DE386203C - Device for cooling two reciprocally related aircraft engines - Google Patents

Device for cooling two reciprocally related aircraft engines

Info

Publication number
DE386203C
DE386203C DET26478D DET0026478D DE386203C DE 386203 C DE386203 C DE 386203C DE T26478 D DET26478 D DE T26478D DE T0026478 D DET0026478 D DE T0026478D DE 386203 C DE386203 C DE 386203C
Authority
DE
Germany
Prior art keywords
engine
cooling
aircraft engines
aircraft
related aircraft
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
Application number
DET26478D
Other languages
German (de)
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.)
Individual
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of DE386203C publication Critical patent/DE386203C/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Description

Einrichtung zum Kühlen zweier in wechselseitiger Beziehung stehender Flugzeugmotoren. Die Erfindung betrifft eine Einrichtung zum Kühlen zweier in wechselseitiger Beziehung stehender Flugzeugmotoren, von denen der kleinere zum Anlassen des eigentlichen Flugzeugmotors und zum Treiben der Flugzeugräder dient, und besteht im wesentlichen darin, daß idie beiiden Motoren eine gemeinsame Wasserzirkulation besitzen, die so getroffen ist, daß bei der Ingangsetzung des kleinen Motors das Kühlwasser, das 'die Zylinder des anderen Motors bespült, rasch erwärmt werden kann. Auf diese Weise werden die Zylinder des großen Motors schnell erwärmt.Device for cooling two mutually related Aircraft engines. The invention relates to a device for cooling two mutually Related aircraft engines, the smaller of which is used to start the actual Aircraft engine and serves to drive the aircraft wheels, and consists essentially in the fact that the two engines have a common water circulation, the is such that when the small engine is started, the cooling water, the 'the cylinders of the other motor are flushed and heated up quickly can. In this way, the cylinders of the large engine are warmed up quickly.

Die Zeichnung veranschaulicht eine Ausführungsform des Erfindungsgegenstandes in Anwendung hei zwei in wechselseitiger Beziehung stehenden Flugzeugmotoren. Der Flug zeugmötor io treibt den Propeller ii und kann bei eingerückten Kupplungen 13, 14 und 17,18 durch die Zwischenräder 15, 16 mittels des kleineren Motors 12 angelassen werden, der bei ausgerückter Kupplung 17, i8 durch ein Wechselgetriebe 21, 22, 23 die Welle 2o und dadurch die Flugzeugräder treiben kann. Zum Artgassen des kleineren Motors 12 kann auch umgekehrt der Flugzeugmotor io herangezogen werden.The drawing illustrates an embodiment of the subject matter of the invention in use with two mutually related aircraft engines. The Flugzeugmötor io drives the propeller ii and can be started with the clutches 13, 14 and 17,18 engaged by the intermediate gears 15, 16 by means of the smaller motor 12, which with disengaged clutch 17, i8 by a gearbox 21, 22, 23 die Wave 2o and thereby can drive the aircraft wheels. Conversely, the aircraft engine io can also be used for the type alleys of the smaller engine 12.

Erfindungsgemäß ist der Flugzeugmotor io mit einem Kühler 29 versehen, welcher mittels passender Rohre 3, q. nicht nur mit den Kraftzylindern des Motors io, sondern auch mit denen des Motors 12 verbunden ist. In dieser Weise ist es möglich, für beide Motoren einen gemeinsamen Wasserumlauf vorzusehen, wobei der während des Fluges arbeitende Kühler zur Kühlung des kleinen Motors benutzt wird, wenn dieser auf die Welle 2o einwirkt. Insbesondere gestattet die neue Vorrichtung bei Ingangsetzung des kleinen Motors 12, das die Zylinder des Motors io bespülende Wasser rasch anzuwärmen, was wiederum ermöglicht, das Kleben der Kolbensegmente zu beseitigen und beim Anlassen den Ölumlauf in der Kraftmaschine zu erleichtern.According to the invention, the aircraft engine is provided with a cooler 29, which by means of matching pipes 3, q. not just with the power cylinders of the engine io, but also with those of the engine 12 is connected. In this way it is possible to provide a common water circulation for both engines, whereby the during the In-flight cooler is used to cool the small engine when it is acts on the shaft 2o. In particular, the new device allows upon start-up of the small engine 12 to quickly warm the water flushing the cylinders of the engine, which in turn makes it possible to eliminate the sticking of the piston segments and when starting to facilitate the oil circulation in the engine.

Claims (1)

PATENTANSPRUCH: Einrichtung zum Kühlen zweier in wechselseitiger Beziehung stehender Flugzeugmotoren, von denen der kleinere zum Anlassen des eigentlichen Flugzeugmotors und zum Treiben der Flugzeugräder dient, dadurch gekennzeichnet, da$ die beiden Motoren (io,12) einen gemeinsamen Wasserumlauf besitzen, in welchem bei der Ingangsetzung des kleinen Motors das die Zylinder des anderen Motors bespülende Wasser erwärmt wird. Claim: Device for cooling two mutually related aircraft engines, the smaller of which is used to start the actual aircraft engine and to drive the aircraft wheels, characterized in that the two motors (10, 12) have a common water circuit in which the Starting the small engine, the water flushing the cylinders of the other engine is heated.
DET26478D 1919-01-16 1921-03-25 Device for cooling two reciprocally related aircraft engines Expired DE386203C (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR386203X 1919-01-16

Publications (1)

Publication Number Publication Date
DE386203C true DE386203C (en) 1923-12-17

Family

ID=8895726

Family Applications (1)

Application Number Title Priority Date Filing Date
DET26478D Expired DE386203C (en) 1919-01-16 1921-03-25 Device for cooling two reciprocally related aircraft engines

Country Status (1)

Country Link
DE (1) DE386203C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE765764C (en) * 1940-11-16 1953-02-09 Maybach Motorenbau G M B H Device for warming up internal combustion engines, in particular for motor vehicles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE765764C (en) * 1940-11-16 1953-02-09 Maybach Motorenbau G M B H Device for warming up internal combustion engines, in particular for motor vehicles

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