FR2042636A1 - - Google Patents

Info

Publication number
FR2042636A1
FR2042636A1 FR7017487A FR7017487A FR2042636A1 FR 2042636 A1 FR2042636 A1 FR 2042636A1 FR 7017487 A FR7017487 A FR 7017487A FR 7017487 A FR7017487 A FR 7017487A FR 2042636 A1 FR2042636 A1 FR 2042636A1
Authority
FR
France
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.)
Granted
Application number
FR7017487A
Other languages
French (fr)
Other versions
FR2042636B1 (en
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.)
Saab Bofors AB
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 FR2042636A1 publication Critical patent/FR2042636A1/fr
Application granted granted Critical
Publication of FR2042636B1 publication Critical patent/FR2042636B1/fr
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
    • F42B10/16—Wrap-around fins
FR707017487A 1969-05-14 1970-05-13 Expired FR2042636B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE06892/69A SE331242B (en) 1969-05-14 1969-05-14

Publications (2)

Publication Number Publication Date
FR2042636A1 true FR2042636A1 (en) 1971-02-12
FR2042636B1 FR2042636B1 (en) 1974-07-12

Family

ID=20269849

Family Applications (1)

Application Number Title Priority Date Filing Date
FR707017487A Expired FR2042636B1 (en) 1969-05-14 1970-05-13

Country Status (8)

Country Link
US (1) US3650496A (en)
BE (1) BE750400A (en)
CH (1) CH506771A (en)
FR (1) FR2042636B1 (en)
GB (1) GB1307298A (en)
NL (1) NL159783B (en)
NO (1) NO125114B (en)
SE (1) SE331242B (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3441534A1 (en) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg BEARING ARRANGEMENT FOR THE RUDDER BLADE OF AN AIRCRAFT
IL107844A (en) * 1993-12-02 1996-06-18 Ministry Of Defence Armaments Flying objects control device
US5816532A (en) * 1996-12-17 1998-10-06 Northrop Grumman Corporation Multiposition folding control surface for improved launch stability in missiles
DE19960738C1 (en) * 1999-12-16 2001-08-23 Lfk Gmbh Rudder connection for guided missiles
US6315240B1 (en) * 2000-03-02 2001-11-13 Raytheon Company Tactical missile control surface attachment
US6474594B1 (en) * 2001-05-11 2002-11-05 Raytheon Company Output shaft assembly for a missile control actuation unit
RU2482433C1 (en) * 2011-12-07 2013-05-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Unfolding wing of two-stage missile
RU2482434C1 (en) * 2011-12-14 2013-05-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Unfolding wing of two-stage missile
RU2478907C1 (en) * 2011-12-14 2013-04-10 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Unfolding wing of two-stage rocket
US8847134B2 (en) 2012-02-16 2014-09-30 Lockheed Martin Corporation Deployable wing and fin control surface actuation
CN102774494A (en) * 2012-07-06 2012-11-14 北京林业大学 Aircraft folding rudder capable of stretching automatically
RU2520812C1 (en) * 2013-03-05 2014-06-27 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Deployable rudder of missile
RU2520846C1 (en) * 2013-03-29 2014-06-27 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Rocket aerodynamic rudder
RU2532286C1 (en) * 2013-07-16 2014-11-10 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Rocket aerodynamic rudder
CN104677200B (en) * 2015-01-21 2016-05-18 浙江理工大学 One twice-folded aerofoil horizontal spreading mechanism
RU2599677C1 (en) * 2015-08-03 2016-10-10 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Spreading aerodynamic surface
DE102015014368A1 (en) * 2015-11-06 2017-05-11 Mbda Deutschland Gmbh Folding wing for a missile and a missile with at least one folding wing arranged thereon
DE102015014367B4 (en) * 2015-11-06 2020-07-16 Mbda Deutschland Gmbh Folding wing for a missile and missile with at least one folding wing arranged thereon
US10150556B2 (en) 2016-05-23 2018-12-11 The Boeing Company Low-profile wing hinge mechanism
RU169784U1 (en) * 2016-12-16 2017-04-03 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации DETECTED AERODYNAMIC SURFACE OF TWO-STAGE ROCKET
RU2652035C1 (en) * 2016-12-19 2018-04-24 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Mechanism of aircraft outer wings unfolding
RU185462U1 (en) * 2018-02-15 2018-12-07 Общество с ограниченной ответственностью НАУЧНО-ПРОИЗВОДСТВЕННОЕ ОБЪЕДИНЕНИЕ "ЦЕЛЬ" AERODYNAMIC SURFACE DISPLAY NODE OF AIRCRAFT
RU2685407C1 (en) * 2018-06-01 2019-04-17 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Device folding wing consoles aircraft
RU2685635C1 (en) * 2018-06-14 2019-04-22 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Device regulation and fixing the final position of the wings
RU2704687C1 (en) * 2018-11-08 2019-10-30 Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени Академика П.Д. Грушина" Folding aerodynamic aircraft steering wheel
CN112498661B (en) * 2020-12-04 2024-01-30 中国航空工业集团公司沈阳飞机设计研究所 Multifunctional control surface structure

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125956A (en) * 1964-03-24 Fold able fin
US2925966A (en) * 1957-10-08 1960-02-23 Kongelbeck Sverre Folding fin or wing for missiles
NL250199A (en) * 1959-04-13
US3273500A (en) * 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin

Also Published As

Publication number Publication date
GB1307298A (en) 1973-02-14
CH506771A (en) 1971-04-30
DE2023212A1 (en) 1970-11-26
DE2023212B2 (en) 1975-12-18
SE331242B (en) 1970-12-14
NO125114B (en) 1972-07-17
NL7006982A (en) 1970-11-17
NL159783B (en) 1979-03-15
FR2042636B1 (en) 1974-07-12
US3650496A (en) 1972-03-21
BE750400A (en) 1970-10-16

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