ATE523424T1 - Flugzeug mit einem trimmbaren höhenleitwerk - Google Patents
Flugzeug mit einem trimmbaren höhenleitwerkInfo
- Publication number
- ATE523424T1 ATE523424T1 AT07787319T AT07787319T ATE523424T1 AT E523424 T1 ATE523424 T1 AT E523424T1 AT 07787319 T AT07787319 T AT 07787319T AT 07787319 T AT07787319 T AT 07787319T AT E523424 T1 ATE523424 T1 AT E523424T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- elevator
- horizontal stabilizer
- trimable
- fuselage
- Prior art date
Links
Classifications
-
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Vehicle Body Suspensions (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Cage And Drive Apparatuses For Elevators (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102006032003.4A DE102006032003B4 (de) | 2006-07-11 | 2006-07-11 | Trimmbares Höhenleitwerk |
| PCT/EP2007/057044 WO2008006831A1 (en) | 2006-07-11 | 2007-07-10 | Trimmable horizontal stabilizer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE523424T1 true ATE523424T1 (de) | 2011-09-15 |
Family
ID=38476155
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT07787319T ATE523424T1 (de) | 2006-07-11 | 2007-07-10 | Flugzeug mit einem trimmbaren höhenleitwerk |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US7963485B2 (de) |
| EP (1) | EP2038171B1 (de) |
| JP (1) | JP5257996B2 (de) |
| CN (1) | CN101495367B (de) |
| AT (1) | ATE523424T1 (de) |
| BR (1) | BRPI0712881A2 (de) |
| CA (1) | CA2656794A1 (de) |
| DE (1) | DE102006032003B4 (de) |
| RU (1) | RU2448019C2 (de) |
| WO (1) | WO2008006831A1 (de) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8042772B2 (en) | 2008-03-05 | 2011-10-25 | The Boeing Company | System and method for pneumatically actuating a control surface of an airfoil |
| KR101730664B1 (ko) | 2009-02-02 | 2017-04-26 | 에어로바이론먼트, 인크. | 멀티모드 무인 항공기 |
| DK3133019T3 (en) | 2009-09-09 | 2019-02-18 | Aerovironment Inc | NOISE DEVICE FOR A DRONE PROTECTION PIPE |
| JP5886201B2 (ja) | 2009-09-09 | 2016-03-16 | エアロバイロメント, インコーポレイテッドAerovironment, Inc. | エレボン制御システム |
| US8727280B1 (en) | 2009-12-08 | 2014-05-20 | The Boeing Company | Inflatable airfoil system having reduced radar and infrared observability |
| US8931739B1 (en) | 2009-12-08 | 2015-01-13 | The Boeing Company | Aircraft having inflatable fuselage |
| US8342451B1 (en) * | 2009-12-08 | 2013-01-01 | The Boeing Company | Variable pitch airfoils |
| US9175702B1 (en) | 2011-05-24 | 2015-11-03 | Stephen Lee Bailey | Externally supported foil with reversible camber and variable chord length |
| WO2015053838A1 (en) | 2013-07-22 | 2015-04-16 | Learjet Inc. | Tailplane with positive camber |
| CN103387048B (zh) * | 2013-07-27 | 2016-01-06 | 哈尔滨工业大学 | 气动驱动/变形/承载一体化的变体柔性后缘结构 |
| CN103466076B (zh) * | 2013-08-23 | 2015-12-02 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机平尾随动装置 |
| ES2683159T3 (es) * | 2015-12-31 | 2018-09-25 | Airbus Operations S.L | Aeronave con motores montados en la parte trasera |
| CN105691594A (zh) * | 2016-01-19 | 2016-06-22 | 高萍 | 一种新的飞翼布局飞行器控制方法及控制装置 |
| EP3448749B1 (de) | 2016-04-25 | 2020-07-01 | Bombardier Inc. | Luftfahrzeugpitchregelungssystem mit elektronisch übersetztem höhenruder |
| US10106265B2 (en) | 2016-06-24 | 2018-10-23 | General Electric Company | Stabilizer assembly for an aircraft AFT engine |
| US10518865B2 (en) | 2017-05-11 | 2019-12-31 | Bell Helicopter Textron Inc. | Aircraft horizontal stabilizer design |
| US10611460B2 (en) | 2017-05-11 | 2020-04-07 | Bell Helicopter Textron Inc. | Aircraft vertical stabilizer design |
| CN110652713B (zh) * | 2019-09-30 | 2021-02-19 | 浙江海洋大学 | 一种户外运动用回旋镖 |
| CN112429199B (zh) * | 2020-11-18 | 2021-09-24 | 北京北航天宇长鹰无人机科技有限公司 | 一种采用全动升降舵的无人机 |
| US12649566B1 (en) | 2025-02-12 | 2026-06-09 | Textron Aviation Inc. | Apparatus and method for trimming an aircraft stabilizer |
Family Cites Families (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB313415A (en) * | 1927-12-06 | 1929-06-06 | Norman Macmillan | Improvements in or relating to the tail surfaces of aircraft |
| US3285540A (en) * | 1964-06-15 | 1966-11-15 | Lee Shao-Tang | Shiftable variable area wing construction |
| DE2804254C2 (de) * | 1978-02-01 | 1985-02-07 | Grob, Burkhart, Dipl.-Ing. ETH, 8023 Großhesselohe | Tragflügel mit Klappe |
| US4247066A (en) * | 1978-02-21 | 1981-01-27 | General Dynamics Corporation | Airfoil variable cambering device and method |
| JPS54146400A (en) * | 1978-05-10 | 1979-11-15 | Boeing Co | Pilot wing surface automatic recomposing method of stol aircraft and its device |
| US4291853A (en) * | 1978-12-26 | 1981-09-29 | The Boeing Company | Airplane all-moving airfoil with moment reducing apex |
| DE2907912C2 (de) * | 1979-03-01 | 1985-06-05 | Dornier Gmbh, 7990 Friedrichshafen | Quertriebskörper mit veränderbarer Profilierung, insbesondere Nasenteile von Flugzeugtragflügeln |
| US4432516A (en) * | 1980-04-02 | 1984-02-21 | Muscatell Ralph P | Variable airfoil assembly |
| US4582278A (en) * | 1985-02-15 | 1986-04-15 | Northrop Corporation | Air foil having adjustable shape |
| DE3668864D1 (de) * | 1986-01-24 | 1990-03-15 | Boeing Co | Heckklappe. |
| US4790494A (en) * | 1986-10-14 | 1988-12-13 | Grumman Aerospace Corporation | Aircraft empennage with fixed trailing edge horizontal stabilizer |
| US4890803A (en) * | 1987-07-29 | 1990-01-02 | Smith Larry L | Airfoil with fixed and variable upper camber portions |
| JPH0228098A (ja) * | 1988-07-18 | 1990-01-30 | Mitsubishi Heavy Ind Ltd | 形状可変翼 |
| US5004189A (en) * | 1988-08-31 | 1991-04-02 | Igram Dale J | Reconfigurable airfoil |
| JPH0466393A (ja) * | 1990-07-05 | 1992-03-02 | Mitsubishi Heavy Ind Ltd | 航空機 |
| US5181678A (en) * | 1991-02-04 | 1993-01-26 | Flex Foil Technology, Inc. | Flexible tailored elastic airfoil section |
| US5681014A (en) * | 1992-05-15 | 1997-10-28 | Palmer; Harry W. | Torsional twist airfoil control means |
| US5288039A (en) * | 1992-07-29 | 1994-02-22 | Delaurier James D | Spanwise graded twist panel |
| JPH06321189A (ja) * | 1993-05-10 | 1994-11-22 | Mitsubishi Heavy Ind Ltd | 揚力可変装置 |
| DE19707392A1 (de) * | 1997-02-25 | 1998-08-27 | Deutsch Zentr Luft & Raumfahrt | Aerodynamisches Bauteil, wie Landeklappe, Tragflügel, Höhen- oder Seitenleitwerk, mit veränderbarer Wölbung |
| US6016992A (en) * | 1997-04-18 | 2000-01-25 | Kolacny; Gordon | STOL aircraft |
| AU3405499A (en) * | 1998-05-25 | 1999-12-13 | Prospective Concepts Ag | Adaptive pneumatic wings for flying devices with fixed wings |
| US6045096A (en) * | 1998-06-30 | 2000-04-04 | Rinn; Aaron | Variable camber airfoil |
| US6491262B1 (en) * | 1999-01-15 | 2002-12-10 | Sridhar Kota | System for varying a surface contour |
| DE10055961B4 (de) * | 2000-11-11 | 2004-09-09 | Eads Deutschland Gmbh | Variabler Flügelbereich mit einstellbarer, sich in Spannweiten-Richtung erstreckender Profilform |
| US6481667B1 (en) * | 2001-03-05 | 2002-11-19 | Northrop Grumman Corporation | System and method for deflecting an aerodynamic control surface |
| US6843447B2 (en) * | 2003-01-06 | 2005-01-18 | Brian H. Morgan | Vertical take-off and landing aircraft |
| RU30705U1 (ru) * | 2003-02-03 | 2003-07-10 | Федеральное государственное унитарное предприятие Лётно-исследовательский институт им. М.М.Громова | Исполнительный механизм системы автоматического управления самолётом |
| DK1603798T3 (da) * | 2003-03-03 | 2011-02-14 | Flexsys Inc | Tilpasningsdygtigt og fleksibelt vinge- og rotorsystem |
| DE10353672A1 (de) * | 2003-11-12 | 2005-06-23 | Airbus Deutschland Gmbh | Verfahren zur Lastbegrenzung in Antriebssystemen |
| DE102004045651B4 (de) * | 2004-09-21 | 2010-09-16 | Airbus Deutschland Gmbh | Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderbarem Profil |
| DE102004056649A1 (de) * | 2004-11-24 | 2006-06-01 | Airbus Deutschland Gmbh | Deckhaut für eine formvariable aerodynamische Fläche |
| JP4568906B2 (ja) * | 2004-12-16 | 2010-10-27 | 独立行政法人 宇宙航空研究開発機構 | 飛行体用翼、飛行体用翼複合材およびその製造方法 |
-
2006
- 2006-07-11 DE DE102006032003.4A patent/DE102006032003B4/de not_active Expired - Fee Related
-
2007
- 2007-07-10 CA CA002656794A patent/CA2656794A1/en not_active Abandoned
- 2007-07-10 WO PCT/EP2007/057044 patent/WO2008006831A1/en not_active Ceased
- 2007-07-10 US US12/307,619 patent/US7963485B2/en not_active Expired - Fee Related
- 2007-07-10 AT AT07787319T patent/ATE523424T1/de not_active IP Right Cessation
- 2007-07-10 JP JP2009518878A patent/JP5257996B2/ja not_active Expired - Fee Related
- 2007-07-10 CN CN2007800258026A patent/CN101495367B/zh not_active Expired - Fee Related
- 2007-07-10 RU RU2009103772/11A patent/RU2448019C2/ru not_active IP Right Cessation
- 2007-07-10 EP EP07787319A patent/EP2038171B1/de not_active Not-in-force
- 2007-07-10 BR BRPI0712881-9A patent/BRPI0712881A2/pt not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| DE102006032003A1 (de) | 2008-01-24 |
| RU2009103772A (ru) | 2010-08-20 |
| CA2656794A1 (en) | 2008-01-17 |
| EP2038171A1 (de) | 2009-03-25 |
| JP2009542520A (ja) | 2009-12-03 |
| JP5257996B2 (ja) | 2013-08-07 |
| CN101495367A (zh) | 2009-07-29 |
| CN101495367B (zh) | 2013-04-24 |
| US20090289144A1 (en) | 2009-11-26 |
| US7963485B2 (en) | 2011-06-21 |
| WO2008006831A1 (en) | 2008-01-17 |
| RU2448019C2 (ru) | 2012-04-20 |
| BRPI0712881A2 (pt) | 2012-10-09 |
| DE102006032003B4 (de) | 2015-10-22 |
| EP2038171B1 (de) | 2011-09-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BRPI0911484A2 (pt) | asa de sustentação para uma aeronave | |
| IT1391165B1 (it) | Sistema di controllo aerodinamico per elicottero a pale controrotanti mediante superfici orientabili e senza variazione ciclica del passo | |
| WO2014158295A3 (en) | High-wing-aircraft fuselage support structure | |
| BR112018009344A2 (en) | air vehicle with folding components | |
| BRPI0920950A2 (pt) | aeronave e método de controlar a direção a direção de vôo de uma aeronave | |
| EP2625098A4 (de) | Flugzeug mit tragflächen und beweglichen propellern | |
| WO2009130467A3 (en) | A wind turbine blade | |
| WO2015007259A3 (de) | Veränderbares flügelprofil | |
| BRPI0915207A2 (pt) | dispositivo para formação de vórtices aerodinâmicos, bem como flape de regulagem e asa de sustentação com um dispositivo para formação de vórtices aerodinâmicos | |
| BR112012026076A2 (pt) | aeronave com uma estrutura de deformação absorvedora de energia integrada e aeronave com uma fuselagem desse tipo | |
| FR2933953B1 (fr) | Avion a empennage vertical a surface variable | |
| EP2735503A3 (de) | Modularer Strukturaufbau | |
| BRPI0810569A2 (pt) | elemento estrutural de fuselagem de uma aeronave | |
| FR2992626B1 (fr) | Plateforme semi-submersible a aileron stabilisateur, et centrale houlomotrice offshore integrant une telle plateforme | |
| GB201306712D0 (en) | Combined stairway and lift installation | |
| ES2462520T8 (es) | Un método de fabricación de mástiles, largueros y vigas de fuselaje que tienen sección transversal variable en forma de H | |
| IL239205A0 (en) | An airplane with vertical takeoff and landing | |
| FR2975666B1 (fr) | Aeronef a partie arriere orientable | |
| WO2014121344A3 (en) | Stair modules which co operate to form a temporary stair case | |
| GB201301748D0 (en) | Aircraft for Vertical Take-off and Landing with a Wing Arrangement comprising an extendible lift increasing system | |
| ATE542739T1 (de) | Flugzeugflügel | |
| Zhao | Flutter suppression of a high aspect-ratio wing with multiple control surfaces | |
| ATE380364T1 (de) | Elektrischer flugregler für flugzeughöhenruder | |
| GB2510412B (en) | Aircraft landing gear pitch trimmer actuator with variable damping | |
| WO2014104931A3 (ru) | Трансформируемая площадка |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |