GB568667A - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
GB568667A
GB568667A GB17352/42A GB1735242A GB568667A GB 568667 A GB568667 A GB 568667A GB 17352/42 A GB17352/42 A GB 17352/42A GB 1735242 A GB1735242 A GB 1735242A GB 568667 A GB568667 A GB 568667A
Authority
GB
United Kingdom
Prior art keywords
conduits
aircraft
wings
upper surfaces
air sucked
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
GB17352/42A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB17352/42A priority Critical patent/GB568667A/en
Publication of GB568667A publication Critical patent/GB568667A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/01Boundary layer ingestion [BLI] propulsion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/06Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/04Boundary layer controls by actively generating fluid flow
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Abstract

568,667. Reducing surface friction on aircraft. UMPLEBY, F. Dec. 7, 1942, No. 17352. [Class 4] Air sucked through openings in the upper surfaces of an aircraft fuselage and wings in order to control the boundary layer is fed to the aero-engine or to a jet propulsion device, the conduits being so arranged that a forward reaction due to the airflow around bends in the conduits is obtained. As shown, air sucked through slots 7, 8 in the upper surfaces of the wings and fuselage flows through conduits 6 having rearward bends 9 to internal-combustion, turbo-blower, jet propulsion units 1, 2, 3. The units 1, 2 may drive propellers 10. The conduits 6 may form part of the wing structure.
GB17352/42A 1942-12-07 1942-12-07 Improvements in and relating to aircraft Expired GB568667A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB17352/42A GB568667A (en) 1942-12-07 1942-12-07 Improvements in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB17352/42A GB568667A (en) 1942-12-07 1942-12-07 Improvements in and relating to aircraft

Publications (1)

Publication Number Publication Date
GB568667A true GB568667A (en) 1945-04-16

Family

ID=10093669

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17352/42A Expired GB568667A (en) 1942-12-07 1942-12-07 Improvements in and relating to aircraft

Country Status (1)

Country Link
GB (1) GB568667A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2504421A (en) * 1946-04-25 1950-04-18 Lockheed Aircraft Corp Aircraft engine and fuselage arrangement
US2557522A (en) * 1946-05-28 1951-06-19 Sncase Aerodynes equipped with reaction jet propulsion means
US2604277A (en) * 1945-03-31 1952-07-22 Rateau Soc Jet propulsion and boundary layer control system for aircraft
US2657881A (en) * 1947-04-17 1953-11-03 Douglas Aubrey Jet propulsion and boundary layer control means
US2745611A (en) * 1946-05-29 1956-05-15 Rateau Soc Jet propulsion and boundary layer control system for aircraft
US2982495A (en) * 1951-08-16 1961-05-02 Rolls Royce Aircraft with tiltable lift engines
WO2006012809A1 (en) * 2004-07-31 2006-02-09 Birgit Bergmann Aerodynamics optimised by combined air intake for an engine and a boundary suctioning layer

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2604277A (en) * 1945-03-31 1952-07-22 Rateau Soc Jet propulsion and boundary layer control system for aircraft
US2504421A (en) * 1946-04-25 1950-04-18 Lockheed Aircraft Corp Aircraft engine and fuselage arrangement
US2557522A (en) * 1946-05-28 1951-06-19 Sncase Aerodynes equipped with reaction jet propulsion means
US2745611A (en) * 1946-05-29 1956-05-15 Rateau Soc Jet propulsion and boundary layer control system for aircraft
US2657881A (en) * 1947-04-17 1953-11-03 Douglas Aubrey Jet propulsion and boundary layer control means
US2982495A (en) * 1951-08-16 1961-05-02 Rolls Royce Aircraft with tiltable lift engines
WO2006012809A1 (en) * 2004-07-31 2006-02-09 Birgit Bergmann Aerodynamics optimised by combined air intake for an engine and a boundary suctioning layer

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