WO2010010217A3 - Superficie de control de aeronave - Google Patents

Superficie de control de aeronave Download PDF

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Publication number
WO2010010217A3
WO2010010217A3 PCT/ES2009/070291 ES2009070291W WO2010010217A3 WO 2010010217 A3 WO2010010217 A3 WO 2010010217A3 ES 2009070291 W ES2009070291 W ES 2009070291W WO 2010010217 A3 WO2010010217 A3 WO 2010010217A3
Authority
WO
WIPO (PCT)
Prior art keywords
control surface
hinge pin
along
secondary control
primary control
Prior art date
Application number
PCT/ES2009/070291
Other languages
English (en)
French (fr)
Other versions
WO2010010217A2 (es
Inventor
Raúl Carlos LLAMAS SANDÍN
Pablo Timoteo SANZ MARTÍNEZ
Original Assignee
Airbus España S.L.
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 España S.L. filed Critical Airbus España S.L.
Priority to CA2731787A priority Critical patent/CA2731787C/en
Priority to EP09784130.8A priority patent/EP2319759B1/en
Priority to CN200980128895.4A priority patent/CN102105355B/zh
Priority to ES09784130.8T priority patent/ES2562675T3/es
Publication of WO2010010217A2 publication Critical patent/WO2010010217A2/es
Publication of WO2010010217A3 publication Critical patent/WO2010010217A3/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • 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
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Bridges Or Land Bridges (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

Superficie de control (1) de aeronave, en particular para superficie sustentadora (2) de aeronave, que comprende una superficie de control primaria (6) que comprende un eje de charnela (10), y una superficie de control secundaria (7) que comprende un eje de charnela (11), girando la superficie de control secundaria (7) a través de su eje de charnela (11) con respecto a la superficie de control primaria (6), ocupando la citada superficie de control secundaria (7) tan sólo parcialmente la envergadura de la superficie de control primaria (6), siendo la longitud de la superficie de control secundaria (7) a lo largo de su eje de charnela (11) significativamente menor que la longitud de la superficie de control primaria (6) a lo largo de su eje de charnela (10), estrechándose además significativamente la anchura o cuerda de la citada superficie de control secundaria (7) a lo largo de la dirección de su eje de charnela (11) hacia la punta de la superficie sustentadora (2) mediante una ley de estrechamiento diseñada expresamente para adaptar la distribución de rigidez a torsión a lo largo de la envergadura de la superficie sustentadora (2) a la distribución de carga aerodinámica en la misma, a la vez que la distribución de curvatura efectiva debida a la deflexión de la citada superficie de control (1) es tal que aumenta el ángulo de entrada en pérdida aerodinámica de la superficie sustentadora (2).
PCT/ES2009/070291 2008-07-23 2009-07-15 Superficie de control de aeronave WO2010010217A2 (es)

Priority Applications (4)

Application Number Priority Date Filing Date Title
CA2731787A CA2731787C (en) 2008-07-23 2009-07-15 Control surface of aircraft
EP09784130.8A EP2319759B1 (en) 2008-07-23 2009-07-15 Aircraft control surface
CN200980128895.4A CN102105355B (zh) 2008-07-23 2009-07-15 飞机的控制表面
ES09784130.8T ES2562675T3 (es) 2008-07-23 2009-07-15 Superficie de control de aeronave

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200802197 2008-07-23
ESP200802197 2008-07-23

Publications (2)

Publication Number Publication Date
WO2010010217A2 WO2010010217A2 (es) 2010-01-28
WO2010010217A3 true WO2010010217A3 (es) 2010-03-18

Family

ID=41443856

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2009/070291 WO2010010217A2 (es) 2008-07-23 2009-07-15 Superficie de control de aeronave

Country Status (6)

Country Link
US (1) US7992825B2 (es)
EP (1) EP2319759B1 (es)
CN (1) CN102105355B (es)
CA (1) CA2731787C (es)
ES (1) ES2562675T3 (es)
WO (1) WO2010010217A2 (es)

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US8933383B2 (en) * 2010-09-01 2015-01-13 The United States Of America As Represented By The Secretary Of The Army Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards
DE102010051216A1 (de) * 2010-11-12 2012-05-16 Airbus Operations Gmbh Seitenrudersystem an einem Flugzeug
GB201209666D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A hinge assembly for rotatably mounting a control surface on an aircraft
US9429402B2 (en) * 2013-04-24 2016-08-30 Simmonds Precision Products, Inc. Multi-stage drive mechanisms
EP2805879B1 (en) 2013-05-22 2017-07-05 Airbus Operations GmbH Flap arrangement for a wing of an aircraft and an aircraft with a wing comprising such a flap arrangement
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method
CN104648657A (zh) * 2013-11-22 2015-05-27 中国航空工业集团公司西安飞机设计研究所 一种可抑制振动的带调整片操纵面
ES2755765T3 (es) * 2013-12-23 2020-04-23 Airbus Operations Sl Superficie de control de aeronave
US9643716B2 (en) * 2014-04-01 2017-05-09 The Boeing Company Air vehicle, actuator assembly and associated method of manufacture
CN105015762B (zh) * 2014-04-21 2016-12-07 哈尔滨飞机工业集团有限责任公司 一种变传动比的飞机随动调整片机构
US20170106970A1 (en) * 2015-10-15 2017-04-20 The Boeing Company Composite failsafe torque tube
EP3170742B1 (en) * 2015-11-18 2018-02-21 Airbus Operations GmbH Foldable wing for an aircraft and aircraft having a foldable wing
US10487744B2 (en) 2016-05-23 2019-11-26 United Technologies Corporation Fence for duct tone mitigation
US10464667B2 (en) * 2016-09-29 2019-11-05 Ampaire, Inc. Oblique rotor-wing aircraft
CN106986004A (zh) * 2017-03-02 2017-07-28 中国航空研究院 一种飞机方向舵的随动增效器
CN107512384B (zh) * 2017-08-01 2020-04-21 中国航空工业集团公司西安飞机设计研究所 一种升降舵
CN108033012A (zh) * 2017-12-13 2018-05-15 四川宝天智控系统有限公司 Vtol固定翼无人机及其固定翼结构
CN108248825B (zh) * 2018-03-02 2020-12-08 西北工业大学 一种飞行器翼面结构
US10597141B2 (en) * 2018-03-30 2020-03-24 The Boeing Company Wing flap with torque member and method for forming thereof
US10647407B2 (en) * 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US10759516B2 (en) * 2018-03-30 2020-09-01 The Boeing Company Wing flap with torque member and method for forming thereof
CN208429234U (zh) * 2018-06-25 2019-01-25 深圳市大疆创新科技有限公司 固定翼无人机及其尾翼
CN109592012A (zh) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 一种有调整片的通用飞机复合材料方向舵及制造方法
CN111003150A (zh) * 2019-12-26 2020-04-14 中国航空工业集团公司西安飞机设计研究所 大中型飞机的双铰链方向舵结构
US11661175B2 (en) 2020-03-05 2023-05-30 Ruben Leon Wireless autopilot system
US11247767B2 (en) * 2020-03-05 2022-02-15 Ruben Leon Wireless autopilot system
US11623734B2 (en) 2020-12-02 2023-04-11 The Boeing Company Apparatus, system and method for supporting a wing flap of an aircraft

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3958779A (en) * 1975-05-27 1976-05-25 Fairchild Industries Inc. Aircraft control system with a jam isolating coupling
US4479620A (en) * 1978-07-13 1984-10-30 The Boeing Company Wing load alleviation system using tabbed allerons
WO2001005654A2 (en) * 1999-07-20 2001-01-25 The Boeing Company Vehicle control system and method using a control surface and a geared tab
US20090159755A1 (en) * 2007-12-21 2009-06-25 Airbus Espana, S.L. Aircraft control device

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US5651513A (en) * 1995-03-01 1997-07-29 Northrop Grumman Corporation Linear flap drive system
US6598834B2 (en) * 2000-02-14 2003-07-29 Aerotech Services Inc. Method for reducing fuel consumption in aircraft
DE10147827A1 (de) * 2001-09-27 2003-04-24 Airbus Gmbh Vorrichtung zur Änderung der Quertriebsgröße eines Flugzeughauptelementes mit vorzugsweise flächenförmiger Hinterkante
DE10156733B4 (de) * 2001-11-19 2006-04-20 Eads Deutschland Gmbh Aerodynamisches Profil mit verstellbarer Klappe
DE102004045732A1 (de) * 2004-09-21 2006-03-30 Airbus Deutschland Gmbh Flugzeug mit Flügeln, deren maximaler Auftrieb durch steuerbare Flügelkomponenten veränderbar ist
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7708231B2 (en) * 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3958779A (en) * 1975-05-27 1976-05-25 Fairchild Industries Inc. Aircraft control system with a jam isolating coupling
US4479620A (en) * 1978-07-13 1984-10-30 The Boeing Company Wing load alleviation system using tabbed allerons
WO2001005654A2 (en) * 1999-07-20 2001-01-25 The Boeing Company Vehicle control system and method using a control surface and a geared tab
US20090159755A1 (en) * 2007-12-21 2009-06-25 Airbus Espana, S.L. Aircraft control device

Also Published As

Publication number Publication date
ES2562675T3 (es) 2016-03-07
CN102105355B (zh) 2014-04-16
EP2319759B1 (en) 2015-11-25
EP2319759A2 (en) 2011-05-11
CA2731787A1 (en) 2010-01-28
CN102105355A (zh) 2011-06-22
WO2010010217A2 (es) 2010-01-28
US20100019083A1 (en) 2010-01-28
US7992825B2 (en) 2011-08-09
CA2731787C (en) 2016-11-22

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