AT77570B - Aircraft engine coolers. - Google Patents

Aircraft engine coolers.

Info

Publication number
AT77570B
AT77570B AT77570DA AT77570B AT 77570 B AT77570 B AT 77570B AT 77570D A AT77570D A AT 77570DA AT 77570 B AT77570 B AT 77570B
Authority
AT
Austria
Prior art keywords
aircraft
aircraft engine
fuselage
coolers
cooler
Prior art date
Application number
Other languages
German (de)
Inventor
Reinhold Richter
Original Assignee
Reinhold Richter
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 Reinhold Richter filed Critical Reinhold Richter
Application granted granted Critical
Publication of AT77570B publication Critical patent/AT77570B/en

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

  

   <Desc/Clms Page number 1> 
 



  Kühler für Flugzeugmotoren. 



   Die vorliegende Erfindung betrifft einen   Ein. oder Zweiseitenkühlar für Flugzeug.   motoren, dessen innere Ausgestaltung sich im wesentlichen mit der Bauart und dem inneren
Aufbau der bekannten Stirnkühler deckt. Der Erfindung gemäss ist jedoch seine   Stirnfläche   nicht wie beim Stirnkühler gegen die horizontale Mittelebene des Rumpfes, sondern gegen dessen vertikale Mittelebene unter einem bestimmten Winkel geneigt. Hiedurch, wie durch seine Anpassung an die Spantform des Rumpfes, wird der Luftwiderstand verringert und seine Beschädigungsgefahr bei Kopfstürzen beseitigt. 



   In der Zeichnung stellt Fig. 1 eine Vorderansicht, Fig. 2 eine Aufsicht des an-   gebauten Kühlers dar. 



  A ist der Rumpf, B der Kühler, welcher auf beiden Seiten des Rumpfes oder unter   entsprechender   Vergrösserung   auf einer Seite angebaut werden kann. 

**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.



   <Desc / Clms Page number 1>
 



  Aircraft engine coolers.



   The present invention relates to a one. or two-sided cooler for aircraft. motors, the internal configuration of which is essentially related to the type and the internal
Structure of the well-known forehead cooler covers. According to the invention, however, its end face is not inclined towards the horizontal central plane of the fuselage, as is the case with the forehead cooler, but rather towards its vertical central plane at a certain angle. This, as well as its adaptation to the shape of the frame of the trunk, reduces the air resistance and eliminates the risk of damage in the event of a head fall.



   In the drawing, FIG. 1 shows a front view and FIG. 2 shows a top view of the built-on cooler.



  A is the fuselage, B is the cooler, which can be attached to both sides of the fuselage or on one side with a corresponding enlargement.

** WARNING ** End of DESC field may overlap beginning of CLMS **.

Claims (1)

PATENT-ANSPRUCH ; Kühler für Flugzeugmotoren, welcher seitlich am Flugzeug angeordnet ist und dessen innerer Aufbau den bekannten Stirnkühlern gleicht, dadurch gekennzeichnet, dass seine Stirnfläche unter einem bestimmten Winkel gegen die vertikale Mittelebene des Flugzeugrumpfes steht und dass er der Spantform des Rumpfes angepasst ist. EMI1.1 **WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. PATENT CLAIM; Cooler for aircraft engines, which is arranged on the side of the aircraft and whose internal structure is similar to the known forehead coolers, characterized in that its Front face is at a certain angle to the vertical center plane of the aircraft fuselage and that it is adapted to the frame shape of the fuselage. EMI1.1 ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT77570D 1915-11-29 1915-11-29 Aircraft engine coolers. AT77570B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT77570T 1915-11-29

Publications (1)

Publication Number Publication Date
AT77570B true AT77570B (en) 1919-08-11

Family

ID=3599177

Family Applications (1)

Application Number Title Priority Date Filing Date
AT77570D AT77570B (en) 1915-11-29 1915-11-29 Aircraft engine coolers.

Country Status (1)

Country Link
AT (1) AT77570B (en)

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