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GB756319A - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB756319A
GB756319A GB17981/49A GB1798149A GB756319A GB 756319 A GB756319 A GB 756319A GB 17981/49 A GB17981/49 A GB 17981/49A GB 1798149 A GB1798149 A GB 1798149A GB 756319 A GB756319 A GB 756319A
Authority
GB
United Kingdom
Prior art keywords
jet
turbine
aircraft
stalker
nacelle
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
GB17981/49A
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 GB17981/49A priority Critical patent/GB756319A/en
Publication of GB756319A publication Critical patent/GB756319A/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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/06Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0226Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Tires In General (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

756,319. Jet propulsion plant. STALKER, E. A. July 7, 1949, No. 17981/49. Class 110(3) [Also in Group XXXIII] Boundary layer air from the wings and nacelle of a jet-propelled aircraft is fed through passages 50, 51 and a circumferential opening 90 to a ducted fan 26 driven by a gas-turbine 24 and discharged through an annular nozzle 27 surrounding the jet pipe 25 of the turbine 24.
GB17981/49A 1949-07-07 1949-07-07 Improvements in aircraft Expired GB756319A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB17981/49A GB756319A (en) 1949-07-07 1949-07-07 Improvements in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB17981/49A GB756319A (en) 1949-07-07 1949-07-07 Improvements in aircraft

Publications (1)

Publication Number Publication Date
GB756319A true GB756319A (en) 1956-09-05

Family

ID=10104575

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17981/49A Expired GB756319A (en) 1949-07-07 1949-07-07 Improvements in aircraft

Country Status (1)

Country Link
GB (1) GB756319A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2837782A1 (en) * 2002-04-02 2003-10-03 Gilles Vaton TRIMARAN TYPE HIGH SPEED SHIP HULL
WO2008017567A1 (en) * 2006-08-11 2008-02-14 Team Smartfish Gmbh Air inlet for a jet engine
CN117818871A (en) * 2024-03-04 2024-04-05 中国空气动力研究与发展中心高速空气动力研究所 Application method of passive mixed laminar flow nacelle

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2837782A1 (en) * 2002-04-02 2003-10-03 Gilles Vaton TRIMARAN TYPE HIGH SPEED SHIP HULL
WO2003082662A1 (en) * 2002-04-02 2003-10-09 Trading And Investment International Seaworld High-speed marine hull of the trimaran type
WO2008017567A1 (en) * 2006-08-11 2008-02-14 Team Smartfish Gmbh Air inlet for a jet engine
CN117818871A (en) * 2024-03-04 2024-04-05 中国空气动力研究与发展中心高速空气动力研究所 Application method of passive mixed laminar flow nacelle
CN117818871B (en) * 2024-03-04 2024-05-17 中国空气动力研究与发展中心高速空气动力研究所 Application method of passive mixed laminar flow nacelle

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