GB406925A - Improvements in or relating to aircraft engines - Google Patents

Improvements in or relating to aircraft engines

Info

Publication number
GB406925A
GB406925A GB22196/33A GB2219633A GB406925A GB 406925 A GB406925 A GB 406925A GB 22196/33 A GB22196/33 A GB 22196/33A GB 2219633 A GB2219633 A GB 2219633A GB 406925 A GB406925 A GB 406925A
Authority
GB
United Kingdom
Prior art keywords
shaft
thrust bearing
lane
nut
relating
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
GB22196/33A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co Ltd
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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB22196/33A priority Critical patent/GB406925A/en
Publication of GB406925A publication Critical patent/GB406925A/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

406,925. Driving aircraft propellers. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, Middlesex, and FORSYTH, A. G., Venlaw, Burdon Lane, Cheam, Surrey. Aug. 8, 1933, No. 22196. [Class 4.] An airscrew hub a is formed integrally with a shaft b which is telescoped in and connected to a shaft e constituting an independent unit carrying the main reduction gear wheel q, and thrust bearing u with locking nut, the shaft b being removable without dismantling the parts of said unit. The engine crank case is split in a vertical transverse plane to enable the gearing to be inserted from the front. The shaft b is splined to the shaft e and a coned portion c at its front end is drawn against a gun metal washer by a nut k at the rear end of the shaft. The shaft e runs in bearings f, g in addition to the ball-thrust bearing u.
GB22196/33A 1933-08-08 1933-08-08 Improvements in or relating to aircraft engines Expired GB406925A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB22196/33A GB406925A (en) 1933-08-08 1933-08-08 Improvements in or relating to aircraft engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22196/33A GB406925A (en) 1933-08-08 1933-08-08 Improvements in or relating to aircraft engines

Publications (1)

Publication Number Publication Date
GB406925A true GB406925A (en) 1934-03-08

Family

ID=10175497

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22196/33A Expired GB406925A (en) 1933-08-08 1933-08-08 Improvements in or relating to aircraft engines

Country Status (1)

Country Link
GB (1) GB406925A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2547551A1 (en) * 1983-06-14 1984-12-21 Gironnet Bernard Speed reducer for aviation engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2547551A1 (en) * 1983-06-14 1984-12-21 Gironnet Bernard Speed reducer for aviation engine

Similar Documents

Publication Publication Date Title
GB406925A (en) Improvements in or relating to aircraft engines
GB469329A (en) Improvements in and relating to combined motor driving and steering units for boats
GB443750A (en) Improvements in or relating to variable pitch propellers
GB521218A (en) Improvements in helicopters
GB459084A (en) Propellor shafts for motor-vehicles
GB505346A (en) Device for mounting two aeroplane propellers coaxially and with reverse directions of rotation
GB416139A (en) Improvements in gearing for propellers
DE373622C (en) Propeller drive for motor vehicles with car body that tapers towards the rear on all sides
GB520293A (en) Device for mounting two aeroplane propellers coaxially and with reverse directions of rotation, comprising an offset speedreducing gear
GB543851A (en) Improved airscrew-apparatus for the propulsion of aircraft
GB332642A (en) Improvements in or relating to the propulsion of aircraft
GB397135A (en) An improved method of building up crank shafts and securing propellers and the like to shafts
GB214305A (en) A combination helicopter aeroplane
GB526460A (en) Improvements in or relating to the power plants of aircraft
GB536904A (en) Aeroplanes
GB237760A (en) Improvements in and relating to airplanes
US1780561A (en) Aeroplane
GB238742A (en) Driving gear for screw and like propellers of aircraft
GB436707A (en) Improvements in and relating to marine propeller shafts
GB425649A (en) Driving the propellers of aircraft
GB472318A (en) Improvements in or relating to aircraft propulsion
GB285636A (en) Improvements in the drive transmission of internal combustion engines for aircraft
GB534467A (en) Improvements in and relating to variable pitch propellers for aircraft
GB437631A (en) Improvements in or relating to screw propellers
GB605638A (en) Aircraft