AU2239901A - Arrangement in a rudder for an aircraft or watercraft - Google Patents

Arrangement in a rudder for an aircraft or watercraft

Info

Publication number
AU2239901A
AU2239901A AU22399/01A AU2239901A AU2239901A AU 2239901 A AU2239901 A AU 2239901A AU 22399/01 A AU22399/01 A AU 22399/01A AU 2239901 A AU2239901 A AU 2239901A AU 2239901 A AU2239901 A AU 2239901A
Authority
AU
Australia
Prior art keywords
watercraft
rudder
aircraft
arrangement
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.)
Abandoned
Application number
AU22399/01A
Inventor
Patrick Berry
Jubin Ghassabei
Krister Karling
Karin Kruhsberg
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.)
Saab AB
Original Assignee
Saab AB
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
Application filed by Saab AB filed Critical Saab AB
Publication of AU2239901A publication Critical patent/AU2239901A/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/38—Rudders
    • B63H25/381—Rudders with flaps
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steering Devices For Bicycles And Motorcycles (AREA)
  • Toys (AREA)
  • Mechanical Control Devices (AREA)
AU22399/01A 1999-12-20 2000-11-29 Arrangement in a rudder for an aircraft or watercraft Abandoned AU2239901A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE9904657A SE9904657L (en) 1999-12-20 1999-12-20 Device at a rudder for an air or watercraft
SE9904657 1999-12-20
PCT/SE2000/002368 WO2001046008A1 (en) 1999-12-20 2000-11-29 Arrangement in a rudder for an aircraft or watercraft

Publications (1)

Publication Number Publication Date
AU2239901A true AU2239901A (en) 2001-07-03

Family

ID=20418193

Family Applications (1)

Application Number Title Priority Date Filing Date
AU22399/01A Abandoned AU2239901A (en) 1999-12-20 2000-11-29 Arrangement in a rudder for an aircraft or watercraft

Country Status (3)

Country Link
AU (1) AU2239901A (en)
SE (1) SE9904657L (en)
WO (1) WO2001046008A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9108715B2 (en) 2012-05-29 2015-08-18 The Boeing Company Rotary actuated high lift gapped aileron
CN108082449B (en) * 2018-03-06 2022-06-10 中航通飞华南飞机工业有限公司 Large aircraft control surface suspension structure
CN112498661B (en) * 2020-12-04 2024-01-30 中国航空工业集团公司沈阳飞机设计研究所 Multifunctional control surface structure
GB2620625A (en) * 2022-07-14 2024-01-17 Airbus Operations Ltd Aircraft wing trailing edge device

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1506615A1 (en) * 1967-06-12 1969-08-28 Ver Flugtechnische Werke Control flap training and arrangement on a profile of an aircraft
US4705236A (en) * 1981-09-29 1987-11-10 The Boeing Company Aileron system for aircraft and method of operating the same
DE4334680C2 (en) * 1993-10-12 1996-07-11 Daimler Benz Aerospace Airbus Device for adjusting gap control flaps
SE506264C2 (en) * 1996-03-08 1997-11-24 Saab Ab Bidirectional Column Rudder

Also Published As

Publication number Publication date
WO2001046008A1 (en) 2001-06-28
SE9904657D0 (en) 1999-12-20
SE513583C2 (en) 2000-10-02
SE9904657L (en) 2000-10-02

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase