FR2559893B1 - Projectile a ailettes deployables - Google Patents

Projectile a ailettes deployables

Info

Publication number
FR2559893B1
FR2559893B1 FR8417093A FR8417093A FR2559893B1 FR 2559893 B1 FR2559893 B1 FR 2559893B1 FR 8417093 A FR8417093 A FR 8417093A FR 8417093 A FR8417093 A FR 8417093A FR 2559893 B1 FR2559893 B1 FR 2559893B1
Authority
FR
France
Prior art keywords
projectile
deployable fins
deployable
fins
fins projectile
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
Application number
FR8417093A
Other languages
English (en)
Other versions
FR2559893A1 (fr
Inventor
Raimar Steuer
Bernd Brieseck
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
Priority claimed from DE19833340501 external-priority patent/DE3340501C2/de
Application filed by Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of FR2559893A1 publication Critical patent/FR2559893A1/fr
Application granted granted Critical
Publication of FR2559893B1 publication Critical patent/FR2559893B1/fr
Expired 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/146—Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Professional, Industrial, Or Sporting Protective Garments (AREA)
FR8417093A 1983-11-09 1984-11-09 Projectile a ailettes deployables Expired FR2559893B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19833340501 DE3340501C2 (de) 1983-11-09 1983-11-09 Geschoß mit herausklappbaren Flügeln
DE19843403573 DE3403573A1 (de) 1983-11-09 1984-02-02 Geschoss mit herausklappbaren fluegeln

Publications (2)

Publication Number Publication Date
FR2559893A1 FR2559893A1 (fr) 1985-08-23
FR2559893B1 true FR2559893B1 (fr) 1987-10-16

Family

ID=25815486

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8417093A Expired FR2559893B1 (fr) 1983-11-09 1984-11-09 Projectile a ailettes deployables

Country Status (4)

Country Link
US (1) US4664338A (fr)
DE (1) DE3403573A1 (fr)
FR (1) FR2559893B1 (fr)
GB (1) GB2149481B (fr)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3422231A1 (de) * 1984-06-15 1985-12-19 Diehl GmbH & Co, 8500 Nürnberg Einrichtung zum aerodynamischen abbremsen der rotationsbewegung eines koerpers
GB2162623B (en) * 1984-06-15 1988-08-10 Diehl Gmbh & Co A mechanism for aerodynamic deceleration and a body including such a mechanism
DE3523769A1 (de) * 1985-07-03 1987-01-08 Diehl Gmbh & Co Submunitions-flugkoerper mit ausstellbaren gleitfluegeln
DE3738580A1 (de) * 1987-11-13 1989-06-01 Diehl Gmbh & Co Gelenktes artillerieprojektil mit flugbahnregler
US4858851A (en) * 1988-06-07 1989-08-22 General Dynamics Pomona Division Folding wing structure for missile
GB8815060D0 (en) * 1988-06-24 1988-11-16 British Aerospace Fin assembly for projectile
DE3838738A1 (de) * 1988-11-15 1990-05-23 Diehl Gmbh & Co Projektil mit ausklappbaren fluegeln
DE3918244A1 (de) * 1989-06-05 1990-12-06 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
DE4016840A1 (de) * 1990-05-25 1991-11-28 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
US5381986A (en) * 1992-01-30 1995-01-17 The Boeing Company Folding wing-tip system
US5452864A (en) * 1994-03-31 1995-09-26 Alliant Techsystems Inc. Electro-mechanical roll control apparatus and method
US5615846A (en) * 1994-11-04 1997-04-01 Gec Marconi Dynamics Inc. Extendable wing for guided missles and munitions
US6260797B1 (en) * 1998-01-13 2001-07-17 Science Applications International Corporation Transformable gun launched aero vehicle
US6186443B1 (en) 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
DE102004007311A1 (de) 2004-02-14 2005-09-01 Diehl Bgt Defence Gmbh & Co. Kg Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln
US7841559B1 (en) 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
US7628353B2 (en) * 2006-11-14 2009-12-08 Raytheon Company Delayed tail fin deployment mechanism and method
US9127908B2 (en) 2009-02-02 2015-09-08 Aero Vironment, Inc. Multimode unmanned aerial vehicle
KR20120113210A (ko) 2009-09-09 2012-10-12 에어로바이론먼트, 인크. 휴대용 ｒｆ 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치
AU2010325108B2 (en) 2009-09-09 2016-09-01 Aerovironment, Inc. Elevon control system
US8946607B2 (en) * 2011-12-13 2015-02-03 The Boeing Company Mechanisms for deploying and actuating airfoil-shaped bodies on unmanned aerial vehicles
US10124880B1 (en) * 2016-02-03 2018-11-13 Lockheed Martin Corporation Rotatable control surface assembly for an unmanned aerial vehicle

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1339188A (en) * 1918-11-20 1920-05-04 Zigmond Frecska Aerial torpedo
NL90108C (fr) * 1951-11-07
DE1203647B (de) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Flossenleitwerk, insbesondere fuer Raketengeschosse
US3636877A (en) * 1964-06-02 1972-01-25 Us Navy Antisubmarine missile
US3507150A (en) * 1966-01-24 1970-04-21 Robert F Stengel Wind velocity probing device and method
GB1258044A (fr) * 1967-11-02 1971-12-22
US3464356A (en) * 1967-12-28 1969-09-02 Us Army Self-stabilizing rod penetrators
FR1563898A (fr) * 1968-02-13 1969-04-18
US3743218A (en) * 1968-06-28 1973-07-03 T Sweeney Semi-rigid airfoil for airborne vehicles
GB1597351A (en) * 1971-06-10 1981-09-09 British Aerospace Missiles
US4351499A (en) * 1979-09-24 1982-09-28 General Dynamics Double fabric, retractable, self-erecting wing for missle
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
IL66624A (en) * 1982-02-10 1986-04-29 Gen Dynamics Corp Wing housing and cover release assembly for self-erecting wing of a structure such as missile
US4586680A (en) * 1982-02-10 1986-05-06 General Dynamics Pomona Division Spring-erected telescopic wing support structure
US4586681A (en) * 1983-06-27 1986-05-06 General Dynamics Pomona Division Supersonic erectable fabric wings
DE3340501C2 (de) * 1983-11-09 1986-12-04 Diehl GmbH & Co, 8500 Nürnberg Geschoß mit herausklappbaren Flügeln

Also Published As

Publication number Publication date
DE3403573A1 (de) 1985-08-08
US4664338A (en) 1987-05-12
GB2149481B (en) 1988-04-20
GB8428010D0 (en) 1984-12-12
FR2559893A1 (fr) 1985-08-23
GB2149481A (en) 1985-06-12

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Legal Events

Date Code Title Description
ST Notification of lapse