GB510418A - Improvements in and relating to the driving of aircraft propellors - Google Patents

Improvements in and relating to the driving of aircraft propellors

Info

Publication number
GB510418A
GB510418A GB34875/38A GB3487538A GB510418A GB 510418 A GB510418 A GB 510418A GB 34875/38 A GB34875/38 A GB 34875/38A GB 3487538 A GB3487538 A GB 3487538A GB 510418 A GB510418 A GB 510418A
Authority
GB
United Kingdom
Prior art keywords
casing
aircraft
supporting
engine
propeller shaft
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
GB34875/38A
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.)
Airbus Defence and Space GmbH
Junkers Flugzeug und Motorenwerke AG
Original Assignee
Messerschmitt Bolkow Blohm AG
Junkers Flugzeug und Motorenwerke AG
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 Messerschmitt Bolkow Blohm AG, Junkers Flugzeug und Motorenwerke AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB510418A publication Critical patent/GB510418A/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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby

Abstract

510,418. Propelling aircraft. JUNKERS FLUGZEUG-UND-MOTORENWERKE AKT.- GES. Nov. 30, 1938. No. 34875. Convention date, Dec. 10, 1937. [Class 4] , . In aircraft engines which-are mounted so as project beyond the post of the aircraft on which they are supported and so that the reactiontorque is transmitted to the supporting post through the engine casing or an intermediate part supporting the casing, the engine torque is transmitted to the propeller shaft in the vicinity of the point at which the engine casing is held against twisting in relation to the supporting post. In one form, Fig. 1, a reciprocating engine is mounted on a supporting part 8 by two sets of struts 11, 12, 13, 14, attached in pairs at 15 and 16 to the crankcase 7 and at 17 and 18 to the part 8. The struts 12 14 absorb the reaction torque and the reduction gear 24, 26 transmitting torque from the crankshaft 25 to the propeller shaft 23 is located adjacent the attachment 16. In a second form the casing 31 of a turbine 30 is attached to a supporting part 8 by screws 32, the tubular shaft 44, carrying the rotors, driving the propeller shaft 23 through a reduction gear 35, 36; 37, 38 located adjacent the rear of the casing.
GB34875/38A 1937-12-10 1938-11-30 Improvements in and relating to the driving of aircraft propellors Expired GB510418A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE510418X 1937-12-10

Publications (1)

Publication Number Publication Date
GB510418A true GB510418A (en) 1939-08-01

Family

ID=6547439

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34875/38A Expired GB510418A (en) 1937-12-10 1938-11-30 Improvements in and relating to the driving of aircraft propellors

Country Status (1)

Country Link
GB (1) GB510418A (en)

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