GB538046A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB538046A
GB538046A GB7415/40A GB741540A GB538046A GB 538046 A GB538046 A GB 538046A GB 7415/40 A GB7415/40 A GB 7415/40A GB 741540 A GB741540 A GB 741540A GB 538046 A GB538046 A GB 538046A
Authority
GB
United Kingdom
Prior art keywords
shafts
shaft
engine
gearing
driven
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
GB7415/40A
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
Priority to GB7415/40A priority Critical patent/GB538046A/en
Publication of GB538046A publication Critical patent/GB538046A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
    • B64D35/04Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors

Abstract

538,046. Driving airscrews. TAMPIER, R. April 24, 1940, No. 7415. [Class 4] An airscrew shaft is driven from an engine shaft through a plurality of intermediate shafts disposed in parallel relationship and connected by gearing. Fig. 12 shows an aeroplane in which four airscrews are driven from a single engine 1 the shaft 5 of which drives through bevel gearing groups of parallel shafts 12, 13, 14, arranged in one plane within the wing, and to which two of the propeller shafts are connected by bevel gearing. The shaft 5 also drives a shaft 6 through a group of four shafts 24 arranged about a common centre in the fuselage and geared to the shafts 5, 6 by spur gearing. The shaft 6 drives two propeller shafts arranged behind the elevators by gearing similar to that which drives the other two propellers. The gears are chosen to give a speed reduction from the engine shaft to the propeller shaft but the intermediate shafts rotate at higher speeds than their driving shafts. In a modification the shaft 6 is driven by a separate engine in the fuselage. A single pair of propellers on the main wing may be driven by shafts similar to the shafts 12, 13, 14. Fig. 7 shows a modification in which propellers on the wings are driven, each through two groups of shafts 24 in addition to the shafts 12, 13, 14. Worm gearing may replace the bevel gearing. Two engines arranged side by side in the fuselage may drive groups of shafts similar to the shafts 12, 13, 14 the two engine shafts being geared together through three intermediate shafts coaxial with the shafts 12, 13, 14. Fig. 11 shows a modification in which two engines drive, through groups of shafts E. F' arranged about two common centres, and through a change speed gear 35 two shafts,30, 31 geared to the propellers. A group of shafts similar to the, groups E, F may replace the change speed gear 35 and couple the shafts 30, 31 together. An engine at the front of the fuselage may drive a propeller at the rear through a group of shafts similar to the group 24 of Fig. 12. Fig. 13 shows an arrangement of gears enabling intermediate shafts arranged in one plane to be brought closer together.
GB7415/40A 1940-04-24 1940-04-24 Improvements in or relating to aircraft Expired GB538046A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7415/40A GB538046A (en) 1940-04-24 1940-04-24 Improvements in or relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7415/40A GB538046A (en) 1940-04-24 1940-04-24 Improvements in or relating to aircraft

Publications (1)

Publication Number Publication Date
GB538046A true GB538046A (en) 1941-07-17

Family

ID=9832682

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7415/40A Expired GB538046A (en) 1940-04-24 1940-04-24 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB538046A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2470155A (en) * 1942-05-16 1949-05-17 Fairey Aviat Co Ltd Power plant assembly
US3115936A (en) * 1961-02-28 1963-12-31 Curtiss Wright Corp Powerplant transmission system
US3136499A (en) * 1962-11-15 1964-06-09 North American Aviation Inc Aircraft power transmission system
CN103171770A (en) * 2012-11-20 2013-06-26 无锡市万凌钢铁有限公司 Engine power transmission system of transport helicopter

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2470155A (en) * 1942-05-16 1949-05-17 Fairey Aviat Co Ltd Power plant assembly
US3115936A (en) * 1961-02-28 1963-12-31 Curtiss Wright Corp Powerplant transmission system
US3136499A (en) * 1962-11-15 1964-06-09 North American Aviation Inc Aircraft power transmission system
CN103171770A (en) * 2012-11-20 2013-06-26 无锡市万凌钢铁有限公司 Engine power transmission system of transport helicopter

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