses.
- the inventor of the present invention based on years of experience on related research and development invents a military electronic apparatus to overcome the foregoing shortcomings.
- an object of the present invention is to provide a military electronic apparatus that will not be detected by a thermal detection signal. Furthermore, a shell and a coating are used to insulate a heat source within an electronic apparatus. A signal generated from a thermal detection apparatus is also absorbed. The military electronic apparatus may not be traced by the thermal detection apparatus so as to achieve the goal of stealth.
- the military electronic apparatus is used to prevent detection of the thermal detection signal
- the military electronic apparatus includes an electronic apparatus, a heat insulation element and an anti-detection element.
- Heat energy is generated by the electronic apparatus while operating.
- the heat insulation element is disposed upon a surface of the electronic apparatus for insulating the heat energy generated from the electronic apparatus.
- the anti-detection element is disposed upon a surface of the heat insulation element for absorbing the thermal detection signal.
- the electronic apparatus is preferably a computer.
- FIG. 1 is a schematic diagram illustrating an electronic apparatus in the military environment
- FIG. 2 is a block diagram illustrating a military electronic apparatus according to an embodiment of the invention.
- FIG. 3 is a block diagram illustrating the military electronic apparatus according to a preferred embodiment of the invention.
- FIG. 2 a block diagram illustrates a military electronic apparatus according to an embodiment of the invention.
- the military electronic apparatus includes an electronic apparatus 22 , a heat insulation element 23 and an anti-detection element 24 .
- a thermal detection signal 21 is sent from a thermal detection apparatus 26 .
- Heat energy 25 is generated by the electronic apparatus 22 while operating.
- the heat insulation element 23 is disposed on a surface of the electronic apparatus 22 for insulating the heat energy 25 generated from the electronic apparatus 22 .
- the anti-detection element 24 is disposed on a surface of the heat insulation element 23 for absorbing the thermal detection signal 21 .
- the heat insulation element 23 is a shell made by a heat insulation material or is heat insulation coating.
- the anti-detection element 24 is a shell made by an anti-thermal detection material, or is anti-thermal detection coating.
- the electronic apparatus 22 is preferably a computer system.
- the military electronic apparatus further includes a heat conduction element for conducting the heat energy 25 to the outside of the military electronic apparatus.
- FIG. 3 a block diagram illustrates the military electronic apparatus according to a preferred embodiment of the invention.
- the military electronic apparatus includes a computer system 32 , heat insulation coating 33 , anti-detection paint 34 and a heat conduction element 37 .
- An infrared thermal signal 31 sent from an infrared thermal sensor 36 is used to detect heat energy 35 .
- the heat energy 35 is generated by the computer system 32 while operating.
- the heat insulation coating 33 is coated on a surface of the computer system 32 for insulating the heat energy 35 generated from the computer system 32 .
- the anti-detection paint 34 is coated on a surface of the heat insulation coating 33 for absorbing the infrared thermal signal 31 .
- the heat conduction element 37 is for conducting the heat energy 35 to the outside of the military electronic apparatus.
Abstract
A military electronic apparatus is used to prevent detection of a thermal detection signal The military electronic apparatus comprises an electronic device, a heat insulation element and an anti-detection element. Heat energy is generated by the electronic device while operating. The heat insulation element is disposed on a surface of the electronic device for insulating the heat energy generated by the electronic device. The anti-detection element is disposed on a surface of the heat insulation element for absorbing the thermal detection signal.
Description
- The present invention relates to a military electronic apparatus that may not be detected by a thermal detection signal and more particularly to use a shell or a coating to achieve the goal of stealth.
- Electronic apparatuses may process more and more data because the processing speed is increased. However, heat energy generated from the electronic apparatus is also increased. When in a usual environment, if the heat dissipation can be overcome, the electronic apparatuses may operate normally. However, when the electronic apparatuses are used in a military environment, the situation may be different. Referring to
FIG. 1 , a schematic diagram illustrates an electronic apparatus for use in the military environment. A heat energy generated by theelectronic apparatus 13 may be sensed by athermal detection signal 12 generated from athermal detection apparatus 11. The position of theelectronic apparatus 13 may be further detected to endanger the safety of users. Therefore, insulating a heat source within the electronic apparatus to prevent the electronic apparatus from being detected by the thermal detection apparatus, and further absorbing the thermal detection signal generated from the thermal detection apparatus are very important issues for military electronic apparatuses. - To insulate the heat source within the electronic apparatus, the inventor of the present invention based on years of experience on related research and development invents a military electronic apparatus to overcome the foregoing shortcomings.
- Accordingly, an object of the present invention is to provide a military electronic apparatus that will not be detected by a thermal detection signal. Furthermore, a shell and a coating are used to insulate a heat source within an electronic apparatus. A signal generated from a thermal detection apparatus is also absorbed. The military electronic apparatus may not be traced by the thermal detection apparatus so as to achieve the goal of stealth.
- To achieve the forgoing object, the military electronic apparatus is used to prevent detection of the thermal detection signal The military electronic apparatus includes an electronic apparatus, a heat insulation element and an anti-detection element. Heat energy is generated by the electronic apparatus while operating. The heat insulation element is disposed upon a surface of the electronic apparatus for insulating the heat energy generated from the electronic apparatus. The anti-detection element is disposed upon a surface of the heat insulation element for absorbing the thermal detection signal. The electronic apparatus is preferably a computer.
- The military electronic apparatus of the invention has advantages as follows:
- (1). The computer in the military environment could still operate normally and continuously without influence from the inside heat.
- (2). The position of a user may not be divulged through the computer in the military environment due to the inside heat.
- (3). The usability of the computer in the military environment could be increased without influence from the inside heat.
- (4). The operation efficiency of the computer in the military environment could be increased without influence from the inside heat.
- Other features and advantages of the present invention and variations thereof will become apparent from the following description, drawings, and claims.
-
FIG. 1 is a schematic diagram illustrating an electronic apparatus in the military environment; -
FIG. 2 is a block diagram illustrating a military electronic apparatus according to an embodiment of the invention; and -
FIG. 3 is a block diagram illustrating the military electronic apparatus according to a preferred embodiment of the invention. - Referring to
FIG. 2 , a block diagram illustrates a military electronic apparatus according to an embodiment of the invention. The military electronic apparatus includes anelectronic apparatus 22, aheat insulation element 23 and ananti-detection element 24. Athermal detection signal 21 is sent from athermal detection apparatus 26.Heat energy 25 is generated by theelectronic apparatus 22 while operating. Theheat insulation element 23 is disposed on a surface of theelectronic apparatus 22 for insulating theheat energy 25 generated from theelectronic apparatus 22. Theanti-detection element 24 is disposed on a surface of theheat insulation element 23 for absorbing thethermal detection signal 21. - The
heat insulation element 23 is a shell made by a heat insulation material or is heat insulation coating. Theanti-detection element 24 is a shell made by an anti-thermal detection material, or is anti-thermal detection coating. Moreover, theelectronic apparatus 22 is preferably a computer system. The military electronic apparatus further includes a heat conduction element for conducting theheat energy 25 to the outside of the military electronic apparatus. - Referring to
FIG. 3 , a block diagram illustrates the military electronic apparatus according to a preferred embodiment of the invention. The military electronic apparatus includes acomputer system 32,heat insulation coating 33,anti-detection paint 34 and aheat conduction element 37. An infraredthermal signal 31 sent from an infraredthermal sensor 36 is used to detectheat energy 35. Theheat energy 35 is generated by thecomputer system 32 while operating. Theheat insulation coating 33 is coated on a surface of thecomputer system 32 for insulating theheat energy 35 generated from thecomputer system 32. Theanti-detection paint 34 is coated on a surface of theheat insulation coating 33 for absorbing the infraredthermal signal 31. Theheat conduction element 37 is for conducting theheat energy 35 to the outside of the military electronic apparatus. - Although the features and advantages of the embodiments according to the preferred invention are disclosed, it is not limited to the embodiments described above, but encompasses any and all modifications and changes within the spirit and scope of the following claims.
Claims (7)
1. A military electronic apparatus, applicable for preventing detection of a thermal detection signal comprising:
an electronic apparatus being operated to additionally generate a heat energy;
a heat insulation element disposed upon a surface of said electronic device for insulating said heat energy generated by said electronic apparatus; and
an anti-detection element disposed upon a surface of said heat insulation element for absorbing said thermal detection signal.
2. The military electronic apparatus of claim 1 , wherein said electronic apparatus is a computer system.
3. The military electronic apparatus of claim 1 , wherein said heat insulation element is a shell made by a heat insulation material.
4. The military electronic apparatus of claim 1 , wherein said heat insulation element is heat insulation coating.
5. The military electronic apparatus of claim 1 , wherein said military electronic apparatus further includes a heat conduction element for conducting said heat energy to the outside of said military electronic apparatus.
6. The military electronic apparatus of claim 1 , wherein said anti-detection element is a shell made by an anti-thermal detection material.
7. The military electronic apparatus of claim 1 , wherein said anti-detection element is anti-thermal detection coating.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/562,356 US20070235169A1 (en) | 2006-01-25 | 2006-11-21 | Military Electronic Apparatus |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW95201697U TWM296512U (en) | 2006-01-25 | 2006-01-25 | Military electronic apparatus |
TW095201697 | 2006-01-25 | ||
US82993106P | 2006-10-18 | 2006-10-18 | |
US11/562,356 US20070235169A1 (en) | 2006-01-25 | 2006-11-21 | Military Electronic Apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
US20070235169A1 true US20070235169A1 (en) | 2007-10-11 |
Family
ID=38573914
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/562,356 Abandoned US20070235169A1 (en) | 2006-01-25 | 2006-11-21 | Military Electronic Apparatus |
Country Status (1)
Country | Link |
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US (1) | US20070235169A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110157814A1 (en) * | 2009-12-30 | 2011-06-30 | Foxconn Technology Co., Ltd. | Notebook computer with thermal insulating layer |
US8751710B2 (en) | 2012-05-08 | 2014-06-10 | Entegra Technologies, Inc. | Reconfigurable modular computing device |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4019699A (en) * | 1974-04-30 | 1977-04-26 | Teledyne Ryan Aeronautical A Division Of Teledyne Industries, Inc. | Aircraft of low observability |
US4020739A (en) * | 1976-07-16 | 1977-05-03 | The United States Of America As Represented By The Secretary Of The Army | Fire control system |
US4156033A (en) * | 1977-05-04 | 1979-05-22 | The United States Of America As Represented By The Secretary Of The Army | Thermal camouflage |
US4529633A (en) * | 1983-01-14 | 1985-07-16 | Diab-Barracuda Ab | Thermal camouflage |
US20040048939A1 (en) * | 2000-12-08 | 2004-03-11 | Kuehl Scott Allan | Electromagnetic energy adaptation material |
US6980418B1 (en) * | 2002-05-06 | 2005-12-27 | Apple Computer, Inc. | Method and apparatus for controlling the temperature of electronic device enclosures |
-
2006
- 2006-11-21 US US11/562,356 patent/US20070235169A1/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4019699A (en) * | 1974-04-30 | 1977-04-26 | Teledyne Ryan Aeronautical A Division Of Teledyne Industries, Inc. | Aircraft of low observability |
US4020739A (en) * | 1976-07-16 | 1977-05-03 | The United States Of America As Represented By The Secretary Of The Army | Fire control system |
US4156033A (en) * | 1977-05-04 | 1979-05-22 | The United States Of America As Represented By The Secretary Of The Army | Thermal camouflage |
US4529633A (en) * | 1983-01-14 | 1985-07-16 | Diab-Barracuda Ab | Thermal camouflage |
US20040048939A1 (en) * | 2000-12-08 | 2004-03-11 | Kuehl Scott Allan | Electromagnetic energy adaptation material |
US6980418B1 (en) * | 2002-05-06 | 2005-12-27 | Apple Computer, Inc. | Method and apparatus for controlling the temperature of electronic device enclosures |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110157814A1 (en) * | 2009-12-30 | 2011-06-30 | Foxconn Technology Co., Ltd. | Notebook computer with thermal insulating layer |
US8751710B2 (en) | 2012-05-08 | 2014-06-10 | Entegra Technologies, Inc. | Reconfigurable modular computing device |
US8924609B2 (en) | 2012-05-08 | 2014-12-30 | Entegra Technologies, Inc. | Reconfigurable modular computing device |
US9213664B2 (en) | 2012-05-08 | 2015-12-15 | Entegra Technologies, Inc. | Reconfigurable modular computing device |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: TWINHEAD INTERNATIONAL CORP., TAIWAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:CHEN, RUI-GUANG;REEL/FRAME:020484/0705 Effective date: 20060407 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |