DE3676506D1 - Aktives steuersystem eines flugzeuges mit biegsamem fluegel. - Google Patents
Aktives steuersystem eines flugzeuges mit biegsamem fluegel.Info
- Publication number
- DE3676506D1 DE3676506D1 DE8686111669T DE3676506T DE3676506D1 DE 3676506 D1 DE3676506 D1 DE 3676506D1 DE 8686111669 T DE8686111669 T DE 8686111669T DE 3676506 T DE3676506 T DE 3676506T DE 3676506 D1 DE3676506 D1 DE 3676506D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- control system
- active control
- bendable wing
- bendable
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- 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
-
- 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
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Mechanical Control Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP86111669A EP0257123B1 (de) | 1986-08-22 | 1986-08-22 | Aktives Steuersystem eines Flugzeuges mit biegsamem Flügel |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3676506D1 true DE3676506D1 (de) | 1991-02-07 |
Family
ID=8195363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8686111669T Expired - Lifetime DE3676506D1 (de) | 1986-08-22 | 1986-08-22 | Aktives steuersystem eines flugzeuges mit biegsamem fluegel. |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0257123B1 (de) |
DE (1) | DE3676506D1 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6766981B2 (en) | 2002-10-25 | 2004-07-27 | Northrop Grumman Corporation | Control system for alleviating a gust load on an aircraft wing |
US9963223B2 (en) | 2011-01-14 | 2018-05-08 | Lockheed Martin Corporation | Aerodynamic force sensing apparatus |
CN102393749B (zh) * | 2011-10-20 | 2014-04-02 | 西北工业大学 | 一种确定多操纵面飞机起飞着陆阶段各操纵面使用优先级的方法 |
CN102431652B (zh) * | 2011-10-20 | 2013-08-28 | 西北工业大学 | 一种确定多操纵面飞机近距阶段各操纵面使用优先级的方法 |
CN102390524B (zh) * | 2011-10-20 | 2013-08-28 | 西北工业大学 | 一种确定多操纵面飞机超视距阶段各操纵面使用优先级的方法 |
US20160200420A1 (en) * | 2014-09-25 | 2016-07-14 | Aurora Flight Sciences Corporation | System and method for unwanted force rejection and vehicle stability |
CN110705153B (zh) * | 2019-09-24 | 2023-09-05 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种无人机多阶安全系数取值方法 |
CN112109876B (zh) * | 2020-09-04 | 2022-01-14 | 北京航空航天大学 | 基于飞行器静气动弹性效应的形状主动控制方法和采用该方法的飞行器 |
CN112394739B (zh) * | 2020-10-29 | 2021-11-05 | 南京航空航天大学 | 主动变形四旋翼飞行器自抗扰飞行控制方法 |
CN115783241B (zh) * | 2023-02-08 | 2023-05-16 | 中国空气动力研究与发展中心计算空气动力研究所 | 融合体飞行器的异步偏转航向控制组合舵控制方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191216890A (en) * | 1911-07-27 | 1913-04-17 | Rumpler Luftfahrzeugbau G M B | Improvements in Aeroplane Steering. |
US4330100A (en) * | 1979-09-28 | 1982-05-18 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Means for controlling aerodynamically induced twist |
US4562546A (en) * | 1983-01-13 | 1985-12-31 | Rockwell International Corporation | Stability augmentation system for a forward swept wing aircraft |
-
1986
- 1986-08-22 DE DE8686111669T patent/DE3676506D1/de not_active Expired - Lifetime
- 1986-08-22 EP EP86111669A patent/EP0257123B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0257123B1 (de) | 1991-01-02 |
EP0257123A1 (de) | 1988-03-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE3762027D1 (de) | Fluegelklappensteuersystem eines flugzeuges. | |
DE68919732D1 (de) | Steuerungssystem eines Hubschraubers. | |
DE3887746D1 (de) | Blattbefestigung einer Flugzeugluftschraube. | |
DE3781941D1 (de) | Flugverwaltungssystem. | |
DE68919811D1 (de) | Flugzeuginstrumentensysteme. | |
NO863224L (no) | Foldevingkonstruksjon for fjernstyrt rakett eller prosjektil. | |
IT8721740A0 (it) | Controllo di spinta di aereo. | |
NO874474L (no) | Vinge for supersonisk vifte eller kompressor. | |
DE3673598D1 (de) | Geschwindigkeitsregler fuer einen stromerzeuger eines flugzeugs. | |
DE3677315D1 (de) | Flugzeugsteuersystem. | |
DE3683480D1 (de) | Instrument-landungssystem. | |
DE3676506D1 (de) | Aktives steuersystem eines flugzeuges mit biegsamem fluegel. | |
DE3778010D1 (de) | Rechnersystem mit moduskonvertierung von rechnerbefehlen. | |
IT8721738A0 (it) | Controllo di spinta di aereo. | |
DK163567C (da) | Siliconeoliefrit antiskummiddel til vandige systemer, antiskummiddelpraeparat fortyndet med vand eller organisk oploesningsmiddel samt fremgangsmaade til skumdaempning af vandige systemer | |
IT7921044A0 (it) | Dispositivo per la precisa condotta di volo e navigazione d'aereoplani. | |
FI860495A0 (fi) | Borste foer spridning av flytande aemne eller emulsion. | |
DE3860476D1 (de) | Landungssystem eines flugzeuges. | |
IT8620545A0 (it) | Controllo per eliche da aereo | |
DE68928110D1 (de) | Steuerungssystem für den Antrieb eines Luftfahrzeugs | |
FR2585326B3 (fr) | Configuration d'arriere de fuselage d'avion | |
DE3789293D1 (de) | System zur Landehilfe für Flugzeuge mit eigenem Bordradar. | |
DE3669475D1 (de) | Flugregelsystem. | |
IT1198021B (it) | Sistema di riduzione di rumore di eliche di aerei | |
FI873057A (fi) | Foerfarande foer framstaellning av homo - och blandpolymer av vinylklorid i emulsion eller mikrosuspension. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8365 | Fully valid after opposition proceedings |