GB2238856B - Deployable shaped wing for a flying projectile - Google Patents

Deployable shaped wing for a flying projectile

Info

Publication number
GB2238856B
GB2238856B GB9026534A GB9026534A GB2238856B GB 2238856 B GB2238856 B GB 2238856B GB 9026534 A GB9026534 A GB 9026534A GB 9026534 A GB9026534 A GB 9026534A GB 2238856 B GB2238856 B GB 2238856B
Authority
GB
United Kingdom
Prior art keywords
shaped wing
flying projectile
deployable
deployable shaped
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 - Fee Related
Application number
GB9026534A
Other versions
GB2238856A (en
GB9026534D0 (en
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
Publication of GB9026534D0 publication Critical patent/GB9026534D0/en
Publication of GB2238856A publication Critical patent/GB2238856A/en
Application granted granted Critical
Publication of GB2238856B publication Critical patent/GB2238856B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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)
GB9026534A 1989-12-08 1990-12-06 Deployable shaped wing for a flying projectile Expired - Fee Related GB2238856B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8916265A FR2655720A1 (en) 1989-12-08 1989-12-08 WING GALBEE DEPLOYABLE FOR FLYING ENGINE.

Publications (3)

Publication Number Publication Date
GB9026534D0 GB9026534D0 (en) 1991-01-23
GB2238856A GB2238856A (en) 1991-06-12
GB2238856B true GB2238856B (en) 1993-12-15

Family

ID=9388300

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9026534A Expired - Fee Related GB2238856B (en) 1989-12-08 1990-12-06 Deployable shaped wing for a flying projectile

Country Status (4)

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

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 (en) * 2001-04-12 2002-10-17 Diehl Munitionssysteme Gmbh Rudder blade storage device for one floor
US6869044B2 (en) * 2003-05-23 2005-03-22 Raytheon Company Missile with odd symmetry tail fins

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB753838A (en) * 1953-12-21 1956-08-01 Brandt Soc Nouv Ets Improvements in and relating to a fin arrangement for a projectile
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
GB1586599A (en) * 1976-06-25 1981-03-25 Europ Propulsion Tail unit for a missile
US4323208A (en) * 1980-02-01 1982-04-06 British Aerospace Folding fins
GB2153982A (en) * 1984-02-02 1985-08-29 Dynamit Nobel Ag Flight body
US4664339A (en) * 1984-10-11 1987-05-12 The Boeing Company Missile appendage deployment mechanism
EP0242180A2 (en) * 1986-04-15 1987-10-21 British Aerospace Public Limited Company Deployment arrangement for spinning body
WO1988005898A1 (en) * 1987-02-02 1988-08-11 Eskam, Armin Finned projectile or missile

Family Cites Families (6)

* 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
FR1485580A (en) * 1966-03-15 1967-06-23 Hotchkiss Brandt Advanced tail for rocket
DE1901521A1 (en) * 1969-01-14 1970-08-13 Messerschmitt Boelkow Blohm Collapsible guide vane mechanism for project - iles fired from containers
DE3611648A1 (en) * 1986-04-07 1989-10-12 Diehl Gmbh & Co Missile having folding wings
FR2623898B1 (en) * 1987-11-26 1990-03-23 France Etat Armement DEVICE FOR DEPLOYING A PROJECTILE FIN
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB753838A (en) * 1953-12-21 1956-08-01 Brandt Soc Nouv Ets Improvements in and relating to a fin arrangement for a projectile
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
GB1586599A (en) * 1976-06-25 1981-03-25 Europ Propulsion Tail unit for a missile
US4323208A (en) * 1980-02-01 1982-04-06 British Aerospace Folding fins
GB2153982A (en) * 1984-02-02 1985-08-29 Dynamit Nobel Ag Flight body
US4664339A (en) * 1984-10-11 1987-05-12 The Boeing Company Missile appendage deployment mechanism
EP0242180A2 (en) * 1986-04-15 1987-10-21 British Aerospace Public Limited Company Deployment arrangement for spinning body
WO1988005898A1 (en) * 1987-02-02 1988-08-11 Eskam, Armin Finned projectile or missile

Also Published As

Publication number Publication date
FR2655720B1 (en) 1994-04-22
IT9067978A1 (en) 1991-06-09
CH684549A5 (en) 1994-10-14
IT9067978A0 (en) 1990-12-07
IT1241019B (en) 1993-12-27
GB2238856A (en) 1991-06-12
GB9026534D0 (en) 1991-01-23
FR2655720A1 (en) 1991-06-14

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19961206