[go: up one dir, main page]

WO2005044661A3 - Avion supersonique a commande aerodynamique - Google Patents

Avion supersonique a commande aerodynamique Download PDF

Info

Publication number
WO2005044661A3
WO2005044661A3 PCT/US2004/027562 US2004027562W WO2005044661A3 WO 2005044661 A3 WO2005044661 A3 WO 2005044661A3 US 2004027562 W US2004027562 W US 2004027562W WO 2005044661 A3 WO2005044661 A3 WO 2005044661A3
Authority
WO
WIPO (PCT)
Prior art keywords
supersonic aircraft
aerodynamic control
fuselage
wing
aircraft
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.)
Ceased
Application number
PCT/US2004/027562
Other languages
English (en)
Other versions
WO2005044661A2 (fr
Inventor
John M Morgenstern
Alan E Arslan
Howard Lee
Robert S Cuccias
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.)
Supersonic Aerospace International LLC
Original Assignee
Supersonic Aerospace International LLC
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
Priority claimed from US10/651,782 external-priority patent/US7070146B2/en
Priority claimed from US10/652,128 external-priority patent/US20050045764A1/en
Priority claimed from US10/706,671 external-priority patent/US20050116116A1/en
Application filed by Supersonic Aerospace International LLC filed Critical Supersonic Aerospace International LLC
Publication of WO2005044661A2 publication Critical patent/WO2005044661A2/fr
Publication of WO2005044661A3 publication Critical patent/WO2005044661A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/326—Air braking surfaces associated with fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/04—Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/16—Frontal aspect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/04—Noseplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B64C9/36—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles
    • 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
    • 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
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Details Of Aerials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un avion supersonique (900) comprenant un fuselage (901), une aile (904), et un canard (920) couplé au fuselage (901) à l'avant de l'aile (904) sur une position élevée permettant l'allongement vers l'avant sur la longueur d'élévation de l'avion, permettant d'obtenir une distribution de zone efficace et une signature sonique profilée.
PCT/US2004/027562 2003-08-29 2004-08-25 Avion supersonique a commande aerodynamique Ceased WO2005044661A2 (fr)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US10/652,128 2003-08-29
US10/651,782 US7070146B2 (en) 2003-08-29 2003-08-29 Aircraft thickness/camber control device for low sonic boom
US10/651,782 2003-08-29
US10/652,128 US20050045764A1 (en) 2003-08-29 2003-08-29 Canard position and dihedral for boom reduction and pitch/directional control
US10/706,671 US20050116116A1 (en) 2003-11-11 2003-11-11 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
US10/706,671 2003-11-11

Publications (2)

Publication Number Publication Date
WO2005044661A2 WO2005044661A2 (fr) 2005-05-19
WO2005044661A3 true WO2005044661A3 (fr) 2005-12-29

Family

ID=34577696

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2004/027562 Ceased WO2005044661A2 (fr) 2003-08-29 2004-08-25 Avion supersonique a commande aerodynamique

Country Status (1)

Country Link
WO (1) WO2005044661A2 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10253779B2 (en) 2016-08-11 2019-04-09 General Electric Company Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan
US10252790B2 (en) 2016-08-11 2019-04-09 General Electric Company Inlet assembly for an aircraft aft fan
US10704418B2 (en) 2016-08-11 2020-07-07 General Electric Company Inlet assembly for an aircraft aft fan
US10259565B2 (en) 2016-08-11 2019-04-16 General Electric Company Inlet assembly for an aircraft aft fan
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
CN113148110B (zh) * 2021-05-28 2024-06-18 西北工业大学 机翼变形装置和宽速域高超声速飞行器
CN114715380B (zh) * 2022-04-20 2024-07-02 中国航空发动机研究院 一种变体飞机及其驱动方法
CN115924060B (zh) * 2023-02-22 2023-05-16 中国空气动力研究与发展中心设备设计与测试技术研究所 一种基于连杆组件的非对称翼型反转机构及其使用方法
CN117755478A (zh) * 2024-02-22 2024-03-26 中国航空工业集团公司西安飞机设计研究所 一种飞机气动布局结构及其操纵方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3425650A (en) * 1967-10-02 1969-02-04 Joseph Silva Air deflector for supersonic aircraft
US4828204A (en) * 1979-08-13 1989-05-09 The Boeing Company Supersonic airplane
US5526999A (en) * 1992-11-03 1996-06-18 Meston; Vyacheslav A. Spacecraft with a crew escape system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3425650A (en) * 1967-10-02 1969-02-04 Joseph Silva Air deflector for supersonic aircraft
US4828204A (en) * 1979-08-13 1989-05-09 The Boeing Company Supersonic airplane
US5526999A (en) * 1992-11-03 1996-06-18 Meston; Vyacheslav A. Spacecraft with a crew escape system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
GOEBEL G. ET AL., THE SAAB JAS-39 GRIPEN., 1 June 2002 (2002-06-01), XP002992726, Retrieved from the Internet <URL:http://www.faqs.org/docs/air/avgrpn.html> *

Also Published As

Publication number Publication date
WO2005044661A2 (fr) 2005-05-19

Similar Documents

Publication Publication Date Title
WO2003059736A3 (fr) Conception d&#39;aeronef et aile interne d&#39;aeronef
WO2003004353A3 (fr) Vehicule aerien a decollage et a atterrissage vertical
WO2007133239A3 (fr) Activateurs de plasma pour la réduction de traînée sur les ailes, les nacelles et/ou le fuselage d&#39;aéronefs à décollage et atterrissage vertical
AU2002227282A1 (en) Joined wing supersonic aircraft
EP1607324B8 (fr) Volets de bord d&#39;attaque pour avion et procédés correspondants
EP1995171A3 (fr) Appareil et procédé de contrôle de flux de bord de fuite de surface portante par l&#39;effet d&#39;un plasma
AU2003209426A1 (en) Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom
WO2006073634A3 (fr) Aeronef a decollage et atterrissage verticaux (adav) a aile fixee en fleche negative
WO2009072754A3 (fr) Décollage et atterrissage d&#39;un aéronef à l&#39;aide d&#39;une voilure tournante variable
WO2006108957A3 (fr) Aeronef a faible bruit, notamment lors des decollages et des atterrissages.
EP0980823A3 (fr) Pointe de fuselage pour le pilotage d&#39;aéronefs
WO2007061641A3 (fr) Appareil et procede d&#39;attenuation de la charge alaire
EP2060769A3 (fr) Ensemble d&#39;inversion de poussée
WO2020003239A3 (fr) Aéronef à décollage et atterrissage verticaux
WO2005044661A3 (fr) Avion supersonique a commande aerodynamique
AU2003226692A1 (en) Triple-fuselage aircraft and families of aircraft of said type
EP1344915A3 (fr) Entrée d&#39;air à position variable pour réacteur d&#39;avion
EP2110312A3 (fr) Mise en forme de fuselage et inclusion de corps central sur un avion supersonique pour le contrôle et la réduction de bang sonique
EP1762492A3 (fr) Systèmes et procédés pour contrôler un dispositif de ravitaillement en vol
ATE498548T1 (de) Luftfahrzeug mit zugangsöffnung zur beladung
WO2006133062A3 (fr) Aeronef jouet
CA2514728A1 (fr) Systeme anticouple et de commande de lacet pour aeronef a voilure tournante
WO2004007282A3 (fr) Aeronef a aile tournante
WO2005049424A3 (fr) Dispositif de sustentation d&#39;aeronefs permettant un faible bang supersonique
FR2826055B1 (fr) Dispositif de propulsion a cycle variable par prelevement d&#39;air comprime pour avion supersonique

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NA NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): GM KE LS MW MZ NA SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
122 Ep: pct application non-entry in european phase