[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

GB1332026A - Aircraft - Google Patents

Aircraft

Info

Publication number
GB1332026A
GB1332026A GB3720771A GB1332026DA GB1332026A GB 1332026 A GB1332026 A GB 1332026A GB 3720771 A GB3720771 A GB 3720771A GB 1332026D A GB1332026D A GB 1332026DA GB 1332026 A GB1332026 A GB 1332026A
Authority
GB
United Kingdom
Prior art keywords
wing
lift
jet sheet
aircraft
aug
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
GB3720771A
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.)
British Aircraft Corp Ltd
Original Assignee
British Aircraft Corp Ltd
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 British Aircraft Corp Ltd filed Critical British Aircraft Corp Ltd
Publication of GB1332026A publication Critical patent/GB1332026A/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
    • B64C9/38—Jet flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1332026 Increasing aircraft lift BRITISH AIRCRAFT CORP Ltd 2 Aug 1972 [7 Aug 1971] 37207/71 Heading F2R An aircraft has a wing system including a wing 2 of slender delta planform, means for discharging a gaseous jet sheet 11 into a region forward of the aerodynamic centre 20 so that lift is increased, and lift-increasing srufaces 19 aft of the aerodynamic centre for balancing such increases in lift. A forward part of the wing system, either a separate fore-wing 4, or a part of the delta wing, Fig. 3 (not shown), generates vortices which are shed over the wing, and it is into these vortices that the jet sheet is discharged. The jet sheet may be supplied from power plant 10 or from a separate gas generator, and is given a rearward bias by vanes 12. There may be a further jet sheet 17 discharged aft and outward of the jet sheet 11 from apertures 15.
GB3720771A 1971-08-07 1971-08-07 Aircraft Expired GB1332026A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3720771 1971-08-07

Publications (1)

Publication Number Publication Date
GB1332026A true GB1332026A (en) 1973-10-03

Family

ID=10394661

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3720771A Expired GB1332026A (en) 1971-08-07 1971-08-07 Aircraft

Country Status (2)

Country Link
FR (1) FR2148520A1 (en)
GB (1) GB1332026A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5255881A (en) * 1992-03-25 1993-10-26 Vigyan, Inc. Lift augmentation for highly swept wing aircraft
WO2011026622A3 (en) * 2009-09-02 2011-04-28 Airbus Operations Gmbh Flow body, high‑lift flap or mainplane or fin of an aircraft, as well as a structure component having a flow body such as this
WO2017041018A1 (en) * 2015-09-02 2017-03-09 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
CN110775296A (en) * 2019-11-12 2020-02-11 中国空气动力研究与发展中心计算空气动力研究所 Design method for pressure center backward movement of reusable aerospace vehicle

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2751361C2 (en) * 1977-11-17 1984-09-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München A method for controlling aircraft by controlling detached wing leading edge eddy currents

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5255881A (en) * 1992-03-25 1993-10-26 Vigyan, Inc. Lift augmentation for highly swept wing aircraft
WO2011026622A3 (en) * 2009-09-02 2011-04-28 Airbus Operations Gmbh Flow body, high‑lift flap or mainplane or fin of an aircraft, as well as a structure component having a flow body such as this
US8757556B2 (en) 2009-09-02 2014-06-24 Airbus Operations Gmbh Aerodynamic body, regulating flap or main wing or fin of an aircraft as well as a structural component with such an aerodynamic body
EP3363732A1 (en) * 2015-09-02 2018-08-22 Jetoptera, Inc. Ejector and airfoil configurations
IL257812A (en) * 2015-09-02 2018-04-30 Jetoptera Inc Fluidic propulsive system and thrust and lift generator for aerial vehicles
CN108349585A (en) * 2015-09-02 2018-07-31 杰托普特拉股份有限公司 Fluid propellant system and thrust and lifting force generator for aircraft
WO2017041018A1 (en) * 2015-09-02 2017-03-09 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
US10207812B2 (en) 2015-09-02 2019-02-19 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
EP3344537A4 (en) * 2015-09-02 2019-08-21 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
AU2016315450B2 (en) * 2015-09-02 2020-06-18 Jetoptera, Inc. Fluidic propulsive system and thrust and lift generator for aerial vehicles
US10800538B2 (en) 2015-09-02 2020-10-13 Jetoptera, Inc. Ejector and airfoil configurations
CN108349585B (en) * 2015-09-02 2021-08-10 杰托普特拉股份有限公司 Fluid propulsion system and thrust and lift generator for an aircraft
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
CN110775296A (en) * 2019-11-12 2020-02-11 中国空气动力研究与发展中心计算空气动力研究所 Design method for pressure center backward movement of reusable aerospace vehicle

Also Published As

Publication number Publication date
FR2148520A1 (en) 1973-03-23

Similar Documents

Publication Publication Date Title
GB1306169A (en)
GB1436097A (en) Method and apparatus for elimination of airfoil trailing vortices
GB1014238A (en) Improvements in ducted fan powerplants
GB1089549A (en) Aircraft
GB580995A (en) Improvements in and relating to aircraft employing jet propulsion
GB1336752A (en) Aircraft having auxiliary lift means
GB1332026A (en) Aircraft
GB1012832A (en) Improvements in or relating to vertical take off and landing aircraft
GB1185193A (en) Improvements in or relating to Flying Bodies
GB900040A (en) Exhaust nozzle with thrust deflector
GB940849A (en) Improvements in inlet for vertical take-off aircraft
GB1117266A (en) Supersonic intake for a jet propulsion engine
GB1032113A (en) Improvements in jet-propelled aeroplanes
GB788290A (en) Improvements relating to aircraft
GB1061354A (en) Braking apparatus for jet propelled aircraft
GB788643A (en) An aircraft having a detachable cabin
GB1199923A (en) Improvements in or relating to Aerodynamic Lift Producing Devices
GB886201A (en) Jet noise silencer for an aircraft
GB1074068A (en) Mounting arrangement for gas turbine jet propulsion engines
GB915947A (en) Airborne vehicles
GB856507A (en) Improvements in supersonic airfoil
GB1441516A (en) Fan jet aircraft having means for controlling rolling motion
GB890703A (en) An improved tiltable pod for jet power units on aircraft
FARBRIDGE et al. Ventral segmented nozzles(Patent Application)
GB753657A (en) Improvements in or relating to aircraft structures

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee