FR2683033B1 - Dispositif de reglage de gouverne. - Google Patents

Dispositif de reglage de gouverne.

Info

Publication number
FR2683033B1
FR2683033B1 FR9212762A FR9212762A FR2683033B1 FR 2683033 B1 FR2683033 B1 FR 2683033B1 FR 9212762 A FR9212762 A FR 9212762A FR 9212762 A FR9212762 A FR 9212762A FR 2683033 B1 FR2683033 B1 FR 2683033B1
Authority
FR
France
Prior art keywords
adjustment device
governor adjustment
governor
adjustment
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 - Fee Related
Application number
FR9212762A
Other languages
English (en)
Other versions
FR2683033A1 (fr
Inventor
Gmbh Ÿ Co. Societe De Droit Allemand Diehl
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of FR2683033A1 publication Critical patent/FR2683033A1/fr
Application granted granted Critical
Publication of FR2683033B1 publication Critical patent/FR2683033B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • 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

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)
FR9212762A 1991-10-29 1992-10-27 Dispositif de reglage de gouverne. Expired - Fee Related FR2683033B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4135557A DE4135557C2 (de) 1991-10-29 1991-10-29 Ruderstelleinrichtung

Publications (2)

Publication Number Publication Date
FR2683033A1 FR2683033A1 (fr) 1993-04-30
FR2683033B1 true FR2683033B1 (fr) 1994-01-21

Family

ID=6443613

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9212762A Expired - Fee Related FR2683033B1 (fr) 1991-10-29 1992-10-27 Dispositif de reglage de gouverne.

Country Status (4)

Country Link
US (1) US5249761A (fr)
DE (1) DE4135557C2 (fr)
FR (1) FR2683033B1 (fr)
GB (1) GB2260954B (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4019482A1 (de) * 1990-06-19 1992-01-09 Diehl Gmbh & Co Ruderstelleinrichtung
DE4335785A1 (de) * 1993-10-20 1995-04-27 Diehl Gmbh & Co Ruderstelleinrichtung
IL107844A (en) * 1993-12-02 1996-06-18 Ministry Of Defence Armaments Flying object control system
US5449131A (en) * 1994-01-28 1995-09-12 Eidetics International, Inc. Vertical nose strake for aircraft stability and control
DE19624187C1 (de) * 1996-06-18 1998-01-15 Diehl Gmbh & Co Rakete
DE19635847C2 (de) * 1996-09-04 1998-07-16 Daimler Benz Aerospace Ag Lenkflugkörper mit Staustrahlantrieb
DE19922693A1 (de) * 1999-05-18 2000-11-23 Diehl Stiftung & Co Stelleinrichtung für Ruder eines Flugkörpers
DE19960738C1 (de) * 1999-12-16 2001-08-23 Lfk Gmbh Ruderanbindung für Lenkflugkörper
US6827310B1 (en) * 2003-09-22 2004-12-07 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for fin actuation in a portable missile
US20050211827A1 (en) * 2004-03-29 2005-09-29 The Boeing Company High speed missile wing and associated method
FR2872783B1 (fr) * 2004-07-09 2007-11-30 Mbda France Sa Dispositif de gouverne aerodynamique a moteur deporte
US8080772B2 (en) * 2007-11-02 2011-12-20 Honeywell International Inc. Modular, harnessless electromechanical actuation system assembly
FR2937704B1 (fr) * 2008-10-28 2011-07-08 Skf Aerospace France Ensemble de transmission d'efforts et ensemble de commande comprenant un tel ensemble
DE102009007731A1 (de) * 2009-02-05 2010-08-19 Lfk-Lenkflugkörpersysteme Gmbh Flugabbruchvorrichtung für einen Flugkörper
JP5727697B2 (ja) * 2009-09-30 2015-06-03 川崎重工業株式会社 飛翔体の操舵ユニット
US8921749B1 (en) 2013-07-10 2014-12-30 The United States Of America As Represented By The Secretary Of The Navy Perpendicular drive mechanism for a missile control actuation system
US9546853B2 (en) * 2014-08-05 2017-01-17 Raytheon Company Air vehicle with control system mechanical coupler
DE102015005135A1 (de) 2015-04-22 2016-10-27 Diehl Bgt Defence Gmbh & Co. Kg Flugkörperrudersystem
DE102015014794A1 (de) * 2015-08-25 2017-03-02 Diehl Bgt Defence Gmbh & Co. Kg Flügelanordnung und Flugkörper mit Flügelanordnung
EP3382248B1 (fr) * 2017-03-30 2020-04-29 Hamilton Sundstrand Corporation Mécanisme d'actionnement rotatif
US11300390B1 (en) 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
CN110254691A (zh) * 2019-07-05 2019-09-20 贵州航天控制技术有限公司 一种单舵机构及均布式电动舵机
US20240060552A1 (en) * 2022-08-17 2024-02-22 Raytheon Company Sliding pin-yoke mechanism

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US857551A (en) * 1906-03-22 1907-06-18 Otis Elevator Co Compound brake.
GB481413A (en) * 1937-04-22 1938-03-10 Alsacienne Constr Meca Improved safety device for screw-and-nut gearing
FR891349A (fr) * 1940-12-04 1944-03-03 Messerschmitt Ag Gouvernail de profondeur pour avion
US2714822A (en) * 1951-05-09 1955-08-09 Reliance Electric & Eng Co Sealable adjustable stop for sanitary variable speed transmission
US2944437A (en) * 1958-07-14 1960-07-12 Ferro Stamping Co Method of making feed screw stop
US3774462A (en) * 1972-04-20 1973-11-27 J Thompson Valve actuator
US4655420A (en) * 1983-06-09 1987-04-07 The United States Of America As Represented By The Secretary Of The Air Force Low height fin control actuator
DE3441533A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Kopplungseinrichtung zwischen einem linear-stellglied und einem schwenkelement, insbesondere einem steuerruder
DE3442899C1 (de) * 1984-11-24 1986-06-12 Dornier System Gmbh, 7990 Friedrichshafen Ruderantrieb
DE3702733A1 (de) * 1987-01-30 1988-08-11 Diehl Gmbh & Co Ruderstelleinrichtung
JPH0217799A (ja) * 1988-07-06 1990-01-22 Shicoh Eng Co Ltd 動電型電気音響交換器
JPH02168059A (ja) * 1988-12-19 1990-06-28 Fujitsu Ltd 揺動駆動機構
JP2917030B2 (ja) * 1989-09-12 1999-07-12 日本酸素株式会社 空気液化分離方法
GB9003260D0 (en) * 1990-02-13 1990-11-21 Normalair Garrett Ltd Lock means for missile control fins
US5098043A (en) * 1990-02-27 1992-03-24 Grumman Aerospace Corporation Integrated power hinge actuator
DE4009549A1 (de) * 1990-03-24 1991-09-26 Messerschmitt Boelkow Blohm Ruderantrieb
DE4019482A1 (de) * 1990-06-19 1992-01-09 Diehl Gmbh & Co Ruderstelleinrichtung

Also Published As

Publication number Publication date
GB9222217D0 (en) 1992-12-02
GB2260954A (en) 1993-05-05
GB2260954B (en) 1995-05-17
DE4135557C2 (de) 1999-05-06
US5249761A (en) 1993-10-05
DE4135557A1 (de) 1993-05-06
FR2683033A1 (fr) 1993-04-30

Similar Documents

Publication Publication Date Title
FR2683033B1 (fr) Dispositif de reglage de gouverne.
FR2681444B1 (fr) Dispositif electrochrome.
FR2668567B1 (fr) Dispositif de tension reglable elastiquement.
FR2666287B1 (fr) Dispositif de reglage d'epaule.
FR2685421B1 (fr) Dispositif de reglage de tension de courroie.
FR2662510B1 (fr) Dispositif de retenue d'un element annulaire.
DE69018921D1 (de) Verstellvorrichtung.
FR2682218B1 (fr) Dispositif de contacteur.
FR2671244B1 (fr) Dispositif de retard reglable.
FR2678093B1 (fr) Dispositif photorefractif.
DE59200289D1 (de) Justiervorrichtung.
FR2661966B1 (fr) Dispositif hydraulique de commande.
DE59004171D1 (de) Verstelleinrichtung.
FR2671245B1 (fr) Dispositif de retard reglable.
FR2652490B1 (fr) Dispositif.
FR2673280B1 (fr) Dispositif de surete.
FR2662425B1 (fr) Dispositif de distribution.
FR2680012B1 (fr) Dispositif de dispersion spectrale.
FR2677823B1 (fr) Dispositif amplificateur.
FR2680809B3 (fr) Dispositif de protection antisismique.
FR2657452B1 (fr) Dispositif de reglage de tete.
FR2654603B1 (fr) Dispositif pince-nappe.
FR2672914B1 (fr) Dispositif de pontage.
FR2668970B1 (fr) Dispositif distributeur de ressorts.
FR2684977B1 (fr) Dispositif de desempilage.

Legal Events

Date Code Title Description
ST Notification of lapse