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
Application number
DE8686111669T
Other languages
English (en)
Inventor
Jan Tulinius
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.)
Boeing North American Inc
Original Assignee
Rockwell International Corp
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=8195363&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE3676506(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rockwell International Corp filed Critical Rockwell International Corp
Application granted granted Critical
Publication of DE3676506D1 publication Critical patent/DE3676506D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)
DE8686111669T 1986-08-22 1986-08-22 Aktives steuersystem eines flugzeuges mit biegsamem fluegel. Expired - Lifetime DE3676506D1 (de)

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)

* Cited by examiner, † Cited by third party
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
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
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
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
EP0257123B1 (de) 1991-01-02
EP0257123A1 (de) 1988-03-02

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8365 Fully valid after opposition proceedings