DE60220476D1 - Anordnung einer Ausgangswelle für das Steuersystem einer Rakete - Google Patents

Anordnung einer Ausgangswelle für das Steuersystem einer Rakete

Info

Publication number
DE60220476D1
DE60220476D1 DE60220476T DE60220476T DE60220476D1 DE 60220476 D1 DE60220476 D1 DE 60220476D1 DE 60220476 T DE60220476 T DE 60220476T DE 60220476 T DE60220476 T DE 60220476T DE 60220476 D1 DE60220476 D1 DE 60220476D1
Authority
DE
Germany
Prior art keywords
rocket
arrangement
control system
output shaft
shaft
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
DE60220476T
Other languages
English (en)
Other versions
DE60220476T2 (de
Inventor
Gary H Johnson
Christopher P Owan
William M Hatalsky
Wayne Lee Sunne
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.)
Raytheon Co
Original Assignee
Raytheon 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 Raytheon Co filed Critical Raytheon Co
Application granted granted Critical
Publication of DE60220476D1 publication Critical patent/DE60220476D1/de
Publication of DE60220476T2 publication Critical patent/DE60220476T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Support Of The Bearing (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
DE60220476T 2001-05-11 2002-05-09 Anordnung einer Ausgangswelle für das Steuersystem einer Rakete Expired - Lifetime DE60220476T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/854,273 US6474594B1 (en) 2001-05-11 2001-05-11 Output shaft assembly for a missile control actuation unit
US854273 2001-05-11

Publications (2)

Publication Number Publication Date
DE60220476D1 true DE60220476D1 (de) 2007-07-19
DE60220476T2 DE60220476T2 (de) 2008-01-31

Family

ID=25318212

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60220476T Expired - Lifetime DE60220476T2 (de) 2001-05-11 2002-05-09 Anordnung einer Ausgangswelle für das Steuersystem einer Rakete

Country Status (3)

Country Link
US (1) US6474594B1 (de)
EP (1) EP1256777B1 (de)
DE (1) DE60220476T2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE518657C2 (sv) * 2000-07-03 2002-11-05 Bofors Defence Ab Fenstabiliserad styrbar projektil
SE521445C2 (sv) * 2001-03-20 2003-11-04 Bofors Defence Ab Sätt att synkronisera fenutfällningen vid en fenstabiliserad artillerigranat samt en i enlighet därmed utformad artillerigranat
US6637699B2 (en) * 2002-03-25 2003-10-28 Lockheed Martin Corporation Method and apparatus for controlling a trajectory of a projectile
US7219579B2 (en) * 2004-03-10 2007-05-22 Lockheed Martin Corporation Apparatus and method for actuating control surfaces
US7195197B2 (en) * 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
US8080772B2 (en) * 2007-11-02 2011-12-20 Honeywell International Inc. Modular, harnessless electromechanical actuation system assembly
US7781709B1 (en) * 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
EP2884865B1 (de) 2012-08-20 2017-12-27 Forever Mount, LLC Lötverbindung zur befestigung von edelsteinen
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

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4037806A (en) * 1964-09-16 1977-07-26 General Dynamics Corporation Control system for rolling missile with target seeker head
SE331242B (de) * 1969-05-14 1970-12-14 Bofors Ab
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
US4568041A (en) 1984-03-19 1986-02-04 The United States Of America As Represented By The Secretary Of The Navy Fin attachment
DE3441534A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Lageranordnung fuer das ruderblatt eines flugkoerpers
US4884766A (en) * 1988-05-25 1989-12-05 The United States Of America As Represented By The Secretary Of The Air Force Automatic fin deployment mechanism
DE4019482A1 (de) * 1990-06-19 1992-01-09 Diehl Gmbh & Co Ruderstelleinrichtung
US5593109A (en) * 1995-01-10 1997-01-14 Lucas Western, Inc. Actuator system and method
US6250584B1 (en) * 1999-10-18 2001-06-26 Hr Textron, Inc. Missile fin locking mechanism
DE19960738C1 (de) * 1999-12-16 2001-08-23 Lfk Gmbh Ruderanbindung für Lenkflugkörper

Also Published As

Publication number Publication date
US6474594B1 (en) 2002-11-05
DE60220476T2 (de) 2008-01-31
EP1256777B1 (de) 2007-06-06
EP1256777A3 (de) 2003-10-22
US20020166921A1 (en) 2002-11-14
EP1256777A2 (de) 2002-11-13

Similar Documents

Publication Publication Date Title
DE69919672D1 (de) Stator für Axiallüfter
DE60127756D1 (de) Fluid-Regelung für Schubdüsen
DE69911573D1 (de) Automatische Regelvorrichtung für das Statorschaufelspiel einer Gasturbine
DE60117200D1 (de) Steueranordnung für Kanalverbindungen
DE69824817D1 (de) Schwingungsgedämpfte Turbomaschinenschaufel
DE69936176D1 (de) Berstschutzring für Turbinen
DE19882569T1 (de) Steuerung für einen Wechselstrommotor
ATE348954T1 (de) Luftdichteabhängige leistungsregelung für eine windturbine
ITTO20010505A0 (it) Turbina a geometria variabile.
ITTO20010506A0 (it) Turbina a geometria variabile.
DE60302077D1 (de) Befestiganordnung für den Statorring einer Turbomaschine
DE69820207D1 (de) Rotor für gasturbinen
DE60036518D1 (de) Axialturbinen
ATE365276T1 (de) Mehrachsige turbine
DE69504926D1 (de) Steuerung für ein hilfskraftbetätigtes Schaltgetriebe
DE60137099D1 (de) Kühlstruktur für das Endstück einer Gasturbinenbrennkammer
DE60220476D1 (de) Anordnung einer Ausgangswelle für das Steuersystem einer Rakete
DE60300388D1 (de) Gasturbinentriebwerksregelungssystem
DE59912034D1 (de) Axialturbine
FR2825758B1 (fr) Liaison arbre-moyeu
DE69911025D1 (de) Axiale schaufelblattfixierung für einen turbinenrotor
DE69935253D1 (de) Numerisches steuerverfahren für universalmotoren, insbesondere für haushaltsanwendungen
DE10193306T1 (de) Integriertes Kraftübertragungsvorrichtungssteuersystem für Grosse Motoren
ITTO20010444A0 (it) Turbina assiale per applicazioni aeronautiche.
DE59910579D1 (de) Steuerelement für Fluid

Legal Events

Date Code Title Description
8364 No opposition during term of opposition