GB1487077A - Aircraft wing assemblies - Google Patents
Aircraft wing assembliesInfo
- Publication number
- GB1487077A GB1487077A GB46863/74A GB4686374A GB1487077A GB 1487077 A GB1487077 A GB 1487077A GB 46863/74 A GB46863/74 A GB 46863/74A GB 4686374 A GB4686374 A GB 4686374A GB 1487077 A GB1487077 A GB 1487077A
- Authority
- GB
- United Kingdom
- Prior art keywords
- trailing edge
- flap
- edge portion
- efflux
- 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
- 230000000712 assembly Effects 0.000 title 1
- 238000000429 assembly Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
1487077 Aircraft wings DEFENCE SECRETARY OF STATE FOR 20 Oct 1975 [29 Oct 1974] 46863/74 Heading F2R [Also in Division B7] An aircraft wing 2 which receives the efflux of a jet engine 1 along its upper surface, has a hinged trailing edge portion 2a and retractable flap 4. The trailing edge portion is movable between a lower position in which it abuts the flap 4 and forms with it a continuous curved surface, and an upper cruise position (shown) in which the efflux is not directed over the flap 4. In its lower position the trailing edge portion serves to direct the efflux over the flap 4 and an additional flap 5 to increase lift. The trailing edge portion 2a may also be positioned upwardly so as to act as a spoiler to reduce lift. The trailing edge portions 2a of the port and starboard wings may be linked so as to act in the opposite sense and thus control roll of the aircraft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB46863/74A GB1487077A (en) | 1975-10-20 | 1975-10-20 | Aircraft wing assemblies |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB46863/74A GB1487077A (en) | 1975-10-20 | 1975-10-20 | Aircraft wing assemblies |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1487077A true GB1487077A (en) | 1977-09-28 |
Family
ID=10442875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB46863/74A Expired GB1487077A (en) | 1975-10-20 | 1975-10-20 | Aircraft wing assemblies |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1487077A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0078245A1 (en) * | 1981-10-15 | 1983-05-04 | AERITALIA - Società Aerospaziale Italiana - p.A. | Aircraft with jet propulsion |
WO2010119280A1 (en) | 2009-04-14 | 2010-10-21 | Moog Wolverhampton Limited | High lift devices for aircraft |
WO2015094003A1 (en) * | 2013-12-16 | 2015-06-25 | Дмитрий Георгиевич КОШКАРЕВ | Combination aircraft wing |
-
1975
- 1975-10-20 GB GB46863/74A patent/GB1487077A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0078245A1 (en) * | 1981-10-15 | 1983-05-04 | AERITALIA - Società Aerospaziale Italiana - p.A. | Aircraft with jet propulsion |
WO2010119280A1 (en) | 2009-04-14 | 2010-10-21 | Moog Wolverhampton Limited | High lift devices for aircraft |
WO2015094003A1 (en) * | 2013-12-16 | 2015-06-25 | Дмитрий Георгиевич КОШКАРЕВ | Combination aircraft wing |
RU2626773C1 (en) * | 2013-12-16 | 2017-08-01 | Чепик Александр Ануфриевич | Combined aircraft wing |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |