DE300174C - - Google Patents
Info
- Publication number
- DE300174C DE300174C DENDAT300174D DE300174DA DE300174C DE 300174 C DE300174 C DE 300174C DE NDAT300174 D DENDAT300174 D DE NDAT300174D DE 300174D A DE300174D A DE 300174DA DE 300174 C DE300174 C DE 300174C
- Authority
- DE
- Germany
- Prior art keywords
- cooler
- nacelle
- circular
- ring
- coolers
- 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.)
- Active
Links
- 238000001816 cooling Methods 0.000 claims description 4
- 230000001105 regulatory Effects 0.000 claims description 2
- 210000002356 Skeleton Anatomy 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000002349 favourable Effects 0.000 description 1
- 210000000056 organs Anatomy 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
Description
Bei den bisher üblichen Ausführungen der mit Explosionsmotoren betriebenen Luftfahrzeuge wurden die Kühler für AVasscr oder Öl außerhalb des Gondelkörpers an beliebiger, für die Bedienung möglichst geeigneter Stelle, und zAvar meistens in Verbindung mit dem Schiffsgerippe selbst untergebracht. Bei einigen Bauarten befinden sich die Kühler auch neben oder in den Gondelseitenwänden.In the previously common designs of aircraft operated with explosion engines were the coolers for AVasscr or oil outside the nacelle body at any for the operation as suitable as possible, and zAvar mostly in connection with housed in the skeleton of the ship itself. In some designs there are coolers also next to or in the side walls of the gondola.
ίο Alle diese Ausführungen haben entweder den Nachteil, durch die großen im Luftstrom befindlichen Querschnitte erhebliche Widerstände zu billden, oder sie bringen ungenügende Bedienungsmöglichkeiten, schlechte Übersicht und Zugänglichkeit sowie unbefriedigende Regelung der Kühlluft mit sich.ίο All of these designs have either the disadvantage of considerable resistance due to the large cross-sections in the air flow to bill, or they bring inadequate operating options, poor overview and accessibility as well as unsatisfactory Regulation of the cooling air with it.
Die vorliegende und i;m folgendün beschriebene Erfindung vermeidet alle diese Nachteile' und verbindet geringsten Luftwiderstand mit guter Übersicht und Bedienungsmöglichkeit bei weitgehender Kühlung und beliebiger Regelung derselben.The present and i; m described below The invention avoids all of these disadvantages and combines the lowest possible air resistance with a good overview and operating options with extensive cooling and any control of the same.
Die in windschnittiger Form ausgeführte Gondel beliebigen Querschnittes wird im Vorderteil durch eine der Form der äußeren Begrenzungslinie angepaßte Innenwand in zwei ungleich große Räume geteilt. In dem vorderen der Windrichtung entgegengesetzten Räume sind die jeweils erforderlichen Kühler angebracht. Die Umfangslinien und Formen der Kühler passen sich den Linien des Gondelkörpers an. Die Kühler sind in Kanalräumen eingebaut, die gleichzeitig den durchtretenden Kühlluftmengen genügende Abflußquerschnitte günstiger Formgebung bieten. Die Kühler selbst erhalten jeweils beliebige der Gondelbauart entsprechende Formen. The streamlined gondola with any cross-section is used in the Front part through an inner wall adapted to the shape of the outer boundary line in divided two rooms of unequal size. In the front opposite the wind direction The cooler required in each case is attached to the rooms. The perimeter lines and The shapes of the coolers adapt to the lines of the nacelle body. The coolers are in Built-in duct spaces, the drainage cross-sections that are sufficient for the amount of cooling air that passes through offer more favorable design. The coolers themselves are given any shape that corresponds to the type of nacelle.
In Abb. ι sind1 zwei Kühler derart angeordnet, daß der Kreiskühler α in der Mitte und der Ringkühler b hinter α um die Gondelmittellinie angeordnet sind.In Fig. 1 two coolers are arranged such that the circular cooler α in the middle and the ring cooler b are arranged behind α around the center line of the nacelle.
Die den Vorderteil des Gondelkörpers treffende Luft geht durch die Kühler α und b, wird durch die dahinterliegenden und dem 4S inneren Gondelumfang angepaßten Luftkanalräume c geleitet und tritt durch Öffnungen d am Gondelumfang ins Freie. Die Öffnungen für die Luftdurchströmung können durch beliebige Organe, die Öffnungen d z. B. durch die Schieber f, die Öffnungen; für den Mit-' tclkühler durch die Klappen c nach Bedarf ganz oder teilweise geschlossen werden, so daß jeder Kühler für sich geregelt werden kann.The air hitting the front part of the nacelle body passes through the coolers α and b, is passed through the air duct spaces c located behind them and adapted to the 4S inner circumference of the nacelle, and exits through openings d on the circumference of the nacelle. The openings for the air flow through any organs, the openings d z. B. through the slide f, the openings; for the central cooler can be completely or partially closed by the flaps c as required, so that each cooler can be regulated individually.
Der eigentliche Gondelinnenraum ist durch die mit Fenstern h und g versehene AVand i nach außen abgeschlossen. Die Fenster sind beliebig herausnehmbar, schieb- oder klappbar angeordnet, so daß die Bedienung der Kühler, Schieber, Klappen und der sonstigen Betriebsteile jederzeit ge\vährleistet ist.The actual interior of the gondola is closed off from the outside by the AVand i, which is provided with windows h and g. The windows can be removed, slid or folded as required, so that the cooler, slider, flaps and other operating parts can be operated at any time.
Ein weiteres Ausführungsbeispiel der Kühleranordnungen zeigen die Abb. 2 und 3.Another exemplary embodiment of the cooler arrangements is shown in FIGS. 2 and 3.
Claims (3)
Publications (1)
Publication Number | Publication Date |
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DE300174C true DE300174C (en) |
Family
ID=554179
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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DENDAT300174D Active DE300174C (en) |
Country Status (1)
Country | Link |
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DE (1) | DE300174C (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE852943C (en) * | 1942-05-07 | 1952-10-20 | Daimler Benz Ag | Aircraft engine with freely flown ring or drum cooler arranged in a ring nozzle in front of the engine |
DE929525C (en) * | 1942-10-08 | 1955-06-27 | Aeg | Electric motor-driven hand tools for sawing, filing, etc. like |
US7585932B2 (en) | 2005-08-16 | 2009-09-08 | Chevron Phillips Chemical Company Lp | Polymer compositions and processes for making and using same |
US7781484B2 (en) | 2004-02-17 | 2010-08-24 | Chevron Phillips Chemical Company Lp | Thiol ester compositions and processes for making and using same |
-
0
- DE DENDAT300174D patent/DE300174C/de active Active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE852943C (en) * | 1942-05-07 | 1952-10-20 | Daimler Benz Ag | Aircraft engine with freely flown ring or drum cooler arranged in a ring nozzle in front of the engine |
DE929525C (en) * | 1942-10-08 | 1955-06-27 | Aeg | Electric motor-driven hand tools for sawing, filing, etc. like |
US7781484B2 (en) | 2004-02-17 | 2010-08-24 | Chevron Phillips Chemical Company Lp | Thiol ester compositions and processes for making and using same |
US7989655B2 (en) | 2004-02-17 | 2011-08-02 | Chevron Phillips Chemical Company Lp | Thiol ester compositions and processes for making and using same |
US7585932B2 (en) | 2005-08-16 | 2009-09-08 | Chevron Phillips Chemical Company Lp | Polymer compositions and processes for making and using same |
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