FR2613474A1 - Element de voilure gonflable, notamment pour un engin volant - Google Patents

Element de voilure gonflable, notamment pour un engin volant Download PDF

Info

Publication number
FR2613474A1
FR2613474A1 FR8704724A FR8704724A FR2613474A1 FR 2613474 A1 FR2613474 A1 FR 2613474A1 FR 8704724 A FR8704724 A FR 8704724A FR 8704724 A FR8704724 A FR 8704724A FR 2613474 A1 FR2613474 A1 FR 2613474A1
Authority
FR
France
Prior art keywords
wing element
machine
wing
foam
rigid
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
FR8704724A
Other languages
English (en)
French (fr)
Other versions
FR2613474B1 (enrdf_load_stackoverflow
Inventor
Rene Thouron
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.)
Thomson Brandt Armements SA
Original Assignee
Thomson Brandt Armements SA
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 Thomson Brandt Armements SA filed Critical Thomson Brandt Armements SA
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 true FR2613474A1 (fr) 1988-10-07
FR2613474B1 FR2613474B1 (enrdf_load_stackoverflow) 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 (enrdf_load_stackoverflow)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2639105A1 (fr) * 1988-11-15 1990-05-18 Diehl Gmbh & Co Projectile a ailes deployables
FR2647892A1 (fr) * 1989-06-05 1990-12-07 Diehl Gmbh & Co Aileron deployable de missile
FR2765676A1 (fr) * 1989-05-23 1999-01-08 Bodenseewerk Geraetetech Engin volant avec ailes deployables
EP1564521A1 (de) * 2004-02-14 2005-08-17 Diehl BGT Defence GmbH & Co.KG Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln
WO2011002530A3 (en) * 2009-03-18 2011-02-24 Raytheon Company Reinforced inflatable wings for fitment-constrained air vehicles

Citations (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
FR2365776A1 (fr) * 1976-09-24 1978-04-21 Thomson Brandt Empennage deployant et projectile equipe d'un tel empennage, notamment projectile pour mortier
GB1597351A (en) * 1971-06-10 1981-09-09 British Aerospace Missiles

Patent Citations (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

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2639105A1 (fr) * 1988-11-15 1990-05-18 Diehl Gmbh & Co Projectile a ailes deployables
FR2765676A1 (fr) * 1989-05-23 1999-01-08 Bodenseewerk Geraetetech Engin volant avec ailes deployables
FR2647892A1 (fr) * 1989-06-05 1990-12-07 Diehl Gmbh & Co Aileron deployable de missile
EP1564521A1 (de) * 2004-02-14 2005-08-17 Diehl BGT Defence GmbH & Co.KG Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln
WO2011002530A3 (en) * 2009-03-18 2011-02-24 Raytheon Company Reinforced inflatable wings for fitment-constrained air vehicles
US8104713B2 (en) 2009-03-18 2012-01-31 Raytheon Company Reinforced inflatable wings for fitment-constrained air vehicles

Also Published As

Publication number Publication date
FR2613474B1 (enrdf_load_stackoverflow) 1993-02-26

Similar Documents

Publication Publication Date Title
EP0956441B1 (fr) Divergent deployable pour propulseur
FR2465644A1 (fr) Fusee comportant des ailes auto-deployables et retractables
US5615846A (en) Extendable wing for guided missles and munitions
US4336914A (en) Deployable wing mechanism
US7829829B2 (en) Grid fin control system for a fluid-borne object
US5437230A (en) Standoff mine neutralization system and method
US4687455A (en) Flying model rocket and method of recovery
FR2587911A1 (fr) Dispositif d'obturation declenchable pour une fusee-jouet a propulsion hydropneumatique
FR2613474A1 (fr) Element de voilure gonflable, notamment pour un engin volant
CA3200032A1 (fr) Systeme de transport spatial reutilisable
FR2542697A1 (fr) Procede et dispositif pyrotechnique d'ejection hors d'un avion
FR3060652A1 (fr) Nacelle pour turboreacteur d’aeronef equipee d’un dispositif d’extinction de feu
US4659038A (en) Aircraft with deployable wing portions
FR2647892A1 (fr) Aileron deployable de missile
CA1314035C (fr) Avions et hydravions multifuselages a trois surfaces portantes
FR2629908A1 (fr) Dispositif de freinage aerodynamique d'un corps
EP0319379B1 (fr) Corps largable muni de moyens de freinage aérodynamique
FR2748804A1 (fr) Tete de combat en tandem
US7066428B1 (en) Unfolding wing for air-launched, low speed air vehicles
FR2521281A1 (fr) Logement d'aile et dispositif de deblocage de couvercle pour aile a erection automatique pour engins speciaux
FR2724907A1 (fr) Lanceur de leurres electromagnetiques a ejection differee
EP0044251B1 (fr) Dispositif pyrotechnique de découpage et d'éjection d'un élément transparent de verrière d'avion
FR2634454A1 (fr) Unite de sauvetage pour l'equipage de transporteurs spatiaux
DE2410514C2 (de) Rettungs- und Bergungssystem
US4462562A (en) Self-deploying afterbody apparatus for an ejection seat

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20051230