FR2973774B1 - Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef. - Google Patents

Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.

Info

Publication number: FR2973774B1
Authority: FR; France
Prior art keywords: improving; aerodynamic efficiency; vertical aircraft; tension; aircraft tension
Prior art date: 2011-04-06
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.): Expired - Fee Related

Application number

FR1152980A

Other languages

English (en)

Other versions

FR2973774A1 (fr

Inventor

Alain Tanguy

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 SAS

Original Assignee

Airbus Operations 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.)

2011-04-06

Filing date

2011-04-06

Publication date

2015-05-08

2011-04-06 Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS

2011-04-06 Priority to FR1152980A priority Critical patent/FR2973774B1/fr

2012-04-04 Priority to US13/439,341 priority patent/US8783606B2/en

2012-04-06 Priority to CN201210109299.5A priority patent/CN102730184B/zh

2012-10-12 Publication of FR2973774A1 publication Critical patent/FR2973774A1/fr

2015-05-08 Application granted granted Critical

2015-05-08 Publication of FR2973774B1 publication Critical patent/FR2973774B1/fr

Status Expired - Fee Related legal-status Critical Current

2031-04-06 Anticipated expiration legal-status Critical

Links

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
- 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
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
- B64C2003/147—Aerofoil profile comprising trailing edges of particular shape
- 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

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Machines For Laying And Maintaining Railways (AREA)

FR1152980A 2011-04-06 2011-04-06 Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef. Expired - Fee Related FR2973774B1 (fr)

Priority Applications (3)

Application Number	Priority Date	Filing Date	Title
FR1152980A FR2973774B1 (fr)	2011-04-06	2011-04-06	Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.
US13/439,341 US8783606B2 (en)	2011-04-06	2012-04-04	Method for improving the aerodynamic efficiency of the vertical tail of an aircraft
CN201210109299.5A CN102730184B (zh)	2011-04-06	2012-04-06	用于提高飞行器的垂直尾翼的空气动力学效率的方法

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR1152980A FR2973774B1 (fr)	2011-04-06	2011-04-06	Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.

Publications (2)

Publication Number	Publication Date
FR2973774A1 FR2973774A1 (fr)	2012-10-12
FR2973774B1 true FR2973774B1 (fr)	2015-05-08

Family

ID=44549563

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR1152980A Expired - Fee Related FR2973774B1 (fr)	2011-04-06	2011-04-06	Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.

Country Status (3)

Country	Link
US (1)	US8783606B2 (fr)
CN (1)	CN102730184B (fr)
FR (1)	FR2973774B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2945790B1 (fr) *	2009-05-20	2011-07-22	Airbus France	Procede pour l'amelioration de l'efficacite aerodynamique de l'empennage vertical d'un aeronef.
FR2973774B1 (fr) *	2011-04-06	2015-05-08	Airbus Operations Sas	Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2070809A (en) *	1935-08-28	1937-02-16	Douglas Aircraft Co Inc	Control surface
CN1052084A (zh) *	1990-05-31	1991-06-12	邢麟祥	分动式翼型双垂尾
EP0488428A3 (en) *	1990-09-24	1992-10-14	The Boeing Company	Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts
US5692704A (en) *	1995-06-07	1997-12-02	Buttgereit; Volker	Body tail unit for a commercial aircraft
US6021977A (en) *	1997-06-27	2000-02-08	Mcdonnell Douglas Corporation	Vertical stabilizer fin assembly for an aircraft
DE10361391A1 (de) *	2003-12-29	2005-08-04	Airbus Deutschland Gmbh	Seitenleitwerksanschluss
CA2503275A1 (fr) *	2005-04-07	2006-10-07	Advanced Flow Technologies Inc.	Systeme, methode et dispositif pour mesure acoustique d'ecoulement des fluides
US7913949B2 (en) *	2007-06-11	2011-03-29	The Boeing Company	Symmetric leading edge device and method to delay flow separation
ES2335840B1 (es) *	2007-07-27	2011-02-18	Airbus España, S.L.	Empenaje de aeronave.
ES2345584B1 (es) *	2007-12-21	2011-07-18	Airbus Operations, S.L.	Superficie de control de aeronave.
FR2933953B1 (fr) *	2008-07-16	2011-04-29	Airbus France	Avion a empennage vertical a surface variable
ES2382062B1 (es) *	2008-12-04	2013-04-26	Airbus Operations, S.L.	Superficie estabilizadora y de control direccional de aeronave
ES2367935B1 (es) *	2008-12-18	2012-09-18	Airbus Operations, S.L.	Borde de salida de superficie estabilizadora de aeronave.
DE102009013758A1 (de) *	2009-03-17	2010-09-23	Airbus Deutschland Gmbh	Flugzeug mit einer Vorrichtung zur Beeinflussung der Richtungsstabilität des Flugzeugs sowie Verfahren zur Beeinflussung der Richtungsstabilität des Flugzeugs
FR2945790B1 (fr) *	2009-05-20	2011-07-22	Airbus France	Procede pour l'amelioration de l'efficacite aerodynamique de l'empennage vertical d'un aeronef.
CN101963499B (zh) *	2010-07-21	2012-10-10	中国航空工业集团公司西安飞机设计研究所	一种飞机舵面偏转角测量工具及测量方法
US9090326B2 (en) *	2010-10-13	2015-07-28	The Boeing Company	Active flow control on a vertical stabilizer and rudder
DE102010051216A1 (de) *	2010-11-12	2012-05-16	Airbus Operations Gmbh	Seitenrudersystem an einem Flugzeug
FR2973774B1 (fr) *	2011-04-06	2015-05-08	Airbus Operations Sas	Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.

2011
- 2011-04-06 FR FR1152980A patent/FR2973774B1/fr not_active Expired - Fee Related
2012
- 2012-04-04 US US13/439,341 patent/US8783606B2/en not_active Expired - Fee Related
- 2012-04-06 CN CN201210109299.5A patent/CN102730184B/zh not_active Expired - Fee Related

Also Published As

Publication number	Publication date
FR2973774A1 (fr)	2012-10-12
CN102730184B (zh)	2016-02-17
US8783606B2 (en)	2014-07-22
US20120256047A1 (en)	2012-10-11
CN102730184A (zh)	2012-10-17

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