DE69913602D1 - Flugzeug mit verminderter Flügelbelastung - Google Patents
Flugzeug mit verminderter FlügelbelastungInfo
- Publication number
- DE69913602D1 DE69913602D1 DE69913602T DE69913602T DE69913602D1 DE 69913602 D1 DE69913602 D1 DE 69913602D1 DE 69913602 T DE69913602 T DE 69913602T DE 69913602 T DE69913602 T DE 69913602T DE 69913602 D1 DE69913602 D1 DE 69913602D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- wing load
- reduced wing
- reduced
- load
- 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.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Feedback Control In General (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Handcart (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9805400 | 1998-04-29 | ||
FR9805400A FR2778163B1 (fr) | 1998-04-29 | 1998-04-29 | Aeronef a efforts de voilure diminues |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69913602D1 true DE69913602D1 (de) | 2004-01-29 |
DE69913602T2 DE69913602T2 (de) | 2004-12-23 |
Family
ID=9525830
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69913602T Expired - Lifetime DE69913602T2 (de) | 1998-04-29 | 1999-04-16 | Flugzeug mit verminderter Flügelbelastung |
Country Status (5)
Country | Link |
---|---|
US (1) | US6064923A (de) |
EP (1) | EP0953504B1 (de) |
CA (1) | CA2270752C (de) |
DE (1) | DE69913602T2 (de) |
FR (1) | FR2778163B1 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6915989B2 (en) * | 2002-05-01 | 2005-07-12 | The Boeing Company | Aircraft multi-axis modal suppression system |
CA2444560C (en) * | 2002-10-21 | 2008-09-23 | The Boeing Company | Method and apparatus for rotatably supporting movable components, including canards |
JP4490963B2 (ja) | 2003-02-15 | 2010-06-30 | ガルフストリーム・エアロスペース・コーポレイション | 航空機キャビン大気組成制御方法 |
US20050045764A1 (en) * | 2003-08-29 | 2005-03-03 | Supersonic Aerospace International, Llc | Canard position and dihedral for boom reduction and pitch/directional control |
EP2267569B1 (de) * | 2003-11-03 | 2019-05-08 | The Boeing Company | System zur Unterdrückung der Vibrationsmoden in Drehung auf mehreren Axen eines Flugzeugs |
US7367530B2 (en) * | 2005-06-21 | 2008-05-06 | The Boeing Company | Aerospace vehicle yaw generating systems and associated methods |
DE102005058081B9 (de) * | 2005-12-06 | 2009-01-29 | Airbus Deutschland Gmbh | Verfahren zur Rekonstruktion von Böen und Strukturlasten bei Flugzeugen, insbesondere Verkehrsflugzeugen |
CA2637331A1 (en) * | 2006-01-17 | 2007-07-26 | Gulfstream Aerospace Corporation | System and method for an integrated backup control system |
US7984878B2 (en) * | 2006-01-17 | 2011-07-26 | Gulfstream Aerospace Corporation | Apparatus and method for backup control in a distributed flight control system |
RU2503585C1 (ru) * | 2012-05-21 | 2014-01-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Уфимский государственный авиационный технический университет" | Система автоматического управления углом курса и ограничения нормальной перегрузки летательного аппарата |
US9878776B2 (en) * | 2014-05-15 | 2018-01-30 | The Boeing Company | System and method for optimizing horizontal tail loads |
EP3643605B1 (de) | 2018-10-25 | 2022-08-17 | Bombardier Inc. | System und verfahren zur verringerung der auswirkung einer erregung eines strukturellen flexiblen modus eines flugzeugs |
CN109823514B (zh) * | 2019-02-02 | 2021-01-12 | 北京航空航天大学 | 一种可调节安装角的易拆卸尾翼结构 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2906889C2 (de) | 1979-02-22 | 1986-06-26 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Flugzeug mit vor und hinter dem Schwerpunkt angeordneten Steuerflächen |
US4723214A (en) | 1985-02-15 | 1988-02-02 | Grumman Aerospace Corporation | Automatic camber control |
US4697768A (en) * | 1985-11-12 | 1987-10-06 | Grumman Aerospace Corporation | Flight control system employing complementary filter |
FR2656585B1 (fr) | 1989-12-28 | 1995-01-13 | Aerospatiale | Systeme pour diminuer les efforts appliques a la voilure et notamment a l'emplanture des ailes d'un aeronef en vol. |
US5056027A (en) * | 1990-02-26 | 1991-10-08 | Honeywell Inc. | Apparatus and method for a smooth transition between calibrated airspeed control of an aircraft and mach number control of an aircraft |
US5079711A (en) * | 1990-02-26 | 1992-01-07 | The Boeing Company | Aircraft high altitude vertical flight path and speed control system |
FR2719548B1 (fr) | 1994-05-03 | 1996-07-05 | Aerospatiale | Avion de transport à empennage avant. |
-
1998
- 1998-04-29 FR FR9805400A patent/FR2778163B1/fr not_active Expired - Fee Related
-
1999
- 1999-04-16 DE DE69913602T patent/DE69913602T2/de not_active Expired - Lifetime
- 1999-04-16 EP EP99400928A patent/EP0953504B1/de not_active Expired - Lifetime
- 1999-04-28 CA CA002270752A patent/CA2270752C/fr not_active Expired - Fee Related
- 1999-04-28 US US09/301,171 patent/US6064923A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US6064923A (en) | 2000-05-16 |
CA2270752A1 (fr) | 1999-10-29 |
FR2778163B1 (fr) | 2000-06-23 |
FR2778163A1 (fr) | 1999-11-05 |
CA2270752C (fr) | 2005-10-18 |
EP0953504A1 (de) | 1999-11-03 |
EP0953504B1 (de) | 2003-12-17 |
DE69913602T2 (de) | 2004-12-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |