GB171382A - Reducing gear for aviation engines - Google Patents
Reducing gear for aviation enginesInfo
- Publication number
- GB171382A GB171382A GB29637/21A GB2963721A GB171382A GB 171382 A GB171382 A GB 171382A GB 29637/21 A GB29637/21 A GB 29637/21A GB 2963721 A GB2963721 A GB 2963721A GB 171382 A GB171382 A GB 171382A
- Authority
- GB
- United Kingdom
- Prior art keywords
- teeth
- sleeve
- shaft
- gear
- cam
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
- F02B61/04—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gear Transmission (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
171,382. Barbarou M. J. B. Nov. 13, 1920, [Convention date]. Toothed gearing.-In an aircraft having its propeller driven from the cam-shaft of the engine, the gear wheel c<1> on the cam-shaft is driven from a pinion b on the crank-shaft through two intermediate gear-wheels D, E the centres of which are adjustable towards or away from the adjacent wheels. Each wheel D, E is mounted by means of roller bearings G, H on a sleeve A which is eccentrically mounted on a hollow spindle B. The end of the sleeve A has teeth C adapted to be engaged by corresponding teeth on a plate K, which is secured to the gear casing by screws F after adjustment of the sleeve. The roller bearings H are arranged outside the planes of the edges of the teeth to allow an adequate depth of metal beneath the teeth. A ball thrust-bearing I prevents endways movement of the gear wheel. The Specification as open to inspection under Sect. 91 (3) (a) mentions Specification 157,075, [Class 80 (ii), Gearing, Variable-speed &c.]. This reference does not appear in the Speclfication as accepted.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR171382X | 1920-11-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB171382A true GB171382A (en) | 1923-02-01 |
Family
ID=8877379
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB29637/21A Expired GB171382A (en) | 1920-11-13 | 1921-11-07 | Reducing gear for aviation engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB171382A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7828935B2 (en) | 2003-04-07 | 2010-11-09 | International Paper Company | Papers for liquid electrophotographic printing and method for making same |
| US20180202513A1 (en) * | 2015-07-22 | 2018-07-19 | Francis A. Nardella | Internal combustion piston engine for aviation |
-
1921
- 1921-11-07 GB GB29637/21A patent/GB171382A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7828935B2 (en) | 2003-04-07 | 2010-11-09 | International Paper Company | Papers for liquid electrophotographic printing and method for making same |
| US20180202513A1 (en) * | 2015-07-22 | 2018-07-19 | Francis A. Nardella | Internal combustion piston engine for aviation |
| US10550911B2 (en) * | 2015-07-22 | 2020-02-04 | Francis A Nardella | Internal combustion piston engine for aviation |
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