NO123481B - - Google Patents

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Info

Publication number
NO123481B
NO123481B NO4285/69A NO428569A NO123481B NO 123481 B NO123481 B NO 123481B NO 4285/69 A NO4285/69 A NO 4285/69A NO 428569 A NO428569 A NO 428569A NO 123481 B NO123481 B NO 123481B
Authority
NO
Norway
Prior art keywords
wing
recess
projectile
holder
axis
Prior art date
Application number
NO4285/69A
Other languages
English (en)
Norwegian (no)
Inventor
G Jacobson
O Olsson
Original Assignee
Bofors Ab
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 Bofors Ab filed Critical Bofors Ab
Publication of NO123481B publication Critical patent/NO123481B/no

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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
NO4285/69A 1968-11-01 1969-10-29 NO123481B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE14844/68*A SE325802B (de) 1968-11-01 1968-11-01

Publications (1)

Publication Number Publication Date
NO123481B true NO123481B (de) 1971-11-22

Family

ID=20299762

Family Applications (1)

Application Number Title Priority Date Filing Date
NO4285/69A NO123481B (de) 1968-11-01 1969-10-29

Country Status (9)

Country Link
US (1) US3627233A (de)
BE (1) BE741130A (de)
CH (1) CH505361A (de)
DE (1) DE1954953C3 (de)
FR (1) FR2022395A1 (de)
GB (1) GB1291589A (de)
NL (1) NL160384B (de)
NO (1) NO123481B (de)
SE (1) SE325802B (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3790104A (en) * 1973-03-12 1974-02-05 Us Navy High/low aspect ratio dual-mode fin design
FR2356118A1 (fr) * 1976-06-25 1978-01-20 Europ Propulsion Empennage pour projectile
DE2841773C2 (de) * 1978-09-26 1984-07-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Anordnung des Leitwerks, insbesondere bei Flugkörpern oder Geschossen
AU524255B2 (en) * 1978-12-29 1982-09-09 Commonwealth Of Australia, The Deployable wing
SE433882B (sv) * 1979-10-09 1984-06-18 Bofors Ab Utfellbar fena for en fenstabiliserad ammunitionsenhet i form av en granat
US4588146A (en) * 1984-03-29 1986-05-13 The United States Of America As Represented By The Secretary Of The Army Biaxial folding lever wing
IL101730A (en) * 1992-04-30 1995-12-31 Israel State Moving body such as missile having wings erectable upon acceleration
US8438977B2 (en) 2008-12-25 2013-05-14 Lockheed Martin Corporation Projectile having deployable fin
US11754379B2 (en) * 2018-03-23 2023-09-12 Simmonds Precision Products, Inc. Space saving wing stowage
CN112985190A (zh) * 2021-04-13 2021-06-18 西安航天动力技术研究所 一种涡卷弹簧式折叠弹翼展开机构

Also Published As

Publication number Publication date
US3627233A (en) 1971-12-14
DE1954953B2 (de) 1975-05-28
GB1291589A (en) 1972-10-04
NL6916191A (de) 1970-05-06
CH505361A (de) 1971-03-31
DE1954953A1 (de) 1970-06-18
BE741130A (de) 1970-04-01
SE325802B (de) 1970-07-06
FR2022395A1 (de) 1970-07-31
DE1954953C3 (de) 1976-01-08
NL160384B (nl) 1979-05-15

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