GB501622A - Improvements relating to engine controls particularly for aircraft engines - Google Patents
Improvements relating to engine controls particularly for aircraft enginesInfo
- Publication number
- GB501622A GB501622A GB3224637A GB3224637A GB501622A GB 501622 A GB501622 A GB 501622A GB 3224637 A GB3224637 A GB 3224637A GB 3224637 A GB3224637 A GB 3224637A GB 501622 A GB501622 A GB 501622A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- throttle
- moved
- detent
- roller
- 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
-
- 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
- B64D31/00—Power plant control; Arrangement thereof
- B64D31/02—Initiating means
- B64D31/04—Initiating means actuated personally
Abstract
501,622. Regulating. EXACTOR CONTROL CO., Ltd., and DWERRYHOUSE, P. J. Nov. 23, 1937, No. 32246. [Class 7 (vi)] [Also in Group XXIV] In an arrangement of engine throttle and mixture control levers, the mixture control lever. is urged by a spring to the " rich " position; but is retained by a detent in the " weak " position after it has been moved' there by the pilot, this detent being interconnected with the throttle lever so as to be operative only when the throttle lever is within a certain range of movement, and to be released whenever the throttle lever is moved beyond that range. The Figure shows the throttle control lever T and the mixture control-lever M mounted side-by-side on the same pivot 1, the lever T carrying a roller 10 engaging a cam lever 4 pivoted at 3 and pressed upwards by a spring 6, so that a detent on the cam lever engages a projection 9 on the lever M. When the lever T is in the cruising position C<1>-C<2>, the roller 10 rides in a recess 7 in the cam lever 4 and the lever M is held by the catch 8, 9 in the " weak " position shown ; but if the lever T is moved to the closed position A or full-open position B, the roller 10 depresses the cam lever 4 so as to disengage the catch 8, 9 and allow the lever M to be moved by a spring to the " rich " position D. In a modification, a pair of throttle levers are shown in connection with a single mixture lever. The controls may be of the hydraulic type described in Specification 419,310, [Group XXIX].
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3224637A GB501622A (en) | 1937-11-23 | 1937-11-23 | Improvements relating to engine controls particularly for aircraft engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3224637A GB501622A (en) | 1937-11-23 | 1937-11-23 | Improvements relating to engine controls particularly for aircraft engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB501622A true GB501622A (en) | 1939-03-02 |
Family
ID=10335597
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3224637A Expired GB501622A (en) | 1937-11-23 | 1937-11-23 | Improvements relating to engine controls particularly for aircraft engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB501622A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3508427A1 (en) * | 2018-01-09 | 2019-07-10 | General Electric Company | Single lever control system for engines with multiple control modes |
| CN114136628A (en) * | 2021-10-20 | 2022-03-04 | 中国航发四川燃气涡轮研究院 | Experimental angularly adjustable throttle lever stop device of aeroengine |
-
1937
- 1937-11-23 GB GB3224637A patent/GB501622A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3508427A1 (en) * | 2018-01-09 | 2019-07-10 | General Electric Company | Single lever control system for engines with multiple control modes |
| US11124309B2 (en) | 2018-01-09 | 2021-09-21 | General Electric Company | Single lever control system for engines with multiple control modes |
| EP4079640A1 (en) * | 2018-01-09 | 2022-10-26 | General Electric Company | Single lever control system for engines with multiple control modes |
| CN114136628A (en) * | 2021-10-20 | 2022-03-04 | 中国航发四川燃气涡轮研究院 | Experimental angularly adjustable throttle lever stop device of aeroengine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB501622A (en) | Improvements relating to engine controls particularly for aircraft engines | |
| US1998362A (en) | Controlling supercharged or other high compression ratio aircraft engine | |
| GB731735A (en) | Control means for internal combustion turbine engines for aircraft | |
| US2388079A (en) | Control lever | |
| GB539020A (en) | Control mechanism for engines using producer gas and petrol | |
| JPS55139924A (en) | Intake device for engine | |
| GB447324A (en) | Improvements in controls for superchargers on aircraft | |
| GB544073A (en) | Improvements in and relating to internal combustion engines using either liquid fuelor gas | |
| GB1090084A (en) | Improvements in or relating to throttle linkages for vehicle engines | |
| GB1224142A (en) | Linkages | |
| GB526764A (en) | Improvements in or relating to throttle control mechanism for aircraft engines | |
| GB597930A (en) | Improved control mechanism for supercharged aircraft engines | |
| GB453915A (en) | Improvements in or relating to supercharged internal-combustion engines for aircraft | |
| GB1183954A (en) | Improvements in or relating to Internal Combustion Engines | |
| GB419472A (en) | Improvements in and relating to means for controlling super-charged, or other high compression ratio internal combustion aircraft engines | |
| GB395494A (en) | Improved means for controlling supercharged internal combustion engines for aircraft | |
| GB386948A (en) | Improvements in or relating to controlling devices for internal combustion engines | |
| GB390710A (en) | Improvements in carburetters | |
| GB529704A (en) | Improvements in or relating to the regulation of the output of internal combustion engines | |
| GB450587A (en) | Improvements in or relating to supercharged internal-combustion engines for aircraft | |
| GB369459A (en) | Improvements in and relating to controlling means for internal combustion engines | |
| GB511794A (en) | Improvements in or relating to linkage mechanisms suitable for the throttle control of aero engines | |
| GB363081A (en) | Improvements in or relating to means for regulating diesel engines | |
| GB473467A (en) | Improvements relating to carburettors for internal combustion engines | |
| GB587822A (en) | Improvements in manual controls for twin-engined aircraft |