GB283532A - Improvements in means for regulating the fuel supply to internal combustion aircraft engines - Google Patents
Improvements in means for regulating the fuel supply to internal combustion aircraft enginesInfo
- Publication number
- GB283532A GB283532A GB1129/28A GB112928A GB283532A GB 283532 A GB283532 A GB 283532A GB 1129/28 A GB1129/28 A GB 1129/28A GB 112928 A GB112928 A GB 112928A GB 283532 A GB283532 A GB 283532A
- Authority
- GB
- United Kingdom
- Prior art keywords
- levers
- engines
- control
- mixture
- controlled
- 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 title abstract 2
- 230000001105 regulatory effect Effects 0.000 title abstract 2
- 239000000203 mixture Substances 0.000 abstract 3
- 238000004873 anchoring Methods 0.000 abstract 1
- 230000000994 depressogenic effect Effects 0.000 abstract 1
- 239000002783 friction material Substances 0.000 abstract 1
- 210000001331 nose Anatomy 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
-
- 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
- B64D31/04—Initiating means actuated personally
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
283,532. Rohrbach Metall-Flugzeugbau Ges. Jan. 12, 1927, [Convention date]. Propelling. - A device for regulating the fuel supply to the internal-combustion engines of aircraft comprises two levers 7 connected by bevel gear 6 to a hand-lever 1<1> which can swing about the axis of the two levers 7 and can also be turned about its own axis and two other levers 11' mounted coaxially with the first two and provided with separate hand-levers 10' projecting through slots in a common housing. When used with two engines the levers 7 are connected to the two throttles which can be moved together or differentially and the two outer levers control the mixture at high altitudes. Plates 16, which may have interposed friction material, are placed between the levers 7, 11' and anchored to bolts 14 which secure the two halves of the casing together. Springs 17 press the levers and plates 16 into contact. When used with three or four engines, the levers 10' are provided with toothed quadrants 20 adapted to be engaged by noses 19 when depressed against a spring 21 by a rod 18 provided with a push button so that all four levers can be moved together to control the throttles. This clutching device is omitted in the twin engine control. For use with three engines, the two outer levers are connected to the throttle of the central engine which can therefore be controlled by either of the levers 10'. In this case the mixture is controlled by a separate similar device but without the bevel gear 6. The mixture for four engines is controlled by a separate device in a similar casing but comprising four coaxial levers separated bv anchoring plates and provided with control handles.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE283532X | 1927-01-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB283532A true GB283532A (en) | 1928-08-09 |
Family
ID=6046844
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1129/28A Expired GB283532A (en) | 1927-01-12 | 1928-01-12 | Improvements in means for regulating the fuel supply to internal combustion aircraft engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB283532A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1958870A1 (en) * | 2007-02-19 | 2008-08-20 | Ratier-Figeac | Manual control of aircraft flight |
| FR2956756A1 (en) * | 2010-02-23 | 2011-08-26 | Airbus Operations Sas | PERFECTED RESISTIVE TORQUE GENERATING DEVICE |
| EP3467612B1 (en) * | 2017-10-09 | 2020-09-16 | Lord Solutions France | Device for generating force sensation, by friction, for a flight control system of an aircraft |
-
1928
- 1928-01-12 GB GB1129/28A patent/GB283532A/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1958870A1 (en) * | 2007-02-19 | 2008-08-20 | Ratier-Figeac | Manual control of aircraft flight |
| FR2912724A1 (en) * | 2007-02-19 | 2008-08-22 | Ratier Figeac Soc Par Actions | MANUAL AIRCRAFT FLIGHT CONTROL |
| FR2956756A1 (en) * | 2010-02-23 | 2011-08-26 | Airbus Operations Sas | PERFECTED RESISTIVE TORQUE GENERATING DEVICE |
| WO2011104476A1 (en) * | 2010-02-23 | 2011-09-01 | Airbus Operations S.A.S | Improved device for generating resistive torque |
| US8985521B2 (en) | 2010-02-23 | 2015-03-24 | Airbus Operations Sas | Device for generating resistive torque |
| EP3467612B1 (en) * | 2017-10-09 | 2020-09-16 | Lord Solutions France | Device for generating force sensation, by friction, for a flight control system of an aircraft |
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