GB935656A - Improvements in and relating to supersonic aircraft - Google Patents
Improvements in and relating to supersonic aircraftInfo
- Publication number
- GB935656A GB935656A GB39835/60A GB3983560A GB935656A GB 935656 A GB935656 A GB 935656A GB 39835/60 A GB39835/60 A GB 39835/60A GB 3983560 A GB3983560 A GB 3983560A GB 935656 A GB935656 A GB 935656A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flaps
- operated
- nose
- control
- wing
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
935,656. Controlling aircraft. ENGLISH ELECTRIC CO. Ltd. Nov. 17, 1961 [Nov. 18, 1960], No. 39835/60. Class 4. A high-speed slender wing air craft, in which the leading edges are swept back at an angle of at least 60 degrees from a spanwise line and the aspect ratio does not exceed 2, is provided with a pail of nose flaps 10 hinged to the fuselage 1 about spanwise hinge line 11 and connected by a horse shoe bridge member 13 attached to a pair of jacks 14, the flaps normally being aligned with strakes 12 on the forward part o: the fuselage. The trailing edge o: the wing carries flaps 6, 7 inboarc and outboard of engine nacelles 8 the flaps 6, 7 being deflected downward simulataneously with upward deflection of the nose flaps 10 to balance the resulting nose-up pitching moment. They provide pitch control when operated in unison and roll control when operated differentially. Fluid pressure control apparatus, operated by separate control members, is described to enable the flaps 6 and 7 to be operated alone both in unison and differentially to control the aircraft and to simultaneously pivot flaps 10 upwards and flaps 6 and 7 downwardly during a landing approach to increase the lift of the wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB39835/60A GB935656A (en) | 1960-11-18 | 1960-11-18 | Improvements in and relating to supersonic aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB39835/60A GB935656A (en) | 1960-11-18 | 1960-11-18 | Improvements in and relating to supersonic aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB935656A true GB935656A (en) | 1963-09-04 |
Family
ID=10411762
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB39835/60A Expired GB935656A (en) | 1960-11-18 | 1960-11-18 | Improvements in and relating to supersonic aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB935656A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3478989A (en) * | 1966-11-14 | 1969-11-18 | Hamburger Flugzeugbau Gmbh | Supersonic aircraft |
| US3653611A (en) * | 1970-03-24 | 1972-04-04 | Mason Trupp | Slotted delta wing aircraft |
| CN116985994A (en) * | 2023-09-21 | 2023-11-03 | 中国空气动力研究与发展中心计算空气动力研究所 | Invisible aircraft |
-
1960
- 1960-11-18 GB GB39835/60A patent/GB935656A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3478989A (en) * | 1966-11-14 | 1969-11-18 | Hamburger Flugzeugbau Gmbh | Supersonic aircraft |
| US3653611A (en) * | 1970-03-24 | 1972-04-04 | Mason Trupp | Slotted delta wing aircraft |
| CN116985994A (en) * | 2023-09-21 | 2023-11-03 | 中国空气动力研究与发展中心计算空气动力研究所 | Invisible aircraft |
| CN116985994B (en) * | 2023-09-21 | 2023-11-28 | 中国空气动力研究与发展中心计算空气动力研究所 | Invisible aircraft |
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