GB1487077A - Aircraft wing assemblies - Google Patents

Aircraft wing assemblies

Info

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
Application number
GB46863/74A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB46863/74A priority Critical patent/GB1487077A/en
Publication of GB1487077A publication Critical patent/GB1487077A/en
Expired legal-status Critical Current

Links

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.
GB46863/74A 1975-10-20 1975-10-20 Aircraft wing assemblies Expired GB1487077A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB1083267A (en) Flap systems for aircraft
GB1284108A (en) Improvements in or relating to aircraft wings
US3142457A (en) Stall pattern lift regulator for airplanes
GB1529886A (en) Aerofoil tip-vortex control
GB1212705A (en) An aircraft
FR2076030B1 (en)
GB1079296A (en) A system and method for generating lift of aircraft
GB1258202A (en)
GB1512645A (en) Aircraft
GB1252759A (en)
GB945078A (en) Improvements in or relating to wing-fan doors of vertical take-off aircraft
GB1470356A (en) Towed airborne target
GB1487077A (en) Aircraft wing assemblies
GB1381646A (en) Aircraft with short take-off and landing characteristics
GB1448245A (en) Combination jet engine clam-shell thrust reverser and variable nozzle area ramp
GB1167911A (en) Pod for a Gas Turbine Engine.
FR2310258A1 (en) Inflated wing for ultra light aircraft - maintained shape by internal pressure from relative airspeed or propeller slipstream
GB1496519A (en) Aircraft wings
GB1151431A (en) Improvements in or relating to Aircraft Wings
GB1404153A (en) Aircraft wings
GB1019061A (en) Improvements relating to control of fluid flow past bodies and to reduction of drag of such bodies
GB1307990A (en) Variable-geometry aircraft
GB1135946A (en) Improvements in aircraft
GB1508389A (en) Aerodynamic lift enhancing apparatus
GB1365305A (en) Aircraft

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee