ES269713A1 - Openable fin arrangement - Google Patents

Openable fin arrangement

Info

Publication number
ES269713A1
ES269713A1 ES0269713A ES269713A ES269713A1 ES 269713 A1 ES269713 A1 ES 269713A1 ES 0269713 A ES0269713 A ES 0269713A ES 269713 A ES269713 A ES 269713A ES 269713 A1 ES269713 A1 ES 269713A1
Authority
ES
Spain
Prior art keywords
flaps
guide
combined
openable
impeller
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
Application number
ES0269713A
Other languages
Spanish (es)
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.)
Hotchkiss Brandt SA
Original Assignee
Hotchkiss Brandt 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 Hotchkiss Brandt SA filed Critical Hotchkiss Brandt SA
Publication of ES269713A1 publication Critical patent/ES269713A1/en
Expired 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
    • 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)
  • Discharge By Other Means (AREA)

Abstract

Folding projectile flap guide, of the type in which the flaps are swung out in longitudinal radial planes of the guide and located towards the front ends of the flaps, and characterized by the fact that their flaps are combined with a device impeller, concentric with respect to the longitudinal axis of the guide and movable along that axis between an anterior position, in which the flaps are retracted, and a posterior position, in which said flaps are deployed and held in that position by the impeller device, which in turn is combined with means to exert on it an axial thrust that tends to move it from the previous position to the posterior position. (Machine-translation by Google Translate, not legally binding)
ES0269713A 1960-07-11 1961-07-10 Openable fin arrangement Expired ES269713A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR832688A FR1270054A (en) 1960-07-11 1960-07-11 Deployable tail for self-propelled projectile
FR865095A FR79945E (en) 1960-07-11 1961-06-15 Deployable tail for self-propelled projectile

Publications (1)

Publication Number Publication Date
ES269713A1 true ES269713A1 (en) 1962-01-01

Family

ID=26186750

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0269713A Expired ES269713A1 (en) 1960-07-11 1961-07-10 Openable fin arrangement

Country Status (9)

Country Link
US (1) US3098446A (en)
BE (1) BE605677A (en)
CH (1) CH370677A (en)
DE (2) DE1195204B (en)
ES (1) ES269713A1 (en)
FI (1) FI41122B (en)
FR (2) FR1270054A (en)
GB (2) GB952960A (en)
NL (3) NL295319A (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3196793A (en) * 1963-01-16 1965-07-27 Milenkovic Veljko Folded fin rocket
US5439188A (en) * 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
US3378216A (en) * 1966-04-29 1968-04-16 Susquehama Corp Integral fin canister-nozzle exit cone
US3690595A (en) * 1970-11-19 1972-09-12 Sarmac Sa Self-propelled, vaned missile
DE2264338A1 (en) * 1972-12-30 1974-07-04 Dynamit Nobel Ag FOLD-OUT TAIL, ESPECIALLY FOR MISSILE
FR2221707B1 (en) * 1973-03-14 1976-04-30 France Etat
US3946969A (en) * 1974-07-30 1976-03-30 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3986685A (en) * 1974-07-30 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3986684A (en) * 1974-07-30 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US3998407A (en) * 1974-07-30 1976-12-21 The United States Of America As Represented By The Secretary Of The Army Folding tail fins
US4523728A (en) * 1983-03-07 1985-06-18 Ford Aerospace & Communications Corporation Passive auto-erecting alignment wings for long rod penetrator
SE444612B (en) * 1984-12-13 1986-04-21 Ffv Affersverket GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL
DE3447852A1 (en) * 1984-12-31 1986-08-28 Heide, Marion, 4030 Ratingen FOLDING ASSEMBLY FOR WING-STABILIZED ROCKET BULLETS
US5235930A (en) * 1992-05-08 1993-08-17 Rockwell International Corporation Self propelled underwater device with steerable fin stabilizer
GB2274904A (en) * 1993-02-05 1994-08-10 British Aerospace Deployable wing
US6559370B1 (en) * 2002-08-06 2003-05-06 The United States Of America As Represented By The Secretary Of The Navy Submarine countermeasure vehicle with folding propeller
FR2863045B1 (en) * 2003-11-27 2006-01-06 Giat Ind Sa DEVICE FOR SECURELY DEPLOYING THE FINS OF A PROJECTILE
US7083141B2 (en) * 2003-12-02 2006-08-01 Edward Nitenson Self-propelled projectile
KR101074028B1 (en) 2009-02-12 2011-10-17 국방과학연구소 Flying object with fixing device for the deployed wing
FR2946423A1 (en) * 2009-06-05 2010-12-10 Tda Armements Sas DEVICE FOR OPENING AND LOCKING A MUNITION STACK
CN113237393A (en) * 2021-04-28 2021-08-10 北京星途探索科技有限公司 High-precision stabilizing device
US11796291B2 (en) * 2022-01-11 2023-10-24 Raytheon Company Effector having morphing airframe and method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR896502A (en) * 1940-09-23 1945-02-23 Commerciale Caproni Comp Device for controlling the fins of a projectile fitted with a tail unit
US2365577A (en) * 1943-08-26 1944-12-19 Stephen A Moore Projectile
BE565999A (en) * 1953-02-06
BE552288A (en) * 1953-10-20
LU33739A1 (en) * 1955-07-21
FR1187193A (en) * 1957-11-15 1959-09-08 Hotchkiss Brandt Deployable stabilizer for projectile
LU36192A1 (en) * 1958-05-22
NL248980A (en) * 1959-03-09

Also Published As

Publication number Publication date
NL266892A (en)
US3098446A (en) 1963-07-23
NL113679C (en)
NL295319A (en)
CH370677A (en) 1963-07-15
BE605677A (en) 1961-11-03
GB952960A (en) 1964-03-18
FR1270054A (en) 1961-08-25
DE1183834B (en) 1964-12-17
DE1195204B (en) 1965-06-16
FR79945E (en) 1963-02-15
FI41122B (en) 1969-04-30
GB945409A (en) 1963-12-23

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