FR2613474B1 - - Google Patents

Info

Publication number
FR2613474B1
FR2613474B1 FR8704724A FR8704724A FR2613474B1 FR 2613474 B1 FR2613474 B1 FR 2613474B1 FR 8704724 A FR8704724 A FR 8704724A FR 8704724 A FR8704724 A FR 8704724A FR 2613474 B1 FR2613474 B1 FR 2613474B1
Authority
FR
France
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 - Fee Related
Application number
FR8704724A
Other languages
French (fr)
Other versions
FR2613474A1 (fr
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 filed Critical
Priority to FR8704724A priority Critical patent/FR2613474A1/fr
Publication of FR2613474A1 publication Critical patent/FR2613474A1/fr
Application granted granted Critical
Publication of FR2613474B1 publication Critical patent/FR2613474B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/146Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16Wrap-around fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
FR8704724A 1987-04-03 1987-04-03 Element de voilure gonflable, notamment pour un engin volant Granted FR2613474A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8704724A FR2613474A1 (fr) 1987-04-03 1987-04-03 Element de voilure gonflable, notamment pour un engin volant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8704724A FR2613474A1 (fr) 1987-04-03 1987-04-03 Element de voilure gonflable, notamment pour un engin volant

Publications (2)

Publication Number Publication Date
FR2613474A1 FR2613474A1 (fr) 1988-10-07
FR2613474B1 true FR2613474B1 (es) 1993-02-26

Family

ID=9349774

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8704724A Granted FR2613474A1 (fr) 1987-04-03 1987-04-03 Element de voilure gonflable, notamment pour un engin volant

Country Status (1)

Country Link
FR (1) FR2613474A1 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3838738A1 (de) * 1988-11-15 1990-05-23 Diehl Gmbh & Co Projektil mit ausklappbaren fluegeln
DE3916690C1 (de) * 1989-05-23 1998-10-01 Bodenseewerk Geraetetech Ausklappbare Flügelanordnung für Flugkörper
DE3918244A1 (de) * 1989-06-05 1990-12-06 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
DE102004007311A1 (de) * 2004-02-14 2005-09-01 Diehl Bgt Defence Gmbh & Co. Kg Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln
US8104713B2 (en) * 2009-03-18 2012-01-31 Raytheon Company Reinforced inflatable wings for fitment-constrained air vehicles

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
GB1597351A (en) * 1971-06-10 1981-09-09 British Aerospace Missiles
FR2365776A1 (fr) * 1976-09-24 1978-04-21 Thomson Brandt Empennage deployant et projectile equipe d'un tel empennage, notamment projectile pour mortier

Also Published As

Publication number Publication date
FR2613474A1 (fr) 1988-10-07

Similar Documents

Publication Publication Date Title
DE3876858D1 (es)
IN170601B (es)
IN165927B (es)
GR3007124T3 (es)
IN168936B (es)
IN167963B (es)
EP0510732A3 (es)
DE3868177D1 (es)
IN168935B (es)
IN170880B (es)
IN168631B (es)
DE3868416D1 (es)
FR2611600B1 (es)
FR2619502B1 (es)
IN173404B (es)
IN169592B (es)
GR3003628T3 (es)
FR2621205B1 (es)
IN169717B (es)
GR3007207T3 (es)
FR2616950B1 (es)
IN169532B (es)
IN169539B (es)
IN166589B (es)
IN166115B (es)

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20051230