FR1191519A - Tail deploying for artillery projectile - Google Patents

Tail deploying for artillery projectile

Info

Publication number
FR1191519A
FR1191519A FR758227A FR758227A FR1191519A FR 1191519 A FR1191519 A FR 1191519A FR 758227 A FR758227 A FR 758227A FR 758227 A FR758227 A FR 758227A FR 1191519 A FR1191519 A FR 1191519A
Authority
FR
France
Prior art keywords
deploying
tail
artillery projectile
artillery
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
Application number
FR758227A
Other languages
French (fr)
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
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
Priority to FR758227A priority Critical patent/FR1191519A/en
Application granted granted Critical
Publication of FR1191519A publication Critical patent/FR1191519A/en
Expired legal-status Critical Current

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
FR758227A 1958-02-13 1958-02-13 Tail deploying for artillery projectile Expired FR1191519A (en)

Priority Applications (1)

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

Applications Claiming Priority (9)

Application Number Priority Date Filing Date Title
FR758227A FR1191519A (en) 1958-02-13 1958-02-13 Tail deploying for artillery projectile
CH348629D CH348629A (en) 1958-02-13 1959-01-27 Empennage for deployable artillery projectile
BE575185A BE575185A (en) 1958-02-13 1959-01-28 Jibe for deploying artillery projectile.
GB316759A GB846069A (en) 1958-02-13 1959-01-29 Improvements in and relating to a fin arrangement for projectiles
US790407A US3031967A (en) 1958-02-13 1959-02-02 Fin arrangement for projectiles
ES0247439A ES247439A1 (en) 1958-02-13 1959-02-04 Fin arrangement for projectiles
DEH35581A DE1123597B (en) 1958-02-13 1959-02-07 Foldable stabilizing fins for a abzuschiessendes from an artillery shell Geschuetzrohr
NL236009A NL111191C (en) 1958-02-13 1959-02-11
NL295562A NL295562A (en) 1958-02-13 1963-07-19

Publications (1)

Publication Number Publication Date
FR1191519A true FR1191519A (en) 1959-10-20

Family

ID=8705741

Family Applications (1)

Application Number Title Priority Date Filing Date
FR758227A Expired FR1191519A (en) 1958-02-13 1958-02-13 Tail deploying 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)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3058422A (en) * 1959-04-13 1962-10-16 Bofors Ab Wing assembly for missiles
DE4105142A1 (en) * 1991-02-20 1992-08-27 Diehl Gmbh & Co Projectile with fold-out pad
FR2677747A1 (en) * 1991-06-14 1992-12-18 Diehl Gmbh & Co Missile with fins of govern.

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125956A (en) * 1964-03-24 Fold able fin
US3127838A (en) * 1960-10-12 1964-04-07 Bombrini Parodi Delfino Spa Retractable blade tail unit for projectiles
US3697019A (en) * 1970-05-13 1972-10-10 Us Navy Stabilizing fin assembly
DE2342783C2 (en) * 1973-08-24 1983-12-22 Rheinmetall Gmbh, 4000 Duesseldorf, De
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
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

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE201605C (en) *
AT157500B (en) * 1937-01-04 1939-11-25 Sageb Sa Projectile for mortar smooth-bore.
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 ballistic rockets finned deployable empennage
FR1104534A (en) * 1954-05-13 1955-11-21 Soc Tech De Rech Ind deployable empennage
LU33739A1 (en) * 1955-07-21

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3058422A (en) * 1959-04-13 1962-10-16 Bofors Ab Wing assembly for missiles
DE4105142A1 (en) * 1991-02-20 1992-08-27 Diehl Gmbh & Co Projectile with fold-out pad
FR2677747A1 (en) * 1991-06-14 1992-12-18 Diehl Gmbh & Co Missile with fins of govern.

Also Published As

Publication number Publication date
NL295562A (en) 1965-05-10
ES247439A1 (en) 1959-12-16
NL111191C (en) 1965-05-17
US3031967A (en) 1962-05-01
BE575185A1 (en)
CH348629A (en) 1960-08-31
BE575185A (en) 1959-05-15
DE1123597B (en) 1962-02-08
GB846069A (en) 1960-08-24

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