FR2655720B1 - - Google Patents

Info

Publication number
FR2655720B1
FR2655720B1 FR8916265A FR8916265A FR2655720B1 FR 2655720 B1 FR2655720 B1 FR 2655720B1 FR 8916265 A FR8916265 A FR 8916265A FR 8916265 A FR8916265 A FR 8916265A FR 2655720 B1 FR2655720 B1 FR 2655720B1
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
FR8916265A
Other languages
French (fr)
Other versions
FR2655720A1 (fr
Inventor
Marc Bernard
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 FR8916265A priority Critical patent/FR2655720A1/fr
Priority to CH3866/90A priority patent/CH684549A5/fr
Priority to GB9026534A priority patent/GB2238856B/en
Priority to IT67978A priority patent/IT1241019B/it
Publication of FR2655720A1 publication Critical patent/FR2655720A1/fr
Application granted granted Critical
Publication of FR2655720B1 publication Critical patent/FR2655720B1/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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Prostheses (AREA)
FR8916265A 1989-12-08 1989-12-08 Aile galbee deployable pour engin volant. Granted FR2655720A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8916265A FR2655720A1 (fr) 1989-12-08 1989-12-08 Aile galbee deployable pour engin volant.
CH3866/90A CH684549A5 (fr) 1989-12-08 1990-12-06 Aile galbée déployable pour engin volant.
GB9026534A GB2238856B (en) 1989-12-08 1990-12-06 Deployable shaped wing for a flying projectile
IT67978A IT1241019B (it) 1989-12-08 1990-12-07 Ala sagomata dispiegabile per un ordigno volante

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8916265A FR2655720A1 (fr) 1989-12-08 1989-12-08 Aile galbee deployable pour engin volant.

Publications (2)

Publication Number Publication Date
FR2655720A1 FR2655720A1 (fr) 1991-06-14
FR2655720B1 true FR2655720B1 (ja) 1994-04-22

Family

ID=9388300

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8916265A Granted FR2655720A1 (fr) 1989-12-08 1989-12-08 Aile galbee deployable pour engin volant.

Country Status (4)

Country Link
CH (1) CH684549A5 (ja)
FR (1) FR2655720A1 (ja)
GB (1) GB2238856B (ja)
IT (1) IT1241019B (ja)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5480111A (en) * 1994-05-13 1996-01-02 Hughes Missile Systems Company Missile with deployable control fins
DE10118216A1 (de) * 2001-04-12 2002-10-17 Diehl Munitionssysteme Gmbh Ruderblatt-Lagereinrichtung für ein Geschoß
US6869044B2 (en) * 2003-05-23 2005-03-22 Raytheon Company Missile with odd symmetry tail fins

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2044819A (en) * 1933-10-27 1936-06-23 James G Taylor Projectile
BE533456A (ja) * 1953-12-21 Brandt Soc Nouv Ets
US3063375A (en) * 1960-05-19 1962-11-13 Wilbur W Hawley Folding fin
US3127838A (en) * 1960-10-12 1964-04-07 Bombrini Parodi Delfino Spa Retractable blade tail unit for projectiles
FR1485580A (fr) * 1966-03-15 1967-06-23 Hotchkiss Brandt Empennage perfectionné pour roquette
DE1901521A1 (de) * 1969-01-14 1970-08-13 Messerschmitt Boelkow Blohm Klappleitwerk
FR2356118A1 (fr) * 1976-06-25 1978-01-20 Europ Propulsion Empennage pour projectile
US4323208A (en) * 1980-02-01 1982-04-06 British Aerospace Folding fins
DE3403508A1 (de) * 1984-02-02 1985-08-08 Dynamit Nobel Ag, 5210 Troisdorf Flugkoerper
US4664339A (en) * 1984-10-11 1987-05-12 The Boeing Company Missile appendage deployment mechanism
DE3611648A1 (de) * 1986-04-07 1989-10-12 Diehl Gmbh & Co Flugkoerper mit klappfluegeln
GB8609166D0 (en) * 1986-04-15 1986-09-17 British Aerospace Deployment arrangement for spinning body
FR2623898B1 (fr) * 1987-11-26 1990-03-23 France Etat Armement Dispositif de deploiement d'une ailette de projectile
WO1988005898A1 (en) * 1987-02-02 1988-08-11 Eskam, Armin Finned projectile or missile
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil

Also Published As

Publication number Publication date
IT9067978A1 (it) 1991-06-09
IT9067978A0 (it) 1990-12-07
GB2238856A (en) 1991-06-12
GB2238856B (en) 1993-12-15
IT1241019B (it) 1993-12-27
GB9026534D0 (en) 1991-01-23
CH684549A5 (fr) 1994-10-14
FR2655720A1 (fr) 1991-06-14

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Legal Events

Date Code Title Description
ST Notification of lapse