GB406925A - Improvements in or relating to aircraft engines - Google Patents
Improvements in or relating to aircraft enginesInfo
- 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
Links
- 239000002184 metal Substances 0.000 abstract 1
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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2547551A1 (en) * | 1983-06-14 | 1984-12-21 | Gironnet Bernard | Speed reducer for aviation engine |
-
1933
- 1933-08-08 GB GB22196/33A patent/GB406925A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2547551A1 (en) * | 1983-06-14 | 1984-12-21 | Gironnet Bernard | Speed reducer for aviation engine |
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