FR2148520A1 - - Google Patents

Info

Publication number
FR2148520A1
FR2148520A1 FR7228467A FR7228467A FR2148520A1 FR 2148520 A1 FR2148520 A1 FR 2148520A1 FR 7228467 A FR7228467 A FR 7228467A FR 7228467 A FR7228467 A FR 7228467A FR 2148520 A1 FR2148520 A1 FR 2148520A1
Authority
FR
France
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.)
Withdrawn
Application number
FR7228467A
Other languages
English (en)
French (fr)
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 FR2148520A1 publication Critical patent/FR2148520A1/fr
Withdrawn legal-status Critical Current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)
FR7228467A 1971-08-07 1972-08-07 Withdrawn FR2148520A1 (cs)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
FR2148520A1 true FR2148520A1 (cs) 1973-03-23

Family

ID=10394661

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7228467A Withdrawn FR2148520A1 (cs) 1971-08-07 1972-08-07

Country Status (2)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2409193A1 (fr) * 1977-11-17 1979-06-15 Messerschmitt Boelkow Blohm Procede de commande des avions par controle des courants tourbillonnaires qui se degagent des bords d'attaque des ailes

Families Citing this family (7)

* 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
DE102009039769A1 (de) * 2009-09-02 2011-03-17 Airbus Operations Gmbh Strömungskörper, Stellklappe oder Hauptflügel oder Flosse eines Flugzeugs sowie Strukturbauteil mit einem solchen Strömungskörper
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
JP6930743B2 (ja) * 2015-09-02 2021-09-01 ジェトプテラ、インコーポレイテッド エジェクタ及びエアフォイル形状
CN110775296A (zh) * 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 一种可重复使用空天飞行器压心后移的设计方法
CN119872868A (zh) * 2025-01-17 2025-04-25 清华大学 一种提高大攻角状态下飞翼舵效的翼刀型涡流发生器

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2409193A1 (fr) * 1977-11-17 1979-06-15 Messerschmitt Boelkow Blohm Procede de commande des avions par controle des courants tourbillonnaires qui se degagent des bords d'attaque des ailes

Also Published As

Publication number Publication date
GB1332026A (en) 1973-10-03

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Legal Events

Date Code Title Description
ST Notification of lapse