BR112015025381A2 - dispositivo para controlar a velocidade de um avião espacial durante a transição de uma fase de voo espacial para uma fase de voo aeronáutico e método de transição associado - Google Patents

dispositivo para controlar a velocidade de um avião espacial durante a transição de uma fase de voo espacial para uma fase de voo aeronáutico e método de transição associado

Info

Publication number
BR112015025381A2
BR112015025381A2 BR112015025381A BR112015025381A BR112015025381A2 BR 112015025381 A2 BR112015025381 A2 BR 112015025381A2 BR 112015025381 A BR112015025381 A BR 112015025381A BR 112015025381 A BR112015025381 A BR 112015025381A BR 112015025381 A2 BR112015025381 A2 BR 112015025381A2
Authority
BR
Brazil
Prior art keywords
flight phase
space
transition
aeronautical
controlling
Prior art date
Application number
BR112015025381A
Other languages
English (en)
Inventor
Santerre Angélique
Faure Benjamin
Favre Christophe
Ferreira Eugénio
Parpaite Pierre
Chevrollier Samuel
Original Assignee
Airbus Defence & Space Sas
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 Airbus Defence & Space Sas filed Critical Airbus Defence & Space Sas
Publication of BR112015025381A2 publication Critical patent/BR112015025381A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • 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
    • B64C9/323—Air braking surfaces associated with wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/14—Space shuttles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
    • B64G1/623—Retarding devices, e.g. retrorockets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • 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)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Retarders (AREA)
  • Traffic Control Systems (AREA)

Abstract

resumo dispositivo para controlar a velocidade de um avião espacial durante a transição de uma fase de voo espacial para uma fase de voo aeronáutico e método de transição associado um avião espacial (10) apropriado para voo aeronáutico compreendendo um corpo e uma asa (15) definindo uma superfície de aerofólio inferior além de meios de controle de atitude que compreendem um ou uma pluralidade de obturadores (11) dispostos sob a superfície de aerofólio inferior dos mesmos e manobráveis entre uma posição retraída e uma posição estendida inclinada para frenagem aerodinâmica durante a transição de uma fase de voo do espaço para uma fase de voo aeronáutico da aeronave.
BR112015025381A 2013-04-05 2014-03-28 dispositivo para controlar a velocidade de um avião espacial durante a transição de uma fase de voo espacial para uma fase de voo aeronáutico e método de transição associado BR112015025381A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1353088A FR3004167B1 (fr) 2013-04-05 2013-04-05 Dispositif de controle de la vitesse d'un avion spatial lors de la transition d'une phase de vol spatial vers une phase de vol aeronautique et procede de transition associe
PCT/EP2014/056349 WO2014161794A1 (fr) 2013-04-05 2014-03-28 Dispositif de contrôle de la vitesse d'un avion spatial lors de la transition d'une phase de vol spatial vers une phase de vol aéronautique et procédé de transition associé

Publications (1)

Publication Number Publication Date
BR112015025381A2 true BR112015025381A2 (pt) 2017-07-18

Family

ID=49003836

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015025381A BR112015025381A2 (pt) 2013-04-05 2014-03-28 dispositivo para controlar a velocidade de um avião espacial durante a transição de uma fase de voo espacial para uma fase de voo aeronáutico e método de transição associado

Country Status (9)

Country Link
US (1) US10046868B2 (pt)
EP (1) EP2981461B1 (pt)
JP (1) JP2016514647A (pt)
CN (1) CN105228900A (pt)
BR (1) BR112015025381A2 (pt)
FR (1) FR3004167B1 (pt)
RU (1) RU2015147386A (pt)
SG (1) SG11201508164SA (pt)
WO (1) WO2014161794A1 (pt)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2579221A (en) * 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft control mechanism
RU2710992C1 (ru) * 2019-05-16 2020-01-14 Анатолий Михайлович Криштоп Суборбитальный ракетоплан криштопа (срк), гибридная силовая установка (гсу) для срк и способ функционирования срк с гсу (варианты)
CN112357060B (zh) * 2020-10-29 2022-08-02 天津腾云智航科技有限公司 一种固定翼无人机襟翼高程收敛控制方法

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3289974A (en) * 1964-01-02 1966-12-06 Trw Inc Manned spacecraft with staged re-entry
US3390853A (en) * 1966-05-23 1968-07-02 North American Rockwell Variable geometry re-entry vehicle
US3511453A (en) * 1967-04-27 1970-05-12 Raytheon Co Controllable reentry vehicle
US3485465A (en) * 1967-11-21 1969-12-23 Gen Dynamics Corp Single unit main landing gear system
US7240878B2 (en) * 1996-05-13 2007-07-10 Andrew James Towne High wing monoplane aerospace plane based fighter
US6193187B1 (en) * 1998-12-31 2001-02-27 Harry Scott Payload carry and launch system
US6735842B1 (en) * 1999-03-08 2004-05-18 Man Technologie Ag Movable structural component for a thermomechanically stressed assembly as well as a process for producing the structural component
JP2001206298A (ja) * 2000-01-28 2001-07-31 Fuji Heavy Ind Ltd 航空宇宙機
CN1412083A (zh) * 2002-06-25 2003-04-23 潘延军 超高压气动空天飞机
US7654489B2 (en) * 2003-06-10 2010-02-02 Aviation Dynamics, Corp Lifting body aircraft and reentry vehicle with chines
US7834494B2 (en) * 2004-06-04 2010-11-16 The Boeing Company Fault-tolerant electromechanical actuator having a torque sensing control system
US20070068138A1 (en) * 2005-05-17 2007-03-29 Sheerin Geoffrey T Rocket vehicle and engine
US7229048B1 (en) * 2005-11-30 2007-06-12 The Boeing Company Aerodynamic control of a hypersonic entry vehicle
US7611095B1 (en) * 2006-04-28 2009-11-03 The Boeing Company Aerodynamic re-entry vehicle control with active and passive yaw flaps
US20100096491A1 (en) * 2006-10-02 2010-04-22 Rocket Racing, Inc. Rocket-powered entertainment vehicle
FR2924411B1 (fr) 2007-11-29 2010-02-12 Astrium Sas Dispositif d'arriere corps d'engin spatial
CN100576124C (zh) * 2008-10-30 2009-12-30 北京控制工程研究所 一种空天飞机高空爬升纵向控制方法
FR2961179B1 (fr) * 2010-06-14 2012-07-27 Astrium Sas Module reutilisable simplifie pour lanceur
US8528853B2 (en) * 2010-07-29 2013-09-10 David I. Luther In-line staged horizontal takeoff and landing space plane
DE102011016336A1 (de) * 2011-04-07 2012-10-11 Airbus Operations Gmbh Hochauftriebssystem für ein Luftfahrzeug
CN102826227B (zh) * 2012-08-22 2015-09-09 冯加伟 无人空天战机
US9073647B2 (en) * 2013-04-25 2015-07-07 Biosphere Aerospace Llc Space shuttle orbiter and return system

Also Published As

Publication number Publication date
SG11201508164SA (en) 2015-11-27
JP2016514647A (ja) 2016-05-23
US10046868B2 (en) 2018-08-14
EP2981461A1 (fr) 2016-02-10
US20160052650A1 (en) 2016-02-25
WO2014161794A1 (fr) 2014-10-09
FR3004167B1 (fr) 2015-07-10
EP2981461B1 (fr) 2017-01-11
RU2015147386A (ru) 2017-05-10
CN105228900A (zh) 2016-01-06
FR3004167A1 (fr) 2014-10-10

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]