EP0834717A3 - Dispositif de manoeuvre pour changer la position des ailettes de guidage d'un missile guidé - Google Patents

Dispositif de manoeuvre pour changer la position des ailettes de guidage d'un missile guidé Download PDF

Info

Publication number: EP0834717A3
Authority: EP; European Patent Office
Prior art keywords: rudder; driven; drive wheels; guided missile; changing
Prior art date: 1996-10-01
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

EP97116925A

Other languages

German (de)

English (en)

Other versions

EP0834717B1 (fr

EP0834717A2 (fr

Inventor

Hans-Günter Ing. Ullrich

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.)

LFK Lenkflugkoerpersysteme GmbH

Original Assignee

LFK Lenkflugkoerpersysteme GmbH

Daimler Benz Aerospace AG

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.)

1996-10-01

Filing date

1997-09-30

Publication date

1999-05-06

1997-09-30 Application filed by LFK Lenkflugkoerpersysteme GmbH, Daimler Benz Aerospace AG filed Critical LFK Lenkflugkoerpersysteme GmbH

1998-04-08 Publication of EP0834717A2 publication Critical patent/EP0834717A2/fr

1999-05-06 Publication of EP0834717A3 publication Critical patent/EP0834717A3/fr

2000-12-13 Application granted granted Critical

2000-12-13 Publication of EP0834717B1 publication Critical patent/EP0834717B1/fr

2017-09-30 Anticipated expiration legal-status Critical

Status 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)
Retarders (AREA)
Toys (AREA)
Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

EP97116925A 1996-10-01 1997-09-30 Dispositif de manoeuvre pour changer la position des ailettes de guidage d'un missile guidé Expired - Lifetime EP0834717B1 (fr)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
DE19640540A DE19640540C1 (de)	1996-10-01	1996-10-01	Ruderstellsystem für einen Lenkflugkörper
DE19640540		1996-10-01

Publications (3)

Publication Number	Publication Date
EP0834717A2 EP0834717A2 (fr)	1998-04-08
EP0834717A3 true EP0834717A3 (fr)	1999-05-06
EP0834717B1 EP0834717B1 (fr)	2000-12-13

Family

ID=7807603

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
EP97116925A Expired - Lifetime EP0834717B1 (fr)	1996-10-01	1997-09-30	Dispositif de manoeuvre pour changer la position des ailettes de guidage d'un missile guidé

Country Status (3)

Country	Link
US (1)	US5975461A (fr)
EP (1)	EP0834717B1 (fr)
DE (2)	DE19640540C1 (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US6073880A (en) *	1998-05-18	2000-06-13	Versatron, Inc.	Integrated missile fin deployment system
AUPR303501A0 (en) *	2001-02-09	2001-03-08	Kusic, Tom	Spiralling missile
US6502785B1 (en)	1999-11-17	2003-01-07	Lockheed Martin Corporation	Three axis flap control system
US6708923B2 (en)	2000-06-26	2004-03-23	Tom Kusic	Aircraft spiralling mechanism
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
ITMI20010648A1 (it) *	2001-03-27	2002-09-27	Finmeccanica S P A Alenia Dife	Gruppo di controllo per alette direzionali di missili e/o proiettili
AUPR583001A0 (en)	2001-06-20	2001-07-12	Kusic, Tom	Aircraft spiralling mechanism
US7093791B2 (en) *	2001-06-22	2006-08-22	Tom Kusic	Aircraft spiralling mechanism—c
US7635104B1 (en)	2001-06-22	2009-12-22	Tom Kusic	Aircraft spiraling mechanism with jet assistance—B
US7165742B2 (en) *	2001-06-22	2007-01-23	Tom Kusic	Aircraft spiralling mechanism - B
US7637453B2 (en) *	2001-06-22	2009-12-29	Tom Kusic	Aircraft spiraling mechanism with jet assistance - A
US6637699B2 (en)	2002-03-25	2003-10-28	Lockheed Martin Corporation	Method and apparatus for controlling a trajectory of a projectile
KR100470820B1 (ko) *	2002-04-19	2005-02-21	한국항공우주연구원	로켓 발사대
DE102004061977B4 (de) *	2004-12-23	2008-04-10	Lfk-Lenkflugkörpersysteme Gmbh	Klein-Flugkörper
FR2895496B1 (fr) *	2005-12-26	2008-03-28	Giat Ind Sa	Dispositif de mesure de la position angulaire d'une ailette ou gouverne d'un projectile et procede de montage d'un tel dispositif
US7642491B2 (en) *	2007-03-19	2010-01-05	Tom Kusic	Aircraft spiraling mechanism with jet assistance—D
US7791007B2 (en) *	2007-06-21	2010-09-07	Woodward Hrt, Inc.	Techniques for providing surface control to a guidable projectile
USD599854S1 (en) *	2008-06-09	2009-09-08	Lockheed Martin Corporation	Writing instrument
US8530809B2 (en) *	2011-08-03	2013-09-10	Raytheon Company	Ring gear control actuation system for air-breathing rocket motors
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
US11300390B1 (en)	2018-03-05	2022-04-12	Dynamic Structures And Materials, Llc	Control surface deployment apparatus and method of use
KR101892900B1 (ko) *	2018-04-26	2018-08-28	국방과학연구소	유도탄 조종날개의 위치정확도 측정장치 및 측정방법
DE102018133113A1 (de) *	2018-12-20	2020-06-25	Rheinmetall Air Defence Ag	Lenkflugkörper mit mehreren mittels einer Antriebsanordnung drehbaren Flügeln mit mindestens einem Aktuator und mindestens einem Planetengetriebe
IL277997B2 (en) *	2020-10-01	2024-08-01	Rafael Advanced Defense Systems Ltd	Aileron control operating system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE6606456U (de) *	1963-06-14	1970-09-24	Telefunken Patent	Vorrichtung zur verstellung des steuerorgans eines lenkflugkoerpers
US4274610A (en) *	1978-07-14	1981-06-23	General Dynamics, Pomona Division	Jet tab control mechanism for thrust vector control
US4438893A (en) *	1973-08-10	1984-03-27	Sanders Associates, Inc.	Prime power source and control for a guided projectile
JPH01300199A (ja) *	1988-05-27	1989-12-04	Mitsubishi Electric Corp	後翼操舵誘導飛しよう体
DE3827590A1 (de) *	1988-08-13	1990-02-22	Messerschmitt Boelkow Blohm	Flugkoerper

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4029270A (en) *	1975-08-11	1977-06-14	General Dynamics Corporation	Mechanical roll rate stabilizer for a rolling missile
US5806791A (en) *	1995-05-26	1998-09-15	Raytheon Company	Missile jet vane control system and method
US5829715A (en) *	1996-04-19	1998-11-03	Lockheed Martin Vought Systems Corp.	Multi-axis unfolding mechanism with rate controlled synchronized movement
US5662290A (en) *	1996-07-15	1997-09-02	Versatron Corporation	Mechanism for thrust vector control using multiple nozzles

1996
- 1996-10-01 DE DE19640540A patent/DE19640540C1/de not_active Expired - Fee Related
1997
- 1997-09-30 EP EP97116925A patent/EP0834717B1/fr not_active Expired - Lifetime
- 1997-09-30 DE DE59702755T patent/DE59702755D1/de not_active Expired - Lifetime
- 1997-09-30 US US08/941,581 patent/US5975461A/en not_active Expired - Lifetime

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE6606456U (de) *	1963-06-14	1970-09-24	Telefunken Patent	Vorrichtung zur verstellung des steuerorgans eines lenkflugkoerpers
US4438893A (en) *	1973-08-10	1984-03-27	Sanders Associates, Inc.	Prime power source and control for a guided projectile
US4274610A (en) *	1978-07-14	1981-06-23	General Dynamics, Pomona Division	Jet tab control mechanism for thrust vector control
JPH01300199A (ja) *	1988-05-27	1989-12-04	Mitsubishi Electric Corp	後翼操舵誘導飛しよう体
DE3827590A1 (de) *	1988-08-13	1990-02-22	Messerschmitt Boelkow Blohm	Flugkoerper

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 14, no. 87 (M - 0937) 19 February 1990 (1990-02-19) *

Also Published As

Publication number	Publication date
DE19640540C1 (de)	1998-04-02
EP0834717B1 (fr)	2000-12-13
US5975461A (en)	1999-11-02
DE59702755D1 (de)	2001-01-18
EP0834717A2 (fr)	1998-04-08

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1999-01-07	RAP1	Party data changed (applicant data changed or rights of an application transferred)	Owner name: LFK LENKFLUGKOERPERSYSTEME GMBH
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