CH348629A - Deployable tail for artillery projectile - Google Patents

Deployable tail for artillery projectile

Info

Publication number
CH348629A
CH348629A CH348629DA CH348629A CH 348629 A CH348629 A CH 348629A CH 348629D A CH348629D A CH 348629DA CH 348629 A CH348629 A CH 348629A
Authority
CH
Switzerland
Prior art keywords
artillery projectile
deployable tail
deployable
tail
artillery
Prior art date
Application number
Other languages
French (fr)
Original Assignee
Hotchkiss Brandt
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 filed Critical Hotchkiss Brandt
Publication of CH348629A publication Critical patent/CH348629A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20Stabilising 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/18Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Basic Packing Technique (AREA)
  • Automatic Assembly (AREA)
  • Portable Nailing Machines And Staplers (AREA)
CH348629D 1958-02-13 1959-01-27 Deployable tail for artillery projectile CH348629A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR758227A FR1191519A (en) 1958-02-13 1958-02-13 Deploying tail for artillery projectile

Publications (1)

Publication Number Publication Date
CH348629A true CH348629A (en) 1960-08-31

Family

ID=8705741

Family Applications (1)

Application Number Title Priority Date Filing Date
CH348629D CH348629A (en) 1958-02-13 1959-01-27 Deployable tail for artillery projectile

Country Status (8)

Country Link
US (1) US3031967A (en)
BE (1) BE575185A (en)
CH (1) CH348629A (en)
DE (1) DE1123597B (en)
ES (1) ES247439A1 (en)
FR (1) FR1191519A (en)
GB (1) GB846069A (en)
NL (2) NL111191C (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125956A (en) * 1964-03-24 Fold able fin
NL101734C (en) * 1959-04-13
US3127838A (en) 1960-10-12 1964-04-07 Bombrini Parodi Delfino Spa Retractable blade tail unit for projectiles
CH480613A (en) * 1967-09-11 1969-10-31 Oerlikon Buehrle Ag Bullet with brake wings
US3697019A (en) * 1970-05-13 1972-10-10 Us Navy Stabilizing fin assembly
DE2342783C2 (en) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Projectile equipped with a tail unit
US4158447A (en) * 1977-11-29 1979-06-19 The United States Of America As Represented By The Secretary Of The Navy Expanding stabilizing fin cup
DE4105142A1 (en) * 1991-02-20 1992-08-27 Diehl Gmbh & Co PROJECTILE WITH FOLD-OUT PAD
DE4119613C2 (en) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Missiles with fold-out guidance devices
FR2895071B1 (en) * 2005-12-19 2008-01-18 Giat Ind Sa ANTI-REBOUND LOCKING DEVICE OF A DEPLOYABLE FIN OF A PROJECTILE.
SE535837C2 (en) * 2011-04-14 2013-01-08 Bae Systems Bofors Ab Fenutfällningsmekanism
US10150556B2 (en) 2016-05-23 2018-12-11 The Boeing Company Low-profile wing hinge mechanism
CN115451757B (en) * 2022-09-13 2024-07-16 北京航星传动科技有限公司 Grid rudder folding and unfolding actuating mechanism and servo system thereof

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE201605C (en) *
DE1048514B (en)
AT157500B (en) * 1937-01-04 1939-11-25 Sageb Sa Bullet for mortar with smooth barrel.
US2145508A (en) * 1937-01-04 1939-01-31 Sageb Sa Bladed projectile
US2427217A (en) * 1943-09-23 1947-09-09 Harry J Lebherz Rocket fin assembly
US2465401A (en) * 1943-09-23 1949-03-29 Leslie A Skinner Rocket fin assembly
US2671398A (en) * 1951-05-11 1954-03-09 Allen S Peck Metal pop-out stabilizing tail for small bombs
FR1061242A (en) * 1952-08-05 1954-04-09 Development of rocket projectiles with deployable tail fins
FR1104534A (en) * 1954-05-13 1955-11-21 Soc Tech De Rech Ind Deployable tail
LU33739A1 (en) * 1955-07-21

Also Published As

Publication number Publication date
FR1191519A (en) 1959-10-20
NL111191C (en) 1965-05-17
NL295562A (en) 1965-05-10
DE1123597B (en) 1962-02-08
ES247439A1 (en) 1959-12-16
US3031967A (en) 1962-05-01
GB846069A (en) 1960-08-24
BE575185A (en) 1959-05-15

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