GB1086161A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB1086161A GB1086161A GB25075/63A GB2507563A GB1086161A GB 1086161 A GB1086161 A GB 1086161A GB 25075/63 A GB25075/63 A GB 25075/63A GB 2507563 A GB2507563 A GB 2507563A GB 1086161 A GB1086161 A GB 1086161A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jack
- jet
- engines
- aircraft
- june
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
1,086,161. Controlling Jet-propelled aircraft- HAWKER SIDDELEY AVIATION Ltd. June 24, 1964 [June 24, 1963], No. 25075/63. Heading B7G. An aircraft has two jet-propulsion engines spaced in the beam direction so that if one engine fails an asymmetric thrust is created, and gas pressure connections are taken from the two engines to opposite sides of a jack, so that the jack will be displaced in the event of one engine failure, the jack actuating means for correcting for the asymmetric thrust. As shown, air is bled from the compressors 11 of two turbo-jet engines and supplied by lines 13 to a jack 14 connected to a wheel 17 fixed to the rudder shaft 23. A by-pass line containing a pilot-operable solenoid valve 18 connects the line so that if one of the lines fails the jack may be rendered inoperative. The jack may alternatively or additionally operate angularly adjustable jet nozzles or deflector plates located inboard of the nozzles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB25075/63A GB1086161A (en) | 1963-06-24 | 1963-06-24 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB25075/63A GB1086161A (en) | 1963-06-24 | 1963-06-24 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1086161A true GB1086161A (en) | 1967-10-04 |
Family
ID=10221802
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB25075/63A Expired GB1086161A (en) | 1963-06-24 | 1963-06-24 | Improvements in or relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1086161A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008043164A2 (en) | 2006-10-10 | 2008-04-17 | EMBRAER-Empresa Brasileira de Aeronáutica S.A. | Aircraft rudder authority control system |
| US9561846B2 (en) | 2011-07-26 | 2017-02-07 | Learjet Inc. | Rudder bias gain changer |
-
1963
- 1963-06-24 GB GB25075/63A patent/GB1086161A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008043164A2 (en) | 2006-10-10 | 2008-04-17 | EMBRAER-Empresa Brasileira de Aeronáutica S.A. | Aircraft rudder authority control system |
| US9561846B2 (en) | 2011-07-26 | 2017-02-07 | Learjet Inc. | Rudder bias gain changer |
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