GB1090351A - Aircraft power plant - Google Patents
Aircraft power plantInfo
- Publication number
- GB1090351A GB1090351A GB7796/66A GB779666A GB1090351A GB 1090351 A GB1090351 A GB 1090351A GB 7796/66 A GB7796/66 A GB 7796/66A GB 779666 A GB779666 A GB 779666A GB 1090351 A GB1090351 A GB 1090351A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- flap
- duct
- pass
- ejector
- 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
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
1,090,351. Jet propelled aircraft. ROLLS ROYCE Ltd. Feb. 22, 1966, No. 7796/66. Heading B7G. [Also in Division F2] 'An aircraft power plant supplies pressurized gas to at least one ejector nozzle upstream of a flap so that ambient air is entrained and caused to flow over the flap, the proportions flowing over the upper and lower surfaces being controlled by a valve. As described, a by-pass gas turbine engine is mounted under an aircraft wing, and by-pass air from the engine is conveyed by a duct 20 to ejector nozzles 24, 25 separated by a hollow splitter 21. Ambient air passes to the ejector nozzles through ducts 27, 31 from a duct 32 opening on to the lower surface of the wing 16, and through the interior of the splitter 21 from its ends. The ejectors discharge over the upper and lower surfaces of a hinged flap 11. The duct 32 is closed at the lower surface of the wing by a spring-loaded door 33 which opens automatically when suction is applied by the ejectors. The lower ejector nozzle has a greater flow rate than the upper, but this may be varied by a flap 42. The engine exhaust gases pass through a nozzle 15, and more by-pass air is supplied to flow over the upper surface of the wing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7796/66A GB1090351A (en) | 1966-02-22 | 1966-02-22 | Aircraft power plant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7796/66A GB1090351A (en) | 1966-02-22 | 1966-02-22 | Aircraft power plant |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1090351A true GB1090351A (en) | 1967-11-08 |
Family
ID=9839912
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7796/66A Expired GB1090351A (en) | 1966-02-22 | 1966-02-22 | Aircraft power plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1090351A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4143086A4 (en) * | 2020-04-27 | 2024-05-15 | Jetoptera, Inc. | Vertical take off and landing aircraft with fluidic propulsion system |
-
1966
- 1966-02-22 GB GB7796/66A patent/GB1090351A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4143086A4 (en) * | 2020-04-27 | 2024-05-15 | Jetoptera, Inc. | Vertical take off and landing aircraft with fluidic propulsion system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3051413A (en) | Vtol aircraft | |
GB852829A (en) | Improvements in or relating to gas-turbine jet propulsion engines | |
GB757496A (en) | Improvements in arrangement for controlling the air-intake orifices of jet propulsion units | |
GB726290A (en) | Improvements in or relating to variable area nozzles for jet propulsion power plant | |
US2914941A (en) | High-speed wind tunnels | |
GB955518A (en) | Thrust-reversal in turbo-jet devices | |
GB1028041A (en) | A gas ejector device | |
GB1166396A (en) | Improvements in Power Plant with Thrust Reverser. | |
GB861480A (en) | Improvements in aircraft | |
GB1090351A (en) | Aircraft power plant | |
GB1027415A (en) | Jet propulsion engine | |
GB955014A (en) | Turbine jet propulsion engine | |
GB905534A (en) | Improvements in or relating to gas turbine engines | |
GB945862A (en) | Gas turbine by-pass engines | |
GB894800A (en) | Jet propulsion engine exhaust noise suppressor | |
GB1415509A (en) | Ducted fan gas turbine jet propulsion engines | |
GB756185A (en) | Improvements in or relating to apparatus for effecting stable combustion in a high velocity gas stream | |
GB871470A (en) | Improvements relating to aircraft incorporating vertical thrust generators | |
GB1056172A (en) | Improvements in or relating to aircraft | |
GB1010100A (en) | Improvements in or relating to vtol or stol aircraft | |
GB733727A (en) | Improvements in arrangements for deflecting fluid jets | |
GB899239A (en) | Improvements in gaseous flow diverting mechanism for aircraft | |
GB921398A (en) | Aircraft | |
GB756319A (en) | Improvements in aircraft | |
GB1020018A (en) | Jet nozzle system for a by-pass type gas turbine jet engine |