[go: up one dir, main page]

WO2006004570A3 - Poutre de queue de commande de vol integrale a inclinaison avant - Google Patents

Poutre de queue de commande de vol integrale a inclinaison avant Download PDF

Info

Publication number
WO2006004570A3
WO2006004570A3 PCT/US2005/001350 US2005001350W WO2006004570A3 WO 2006004570 A3 WO2006004570 A3 WO 2006004570A3 US 2005001350 W US2005001350 W US 2005001350W WO 2006004570 A3 WO2006004570 A3 WO 2006004570A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
support arm
control surface
tail boom
flying control
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/US2005/001350
Other languages
English (en)
Other versions
WO2006004570A2 (fr
WO2006004570B1 (fr
Inventor
Ross Steven Reynolds
Doug Ellwood Shultz
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.)
Northrop Grumman Corp
Original Assignee
Northrop Grumman Corp
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 Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of WO2006004570A2 publication Critical patent/WO2006004570A2/fr
Publication of WO2006004570B1 publication Critical patent/WO2006004570B1/fr
Publication of WO2006004570A3 publication Critical patent/WO2006004570A3/fr
Anticipated expiration legal-status Critical
Ceased 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
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/08—Adjustable control surfaces or members, e.g. rudders bodily displaceable
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

L'invention concerne un mécanisme de commande d'un déplacement d'avion pour réguler le déplacement d'un avion, à partir d'un emplacement éloigné d'une partie du corps de l'avion. Ce mécanisme de commande auxiliaire d'avion présente au moins un bras de support de surface de commande relié à la partie de corps de l'avion et s'étendant à partir de celle-ci, et une surface de commande de flux auxiliaire reliée au bras de support. La commande pivotante du déplacement du bras de support permet de faire fonctionner la surface de commande de flux auxiliaire pour défléchir le flux d'air de sorte à réguler l'orientation de l'avion. En outre, la surface de commande de flux d'air peut également défléchir le flux d'air par une déflexion autour du bras de support.
PCT/US2005/001350 2004-02-09 2005-01-18 Poutre de queue de commande de vol integrale a inclinaison avant Ceased WO2006004570A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/774,932 2004-02-09
US10/774,932 US7111810B2 (en) 2004-02-09 2004-02-09 Forward pivoted full flying control tail boom

Publications (3)

Publication Number Publication Date
WO2006004570A2 WO2006004570A2 (fr) 2006-01-12
WO2006004570B1 WO2006004570B1 (fr) 2006-04-20
WO2006004570A3 true WO2006004570A3 (fr) 2006-05-11

Family

ID=34827092

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/001350 Ceased WO2006004570A2 (fr) 2004-02-09 2005-01-18 Poutre de queue de commande de vol integrale a inclinaison avant

Country Status (2)

Country Link
US (2) US7111810B2 (fr)
WO (1) WO2006004570A2 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060108472A1 (en) * 2004-11-19 2006-05-25 Clark Walter D Control system for an aircraft
US20070262199A1 (en) * 2006-05-11 2007-11-15 Shelton David B Shelton wing in ground effect
US8074926B2 (en) * 2006-12-22 2011-12-13 Calvin Burgess Structural dynamic stability for an aircraft
US8333348B1 (en) * 2010-02-15 2012-12-18 The Boeing Company Wing tip load alleviation device and method
CN105882988A (zh) * 2014-12-31 2016-08-24 航天神舟飞行器有限公司 一种小型无人机载荷与机身快速装卸设计方案
TWI688519B (zh) * 2018-01-08 2020-03-21 經緯航太科技股份有限公司 定翼機起飛系統及其方法
CN114954910B (zh) * 2021-02-18 2024-06-11 海鹰航空通用装备有限责任公司 一种可调后掠角的副翼操纵机构及具有其的无人机

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1929255A (en) * 1929-05-10 1933-10-03 Stearman Aircraft Company Airplane
US2120065A (en) * 1935-05-11 1938-06-07 Pollopas Patents Ltd Balancing device for flying machines
US4598888A (en) * 1980-01-09 1986-07-08 Airbus Industrie Fixed-wing aircraft with tandem supporting surfaces
US6224012B1 (en) * 1998-12-30 2001-05-01 Donald H. Wooley Roadable aircraft combined vehicle for practical use

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1875267A (en) 1932-08-30 Umberto savoja
US641119A (en) 1899-03-24 1900-01-09 James Parkerson Kemper Apparatus for handling sugar-cane.
US1817651A (en) * 1928-07-16 1931-08-04 Rudolph W Schroeder Airplane and method of control
US2173674A (en) 1933-06-07 1939-09-19 Zap Dev Corp Aileron device
US2049188A (en) * 1933-09-15 1936-07-28 Alfaro Heraclio Aeroplane
US2257940A (en) * 1938-06-22 1941-10-07 Dornier Werke Gmbh Airplane having a liftable pusher plant
US2326819A (en) 1940-08-28 1943-08-17 Curtiss Wright Corp Airplane
US2601962A (en) * 1946-01-29 1952-07-01 Douglas Aircraft Co Inc Aircraft balancing means
US2623714A (en) * 1948-12-01 1952-12-30 Sperry Corp Automatic flight control system
US3009670A (en) 1959-04-09 1961-11-21 Advanced Aircraft Dev Corp Airplane with adjustable wings and tail
US3653611A (en) 1970-03-24 1972-04-04 Mason Trupp Slotted delta wing aircraft
US3934843A (en) 1974-08-05 1976-01-27 Black John O Free wing for convertible aircraft structure
US4538779A (en) 1982-09-30 1985-09-03 The Boeing Company Caster type empennage assembly for aircraft
US5395073A (en) 1992-03-13 1995-03-07 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with articulated tail boom
US5863013A (en) 1991-11-20 1999-01-26 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with improved shock dampening and absorbing means
US5769359A (en) 1993-01-22 1998-06-23 Freewing Aerial Robotics Corporation Active feedback loop to control body pitch in STOL/VTOL free wing aircraft
DE19916915B4 (de) * 1999-04-14 2005-08-11 Infineon Technologies Ag Schaltnetzteil und Verfahren zur Ermittlung der Versorgungsspannung in einem Schaltnetzteil
US6181989B1 (en) * 1999-10-22 2001-01-30 Joseph Andrew Gwozdecki Aircraft attitude sensor and feedback control system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1929255A (en) * 1929-05-10 1933-10-03 Stearman Aircraft Company Airplane
US2120065A (en) * 1935-05-11 1938-06-07 Pollopas Patents Ltd Balancing device for flying machines
US4598888A (en) * 1980-01-09 1986-07-08 Airbus Industrie Fixed-wing aircraft with tandem supporting surfaces
US6224012B1 (en) * 1998-12-30 2001-05-01 Donald H. Wooley Roadable aircraft combined vehicle for practical use

Also Published As

Publication number Publication date
US7516921B2 (en) 2009-04-14
US7111810B2 (en) 2006-09-26
US20050173593A1 (en) 2005-08-11
US20060022086A1 (en) 2006-02-02
WO2006004570A2 (fr) 2006-01-12
WO2006004570B1 (fr) 2006-04-20

Similar Documents

Publication Publication Date Title
CN101506050B (zh) 用于飞机的增升系统
CN101668681B (zh) 用于飞行器的空气动力绕流体的扰流器
JP2010512274A5 (fr)
EP1762492A3 (fr) Systèmes et procédés pour contrôler un dispositif de ravitaillement en vol
DE50303170D1 (de) Vorrichtung zur Ansteuerung der Vorflügel und Landeklappen eines Flugzeuges
CA2607358A1 (fr) Systeme de controle de direction de vol
FR2866314B1 (fr) Trappe de train d'atterrissage a cinematique controlee
WO2009020453A3 (fr) Levier de commande adapté pour être utilisé dans un système de commandes de vol électriques, et transmission destinée à être utilisée dans celui-ci
WO2008137217A3 (fr) Algorithme de commande de parcours de vol et de vitesse verticale pour un déplacement collectif utilisant une file d'attente tactile et des retours tactiles
ATE329825T1 (de) Betätigungssystem für ein aerodynamisches ruder
ATE557333T1 (de) Verbesserungen bezüglich eines aktiven steuerknüppels
WO2006004570A3 (fr) Poutre de queue de commande de vol integrale a inclinaison avant
EP0976651A3 (fr) Aéronef avec un fuselage portant et une aile à incidence variable
RU2009122222A (ru) Система обеспечения большой подъемной силы на крыле самолета и способ управления ею
CA2568275A1 (fr) Methode et dispositif permettant de modifier le sillage
WO2008071399B1 (fr) Aile d'aéronef
WO2004042315A3 (fr) Elevation controlee dynamiquement en temps reel et conteneur canon azimut monte sur un vehicule de combat aerien a ailes fixes
DE602004001023D1 (de) System zur automatischen Steuerung von Hochauftriebsklappen eines Flugzeugs, insbesondere Flügelvorderkanten
FR2866313B1 (fr) Trappe articulee pour train d'atterrissage d'aeronef
WO2010055213A8 (fr) Systeme de commande de capot d'inverseur de poussee pour nacelle de turboreacteur
CN110294102A (zh) 一体式襟副翼的复合运动机构
WO2004007282A3 (fr) Aeronef a aile tournante
CN102781776B (zh) 飞机的高升力系统和具有该高升力系统的飞机
US10427779B2 (en) Aircraft wing with an adaptive shock control bump
EP1759994A3 (fr) Cône, en particulier pour un système de ravitaillement en vol

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 SM 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): BW GH 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 IS IT LT 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

B Later publication of amended claims

Effective date: 20060228

121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: DE

WWW Wipo information: withdrawn in national office

Country of ref document: DE

122 Ep: pct application non-entry in european phase

Ref document number: 05793524

Country of ref document: EP

Kind code of ref document: A2