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

    • 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
    • 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
    • F42B10/16—Wrap-around fins
    • 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
    • F42B10/20—Stabilising 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 (cg-RX-API-DMAC7.html) 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 (cg-RX-API-DMAC7.html)

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

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20051230