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EP1054231A3 - Actuation system for an aerodynamic control surface of an air vehicle - Google Patents

Actuation system for an aerodynamic control surface of an air vehicle Download PDF

Info

Publication number
EP1054231A3
EP1054231A3 EP00110018A EP00110018A EP1054231A3 EP 1054231 A3 EP1054231 A3 EP 1054231A3 EP 00110018 A EP00110018 A EP 00110018A EP 00110018 A EP00110018 A EP 00110018A EP 1054231 A3 EP1054231 A3 EP 1054231A3
Authority
EP
European Patent Office
Prior art keywords
control surface
actuation system
air vehicle
aerodynamic control
servomotors
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
EP00110018A
Other languages
German (de)
French (fr)
Other versions
EP1054231B1 (en
EP1054231A2 (en
Inventor
Werner Dipl.-Ing. Schröppel
Josef Dipl.-Ing. Dommer
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 Defence GmbH and Co KG
Original Assignee
Diehl Munitionssysteme GmbH and Co KG
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 Munitionssysteme GmbH and Co KG filed Critical Diehl Munitionssysteme GmbH and Co KG
Publication of EP1054231A2 publication Critical patent/EP1054231A2/en
Publication of EP1054231A3 publication Critical patent/EP1054231A3/en
Application granted granted Critical
Publication of EP1054231B1 publication Critical patent/EP1054231B1/en
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)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

Bei einer Stelleinrichtung für Ruder eines Flugkörpers sind die Ruder 2,3 von Stellmotoren 5,6 über Schubspindeln 15 verstellbar. Für eine kompakte Bauweise bei kleinem Gewicht sind die Statoren 7 der Stellmotoren 5,6 unmittelbar in einem Trägergehäuse 4 angeordnet und die Schubspindel 15 greift in ein Innengewinde 14 der Motorwelle 9 ein.

Figure 00000001
In the case of an actuating device for the rudder of a missile, the rudders 2, 3 of servomotors 5, 6 are adjustable via thrust spindles 15. For a compact design with low weight, the stators 7 of the servomotors 5, 6 are arranged directly in a carrier housing 4 and the thrust spindle 15 engages in an internal thread 14 of the motor shaft 9.
Figure 00000001
EP00110018A 1999-05-18 2000-05-12 Actuation system for an aerodynamic control surface of an air vehicle Expired - Lifetime EP1054231B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19922693 1999-05-18
DE19922693A DE19922693A1 (en) 1999-05-18 1999-05-18 Control device for the rudder of a missile

Publications (3)

Publication Number Publication Date
EP1054231A2 EP1054231A2 (en) 2000-11-22
EP1054231A3 true EP1054231A3 (en) 2002-06-12
EP1054231B1 EP1054231B1 (en) 2005-11-30

Family

ID=7908347

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00110018A Expired - Lifetime EP1054231B1 (en) 1999-05-18 2000-05-12 Actuation system for an aerodynamic control surface of an air vehicle

Country Status (3)

Country Link
US (1) US6299101B1 (en)
EP (1) EP1054231B1 (en)
DE (2) DE19922693A1 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6446906B1 (en) * 2000-04-06 2002-09-10 Versatron, Inc. Fin and cover release system
DE102005038856A1 (en) 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Fastening system for attaching tail unit at fastening surface of airplane, has contact surfaces for attachment at tail unit and fastening surface, where contact surfaces comprise contact line and differentiating angle of specified degrees
WO2010005350A1 (en) * 2008-07-07 2010-01-14 Saab Ab Rudder machinery
US8148670B2 (en) * 2008-08-26 2012-04-03 Woodward Hrt, Inc. Rotary actuator ball-detent locking mechanism
US8324544B2 (en) 2010-06-02 2012-12-04 Woodward Hrt, Inc. Multi-stage fin deployment assembly
US8624172B2 (en) * 2010-10-13 2014-01-07 Woodward Hrt, Inc. Shift lock assembly
US9453531B2 (en) 2013-08-26 2016-09-27 Roller Bearing Company Of America, Inc. Integrated bearing assemblies for guided attack rockets
US9605692B2 (en) 2014-10-01 2017-03-28 Woodward, Inc. Locking rotary actuator

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5040745A (en) * 1987-01-30 1991-08-20 Diehl Gmbh & Co. Setting device for a control surface
US5249761A (en) * 1991-10-29 1993-10-05 Diehl Gmbh & Co. Setting device for a control surface

Family Cites Families (12)

* 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
US4037806A (en) * 1964-09-16 1977-07-26 General Dynamics Corporation Control system for rolling missile with target seeker head
US5393011A (en) * 1965-12-03 1995-02-28 Shorts Missile Systems Limited Control systems for moving bodies
US4438893A (en) * 1973-08-10 1984-03-27 Sanders Associates, Inc. Prime power source and control for a guided projectile
DE3441534A1 (en) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg BEARING ARRANGEMENT FOR THE RUDDER BLADE OF AN AIRCRAFT
DE3441533A1 (en) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg COUPLING DEVICE BETWEEN A LINEAR ACTUATOR AND A SWIVELING ELEMENT, IN PARTICULAR A CONTROL LEVER
DE3613539C1 (en) * 1986-04-22 1997-05-28 Dornier Gmbh Actuator for aerodynamic control surfaces, especially on missiles
US5528092A (en) * 1992-06-23 1996-06-18 Nippon Corporation Spindle motor
DE4325218C2 (en) * 1993-07-28 1998-10-22 Diehl Stiftung & Co Artillery missile and method for increasing the performance of an artillery missile
DE4335785A1 (en) * 1993-10-20 1995-04-27 Diehl Gmbh & Co Control surface actuating device
US5593109A (en) * 1995-01-10 1997-01-14 Lucas Western, Inc. Actuator system and method
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5040745A (en) * 1987-01-30 1991-08-20 Diehl Gmbh & Co. Setting device for a control surface
US5249761A (en) * 1991-10-29 1993-10-05 Diehl Gmbh & Co. Setting device for a control surface

Also Published As

Publication number Publication date
US6299101B1 (en) 2001-10-09
EP1054231B1 (en) 2005-11-30
DE50011724D1 (en) 2006-01-05
EP1054231A2 (en) 2000-11-22
DE19922693A1 (en) 2000-11-23

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