EP0838656A3 - Lenkflugkörper mit Staustrahlantrieb - Google Patents

Lenkflugkörper mit Staustrahlantrieb Download PDF

Info

Publication number
EP0838656A3
EP0838656A3 EP97114018A EP97114018A EP0838656A3 EP 0838656 A3 EP0838656 A3 EP 0838656A3 EP 97114018 A EP97114018 A EP 97114018A EP 97114018 A EP97114018 A EP 97114018A EP 0838656 A3 EP0838656 A3 EP 0838656A3
Authority
EP
European Patent Office
Prior art keywords
guided missile
drive unit
rudder
drive
missile
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.)
Granted
Application number
EP97114018A
Other languages
English (en)
French (fr)
Other versions
EP0838656B1 (de
EP0838656A2 (de
Inventor
Walter Dipl.-Ing. Hetzer
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 Defence and Space GmbH
Original Assignee
LFK Lenkflugkoerpersysteme 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
Application filed by LFK Lenkflugkoerpersysteme GmbH filed Critical LFK Lenkflugkoerpersysteme GmbH
Publication of EP0838656A2 publication Critical patent/EP0838656A2/de
Publication of EP0838656A3 publication Critical patent/EP0838656A3/de
Application granted granted Critical
Publication of EP0838656B1 publication Critical patent/EP0838656B1/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)
  • Transmission Devices (AREA)

Abstract

Lenkflugkörper mit Staustrahlantrieb, mit einem den Zellenquerschnitt ausfüllenden Triebwerk, mit zwei äußeren Lufteinläufen im unteren Zellenbereich, welche mit Nachlaufschächten bis zum Heck führen, mit einem Heckleitwerk aus vier separat schwenkbaren Rudern in Form eines Diagonalkreuzes und mit einer starten Flügelanordnung in Flugkörpermitte oder vorderhalb.
Zu jedem Ruder ist eine Antriebseinheit mit Linearbewegung vorhanden.
In jedem Nachlaufschacht sind zwei Antriebseinheiten in Längs- und Umfangsrichtung des Lenkflugkörpers versetzt längs angeordnet.
Die kinematische Verbindung von der Antriebseinheit zum unteren Ruder bildet je eine Koppelstange mit Gelenken an beiden Enden.
Die kinematische Verbindung von der Antriebseinheit zum oberen Ruder bilden jeweils ein schwenkbarer Doppelhebel und eine Koppelstange mit Kugelgelenken an beiden Enden.
EP97114018A 1996-09-04 1997-08-14 Lenkflugkörper mit Staustrahlantrieb Expired - Lifetime EP0838656B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19635847A DE19635847C2 (de) 1996-09-04 1996-09-04 Lenkflugkörper mit Staustrahlantrieb
DE19635847 1996-09-04

Publications (3)

Publication Number Publication Date
EP0838656A2 EP0838656A2 (de) 1998-04-29
EP0838656A3 true EP0838656A3 (de) 2000-01-19
EP0838656B1 EP0838656B1 (de) 2002-02-13

Family

ID=7804584

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97114018A Expired - Lifetime EP0838656B1 (de) 1996-09-04 1997-08-14 Lenkflugkörper mit Staustrahlantrieb

Country Status (3)

Country Link
US (1) US5904319A (de)
EP (1) EP0838656B1 (de)
DE (2) DE19635847C2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE10007120B4 (de) * 2000-02-17 2007-04-12 LFK Lenkflugkörpersysteme GmbH Stromregelung permanenterregter Synchronmotoren für Lenkflugkörper mit elektromechanischem Ruderstellantrieb
DE10149087B4 (de) * 2000-10-07 2008-04-03 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Ruderblattansteuerung für Flugkörper
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
US6948685B2 (en) 2003-10-27 2005-09-27 Hr Textron, Inc. Locking device with solenoid release pin
US7410120B2 (en) * 2005-01-21 2008-08-12 The Boeing Company Control surface assemblies with torque tube base
US7195197B2 (en) * 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
IL167721A (en) * 2005-03-29 2008-06-05 Israel Aerospace Ind Ltd Steering system and method for guided flying apparatus
DE102009007731A1 (de) * 2009-02-05 2010-08-19 Lfk-Lenkflugkörpersysteme Gmbh Flugabbruchvorrichtung für einen Flugkörper
WO2012003025A2 (en) * 2010-04-07 2012-01-05 Bae Systems Information And Electronic Systems Integration Inc. Wing slot seal
US8530809B2 (en) 2011-08-03 2013-09-10 Raytheon Company Ring gear control actuation system for air-breathing rocket motors
DE102015005135A1 (de) 2015-04-22 2016-10-27 Diehl Bgt Defence Gmbh & Co. Kg Flugkörperrudersystem
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3154015A (en) * 1962-09-19 1964-10-27 Martin Marietta Corp Missile flight control system
US4327886A (en) * 1972-11-30 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Integral rocket ramjet missile
US4560121A (en) * 1983-05-17 1985-12-24 The Garrett Corporation Stabilization of automotive vehicle
DE3441533A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Kopplungseinrichtung zwischen einem linear-stellglied und einem schwenkelement, insbesondere einem steuerruder
DE4135557A1 (de) * 1991-10-29 1993-05-06 Diehl Gmbh & Co, 8500 Nuernberg, De Ruderstelleinrichtung
EP0636852A1 (de) * 1993-07-28 1995-02-01 DIEHL GMBH & CO. Mittels Canard-Rudern gesteuerte Artillerie-Rakete

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3373955A (en) * 1964-05-25 1968-03-19 Huska Paul Pitch and yaw actuator assembly for vehicle guidance surfaces
US5393011A (en) * 1965-12-03 1995-02-28 Shorts Missile Systems Limited Control systems for moving bodies
US4327885A (en) * 1971-10-06 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Thrust augmented rocket
US3901028A (en) * 1972-09-13 1975-08-26 Us Air Force Ramjet with integrated rocket boost motor
US4417441A (en) * 1979-03-29 1983-11-29 Messerschmitt-Bokow-Blohm Gesellschaft mit beschrankter Haftung Ram jet engine
US4369940A (en) * 1979-12-17 1983-01-25 Mcdonnell Douglas Corporation Airbreathing propulsion system for supersonic vehicles
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
DE3441534A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Lageranordnung fuer das ruderblatt eines flugkoerpers
FR2629136B1 (fr) * 1985-09-17 1990-11-09 Aerospatiale Statoreacteur pourvu d'une pluralite de manches d'alimentation en air carbure et missile pourvu d'un tel statoreacteur
FR2631387B1 (fr) * 1988-05-10 1990-07-13 Poudres & Explosifs Ste Nale Propulseur sans tuyere de faible allongement
JPH03199198A (ja) * 1989-12-28 1991-08-30 Shin Etsu Chem Co Ltd ランタンガレート単結晶およびその製造方法
US5505408A (en) * 1993-10-19 1996-04-09 Versatron Corporation Differential yoke-aerofin thrust vector control system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3154015A (en) * 1962-09-19 1964-10-27 Martin Marietta Corp Missile flight control system
US4327886A (en) * 1972-11-30 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Integral rocket ramjet missile
US4560121A (en) * 1983-05-17 1985-12-24 The Garrett Corporation Stabilization of automotive vehicle
DE3441533A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Kopplungseinrichtung zwischen einem linear-stellglied und einem schwenkelement, insbesondere einem steuerruder
DE4135557A1 (de) * 1991-10-29 1993-05-06 Diehl Gmbh & Co, 8500 Nuernberg, De Ruderstelleinrichtung
EP0636852A1 (de) * 1993-07-28 1995-02-01 DIEHL GMBH & CO. Mittels Canard-Rudern gesteuerte Artillerie-Rakete

Also Published As

Publication number Publication date
DE59706370D1 (de) 2002-03-21
EP0838656B1 (de) 2002-02-13
DE19635847A1 (de) 1998-03-12
EP0838656A2 (de) 1998-04-29
DE19635847C2 (de) 1998-07-16
US5904319A (en) 1999-05-18

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