ES2562675T3 - Superficie de control de aeronave - Google Patents

Superficie de control de aeronave Download PDF

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Publication number
ES2562675T3
ES2562675T3 ES09784130.8T ES09784130T ES2562675T3 ES 2562675 T3 ES2562675 T3 ES 2562675T3 ES 09784130 T ES09784130 T ES 09784130T ES 2562675 T3 ES2562675 T3 ES 2562675T3
Authority
ES
Spain
Prior art keywords
control surface
hinge axis
along
airfoil
secondary 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.)
Active
Application number
ES09784130.8T
Other languages
English (en)
Inventor
Raúl Carlos LLAMAS SANDÍN
Pablo Timoteo SANZ MARTÍNEZ
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.)
Airbus Operations SL
Original Assignee
Airbus Operations SL
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 Operations SL filed Critical Airbus Operations SL
Application granted granted Critical
Publication of ES2562675T3 publication Critical patent/ES2562675T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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

Abstract

Superficie de control (1) de aeronave, en particular para superficie sustentadora (2) de aeronave, que comprende una superficie decontrol 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 superficiede control primaria (6), siendo la longitud de la superficie decontrol secundaria (7) a lo largo de su eje de charnela (11) significativamente menor que la longitud de la superficie de controlprimaria (6) a lo largo de su eje de charnela (10), estrechándoseademás significativamente la anchura o cuerda de la citada superficie de control secundaria (7) a lo largo de la dirección de sueje 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 decarga aerodinámica en la misma, a la vez que la distribución decurvatura efectiva debida a la deflexión de la citada superficiede control (1) es tal que aumenta el ángulo de entrada en pérdidaaerodinámica de la superficie sustentadora (2).

Description

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Claims (1)

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ES09784130.8T 2008-07-23 2009-07-15 Superficie de control de aeronave Active ES2562675T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ES200802197 2008-07-23
ES200802197 2008-07-23
PCT/ES2009/070291 WO2010010217A2 (es) 2008-07-23 2009-07-15 Superficie de control de aeronave

Publications (1)

Publication Number Publication Date
ES2562675T3 true ES2562675T3 (es) 2016-03-07

Family

ID=41443856

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09784130.8T Active ES2562675T3 (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)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
EP2886450B1 (en) * 2013-12-23 2019-09-18 Airbus Operations S.L. Aircraft control surface
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
US10759516B2 (en) * 2018-03-30 2020-09-01 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
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
US11247767B2 (en) * 2020-03-05 2022-02-15 Ruben Leon Wireless autopilot system
US11661175B2 (en) 2020-03-05 2023-05-30 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

Family Cites Families (11)

* 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
US5651513A (en) * 1995-03-01 1997-07-29 Northrop Grumman Corporation Linear flap drive system
US6257528B1 (en) * 1999-07-20 2001-07-10 The Boeing Company Vehicle control system and method employing control surface and geared tab
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
ES2345584B1 (es) * 2007-12-21 2011-07-18 Airbus Operations, S.L. Superficie de control de aeronave.

Also Published As

Publication number Publication date
CA2731787C (en) 2016-11-22
CA2731787A1 (en) 2010-01-28
EP2319759B1 (en) 2015-11-25
US7992825B2 (en) 2011-08-09
WO2010010217A2 (es) 2010-01-28
CN102105355A (zh) 2011-06-22
WO2010010217A3 (es) 2010-03-18
US20100019083A1 (en) 2010-01-28
EP2319759A2 (en) 2011-05-11
CN102105355B (zh) 2014-04-16

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