DE602005008820D1 - Vorrichtung und Verfahren zur Reduzierung der Lasten auf eine Rumpfstruktur von Transportmitteln - Google Patents

Vorrichtung und Verfahren zur Reduzierung der Lasten auf eine Rumpfstruktur von Transportmitteln

Info

Publication number
DE602005008820D1
DE602005008820D1 DE602005008820T DE602005008820T DE602005008820D1 DE 602005008820 D1 DE602005008820 D1 DE 602005008820D1 DE 602005008820 T DE602005008820 T DE 602005008820T DE 602005008820 T DE602005008820 T DE 602005008820T DE 602005008820 D1 DE602005008820 D1 DE 602005008820D1
Authority
DE
Germany
Prior art keywords
transport
fuselage structure
loads
reducing
reduction
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.)
Active
Application number
DE602005008820T
Other languages
English (en)
Inventor
Michael Enzinger
Michael Kordt
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 GmbH
Original Assignee
Airbus Operations GmbH
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
Priority claimed from DE102004029196A external-priority patent/DE102004029196B4/de
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of DE602005008820D1 publication Critical patent/DE602005008820D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0066—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for limitation of acceleration or stress
    • 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
    • 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
DE602005008820T 2004-06-16 2005-06-16 Vorrichtung und Verfahren zur Reduzierung der Lasten auf eine Rumpfstruktur von Transportmitteln Active DE602005008820D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004029196A DE102004029196B4 (de) 2004-06-16 2004-06-16 System zur Rumpfstrukturlastabminderung in Verkehrsmitteln
US60666504P 2004-09-02 2004-09-02

Publications (1)

Publication Number Publication Date
DE602005008820D1 true DE602005008820D1 (de) 2008-09-25

Family

ID=34937502

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005008820T Active DE602005008820D1 (de) 2004-06-16 2005-06-16 Vorrichtung und Verfahren zur Reduzierung der Lasten auf eine Rumpfstruktur von Transportmitteln

Country Status (4)

Country Link
EP (1) EP1607326B1 (de)
AT (1) ATE404427T1 (de)
CA (1) CA2510117A1 (de)
DE (1) DE602005008820D1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE102010001102A1 (de) 2009-11-06 2011-05-12 Becker Marine Systems Gmbh & Co. Kg Anordnung zur Ermittlung einer auf ein Ruder wirkenden Kraft

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5072893A (en) * 1987-05-28 1991-12-17 The Boeing Company Aircraft modal suppression system
US5667166A (en) * 1995-01-12 1997-09-16 The Boeing Company Aircraft frequency adaptive modal suppression system
DE19925982B4 (de) * 1999-06-08 2004-09-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Drehflügler mit einer Zelle, an der ein Hauptrotor und ein Heckausleger für einen Heckrotor gelagert sind
US6915989B2 (en) * 2002-05-01 2005-07-12 The Boeing Company Aircraft multi-axis modal suppression system

Also Published As

Publication number Publication date
CA2510117A1 (en) 2005-12-16
EP1607326B1 (de) 2008-08-13
EP1607326A1 (de) 2005-12-21
ATE404427T1 (de) 2008-08-15

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE