FR2445797A1 - Volet de sustentation operant par soufflage sur surface d'extrados et son procede d'utilisation - Google Patents

Volet de sustentation operant par soufflage sur surface d'extrados et son procede d'utilisation

Info

Publication number
FR2445797A1
FR2445797A1 FR7931825A FR7931825A FR2445797A1 FR 2445797 A1 FR2445797 A1 FR 2445797A1 FR 7931825 A FR7931825 A FR 7931825A FR 7931825 A FR7931825 A FR 7931825A FR 2445797 A1 FR2445797 A1 FR 2445797A1
Authority
FR
France
Prior art keywords
shutter
blowing
wing
same
flap
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.)
Granted
Application number
FR7931825A
Other languages
English (en)
Other versions
FR2445797B1 (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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of FR2445797A1 publication Critical patent/FR2445797A1/fr
Application granted granted Critical
Publication of FR2445797B1 publication Critical patent/FR2445797B1/fr
Granted 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
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)

Abstract

L'invention concerne un volet pour système de sustentation opérant par soufflage sur surface d'extrados. Le volet 34 est placé sur le bord de fuite de l'aile 14, en arrière du réacteur correspondant 26 et il comporte une surface d'extrados 38 qui est incurvée de manière que son rayon de courbure augmente, dans la direction de corde, depuis la partie incurvée avant jusqu'au bord de fuite; chaque volet est déplacé d'une position de rangement dans l'aile jusque dans une position de déploiement complet où la surface d'extrados du volet forme un prolongement continu de la partie arrière fixe de la surface d'extrados de l'aile, des générateurs de tourbillons 35 étant placés en avant du volet pour produire des tourbillons servant à réduire le moment de tangage longitudinal quand le volet se trouve dans sa position de déploiement. Application aux avions à décollage et atterissage court.
FR7931825A 1979-01-02 1979-12-27 Volet de sustentation operant par soufflage sur surface d'extrados et son procede d'utilisation Granted FR2445797A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11779A 1979-01-02 1979-01-02
US11679A 1979-01-02 1979-01-02

Publications (2)

Publication Number Publication Date
FR2445797A1 true FR2445797A1 (fr) 1980-08-01
FR2445797B1 FR2445797B1 (fr) 1985-03-29

Family

ID=26667243

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7931825A Granted FR2445797A1 (fr) 1979-01-02 1979-12-27 Volet de sustentation operant par soufflage sur surface d'extrados et son procede d'utilisation

Country Status (4)

Country Link
DE (1) DE2952821A1 (fr)
FR (1) FR2445797A1 (fr)
GB (1) GB2038995B (fr)
IT (1) IT1126857B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518210A (en) * 1994-04-11 1996-05-21 Mcdonnell Douglas Corporation Seal plate for aircraft movable flight control surfaces
US7878458B2 (en) * 2007-10-29 2011-02-01 The Boeing Company Method and apparatus for enhancing engine-powered lift in an aircraft
BR112020013309A2 (pt) * 2017-12-28 2020-12-01 Aero Design Labs, Inc. arranjo de carenagem de saída de duto
CN110539882B (zh) * 2019-07-16 2021-07-16 中国航空研究院 一种前缘变弯襟翼和前缘缝翼交界处流动优化方法及装置
CN114021265A (zh) * 2021-12-08 2022-02-08 辽宁科技大学 一种基于对数螺旋线的飞机用翼型

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3837601A (en) * 1973-03-09 1974-09-24 Boeing Co Aerodynamic slot closing mechanism
US3971534A (en) * 1973-12-28 1976-07-27 The Boeing Company Method of and apparatus for controlling flow attachment to the wing and flap surfaces of an upper surface blowing type aircraft
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
US4019696A (en) * 1973-12-28 1977-04-26 The Boeing Company Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface
GB1508389A (en) * 1976-05-03 1978-04-26 Boeing Co Aerodynamic lift enhancing apparatus

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3987983A (en) * 1974-12-20 1976-10-26 The Boeing Company Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism
US3971532A (en) * 1975-08-04 1976-07-27 Craig Fountain Rudder restraint for grounded aircraft

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3837601A (en) * 1973-03-09 1974-09-24 Boeing Co Aerodynamic slot closing mechanism
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
US3971534A (en) * 1973-12-28 1976-07-27 The Boeing Company Method of and apparatus for controlling flow attachment to the wing and flap surfaces of an upper surface blowing type aircraft
US4019696A (en) * 1973-12-28 1977-04-26 The Boeing Company Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface
GB1508389A (en) * 1976-05-03 1978-04-26 Boeing Co Aerodynamic lift enhancing apparatus

Also Published As

Publication number Publication date
IT8047504A0 (it) 1980-01-02
GB2038995B (en) 1982-11-17
IT1126857B (it) 1986-05-21
GB2038995A (en) 1980-07-30
DE2952821A1 (de) 1980-07-17
FR2445797B1 (fr) 1985-03-29

Similar Documents

Publication Publication Date Title
US4015787A (en) Aircraft wing
US4540143A (en) Nacelle/wing assembly with wake control device
US4449681A (en) Aerodynamically contoured, low drag wing, engine and engine nacelle combination
US4449683A (en) Aerodynamically contoured, low drag wing engine and engine nacelle combination
US4449680A (en) Aerodynamically contoured, low drag wing engine and engine nacelle combination
US5772155A (en) Aircraft wing flaps
US4702441A (en) Aircraft wing stall control device and method
US3504870A (en) Aircraft wing variable camber leading edge flap
FR2427249A1 (fr) Profil de voilure pour aeronef
FR2386449A1 (fr) Dispositif hypersustentateur de bord d'attaque d'ailes d'avions
FR2445798A1 (fr) Mecanisme d'actionnement de volet dans un avion comportant un systeme de sustentation operant par soufflage sur surface d'extrados
CA2291275A1 (fr) Extremites d'aile carrossees a bord d'attaque arrondi
US2261363A (en) Spoiler
EP0466826A1 (fr) Generateur de tourbillons a faible trainee
US5992796A (en) Secondary wing system for use on an aircraft
US3126173A (en) Alvarez-calderdn
JPH01101296A (ja) パイロン
US4489905A (en) Nacelle-pylon configuration for an aircraft and method of using the same
FR2420481A1 (fr) Parachute a voilure multi-cellulaire perfectionnee
EP0735970B1 (fr) Ensemble aile/nacelle d'avion
US5178348A (en) Contoured wing/flap assembly and method
FR2445797A1 (fr) Volet de sustentation operant par soufflage sur surface d'extrados et son procede d'utilisation
US4449682A (en) Aerodynamically contoured, low drag wing, engine and engine nacelle combination
EP0375382A2 (fr) Volet d'aile avec éliminateur de parasites
US4790494A (en) Aircraft empennage with fixed trailing edge horizontal stabilizer

Legal Events

Date Code Title Description
ST Notification of lapse