GB731735A - Control means for internal combustion turbine engines for aircraft - Google Patents
Control means for internal combustion turbine engines for aircraftInfo
- Publication number
- GB731735A GB731735A GB281553A GB281553A GB731735A GB 731735 A GB731735 A GB 731735A GB 281553 A GB281553 A GB 281553A GB 281553 A GB281553 A GB 281553A GB 731735 A GB731735 A GB 731735A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- quadrant
- idling
- moved
- aircraft
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 2
- 239000000446 fuel Substances 0.000 abstract 2
- 238000006243 chemical reaction Methods 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
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- B64D31/02—Initiating means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Abstract
731,735. Aircraft throttle controls. ROLLS-ROYCE, Ltd. Jan. 29, 1954 [Jan. 30, 1953], No. 2815/53. Class 4. A control for a fuel control valve of an internal combustion turbine engine of an aircraft comprises a control lever 10 which can be moved in the sense of effecting closure of the fuel flow control valve beyond a setting suitable for idling at ground level against the reaction of resilient means 14 which return the lever to the idling position when the pressure on the control lever is removed. As described the lever 10 moves in a quadrant 11, ungated, Fig. 2 (not shown) or gated, Fig. 3. The low power end of the quadrant bears a bracket 12 supporting a piston 13 biased by a spring 14. , In normal flight, the lever moves in the right hand portion of the quadrant between maximum power setting at the extreme right, and flight idling conditions 18 at the gate 15. The lever may be moved on its. spindle 17 against a spring 16 through the gate to a position 19 abutting the piston head, which is the ground idling position. For relighting the turbine at altitude, the lever is moved to the extreme left 20 against spring 14.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB281553A GB731735A (en) | 1953-01-30 | 1953-01-30 | Control means for internal combustion turbine engines for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB281553A GB731735A (en) | 1953-01-30 | 1953-01-30 | Control means for internal combustion turbine engines for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB731735A true GB731735A (en) | 1955-06-15 |
Family
ID=9746450
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB281553A Expired GB731735A (en) | 1953-01-30 | 1953-01-30 | Control means for internal combustion turbine engines for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB731735A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2946016A1 (en) * | 2009-05-29 | 2010-12-03 | Airbus France | SYSTEM FOR CONTROLLING AT LEAST ONE AIRCRAFT AND AIRCRAFT ENGINE COMPRISING SUCH A CONTROL SYSTEM |
| US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
| US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
| US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
| US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
| US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
| US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
| CN111846250A (en) * | 2020-07-23 | 2020-10-30 | 中国商用飞机有限责任公司 | Method and system for controlling speed and attitude modes of an aircraft |
-
1953
- 1953-01-30 GB GB281553A patent/GB731735A/en not_active Expired
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
| US8708083B2 (en) | 2009-05-12 | 2014-04-29 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
| FR2946016A1 (en) * | 2009-05-29 | 2010-12-03 | Airbus France | SYSTEM FOR CONTROLLING AT LEAST ONE AIRCRAFT AND AIRCRAFT ENGINE COMPRISING SUCH A CONTROL SYSTEM |
| US8660770B2 (en) | 2009-05-29 | 2014-02-25 | Airbus Operations (Sas) | System for controlling at least one aircraft engine and an aircraft comprising such a control system |
| US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
| US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
| US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
| US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
| US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
| CN111846250A (en) * | 2020-07-23 | 2020-10-30 | 中国商用飞机有限责任公司 | Method and system for controlling speed and attitude modes of an aircraft |
| CN111846250B (en) * | 2020-07-23 | 2022-02-22 | 中国商用飞机有限责任公司 | Method and system for controlling speed and attitude modes of an aircraft |
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