DE102017003797A1 - Zweigeteilter klappflügel für flugkörperleitwerke - Google Patents

Zweigeteilter klappflügel für flugkörperleitwerke Download PDF

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Publication number
DE102017003797A1
DE102017003797A1 DE102017003797.3A DE102017003797A DE102017003797A1 DE 102017003797 A1 DE102017003797 A1 DE 102017003797A1 DE 102017003797 A DE102017003797 A DE 102017003797A DE 102017003797 A1 DE102017003797 A1 DE 102017003797A1
Authority
DE
Germany
Prior art keywords
wing
folding
missile
edge
joint
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.)
Ceased
Application number
DE102017003797.3A
Other languages
German (de)
English (en)
Inventor
Wolf-Dieter Mast
Wolfgang Hierl
Anton Kühnel
Philipp Wagner
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.)
MBDA Deutschland GmbH
Original Assignee
MBDA Deutschland GmbH
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 MBDA Deutschland GmbH filed Critical MBDA Deutschland GmbH
Priority to DE102017003797.3A priority Critical patent/DE102017003797A1/de
Priority to EP17204149.3A priority patent/EP3392603B1/de
Priority to ES17204149T priority patent/ES2775423T3/es
Publication of DE102017003797A1 publication Critical patent/DE102017003797A1/de
Ceased legal-status Critical Current

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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
    • F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

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)
  • Tires In General (AREA)
DE102017003797.3A 2017-04-19 2017-04-19 Zweigeteilter klappflügel für flugkörperleitwerke Ceased DE102017003797A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE102017003797.3A DE102017003797A1 (de) 2017-04-19 2017-04-19 Zweigeteilter klappflügel für flugkörperleitwerke
EP17204149.3A EP3392603B1 (de) 2017-04-19 2017-11-28 Zweigeteilter klappflügel für flugkörperleitwerke
ES17204149T ES2775423T3 (es) 2017-04-19 2017-11-28 Ala plegable de dos partes para colas de misiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102017003797.3A DE102017003797A1 (de) 2017-04-19 2017-04-19 Zweigeteilter klappflügel für flugkörperleitwerke

Publications (1)

Publication Number Publication Date
DE102017003797A1 true DE102017003797A1 (de) 2018-10-25

Family

ID=60484210

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102017003797.3A Ceased DE102017003797A1 (de) 2017-04-19 2017-04-19 Zweigeteilter klappflügel für flugkörperleitwerke

Country Status (3)

Country Link
EP (1) EP3392603B1 (es)
DE (1) DE102017003797A1 (es)
ES (1) ES2775423T3 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10429159B2 (en) * 2017-06-27 2019-10-01 Raytheon Company Deployable airfoil airborne body and method of simultaneous translation and rotation to deploy
CN114537640B (zh) * 2022-02-15 2023-08-25 中天长光(青岛)装备科技有限公司 一种双自由度折叠翼机构

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US17312A (en) 1857-05-19 Improvement in projectiles
US3273500A (en) 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin
DE3038158A1 (de) * 1979-10-09 1981-04-23 Aktiebolaget Bofors, 69180 Bofors Herausklappbare leitflaeche
GB1597098A (en) * 1971-06-23 1981-09-03 British Aerospace Missiles
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
DE3533994A1 (de) 1984-09-25 1986-04-30 Rheinmetall GmbH, 4000 Düsseldorf Leitwerk mit entfaltbaren fluegeln
US4778127A (en) 1986-09-02 1988-10-18 United Technologies Corporation Missile fin deployment device
US4796835A (en) 1986-12-17 1989-01-10 The Marquardt Company Projectile
DE3838735A1 (de) * 1988-11-15 1990-05-31 Diehl Gmbh & Co Klapp-fluegel, insbesondere fuer ein geschoss
DE102015004703A1 (de) 2014-12-11 2016-06-16 Mbda Deutschland Gmbh Klappflügelsystem

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2959143A (en) * 1954-02-02 1960-11-08 Endrezze William Eugene Radial expanding taper formed movable fins for missles or torpedos
DE1203647B (de) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Flossenleitwerk, insbesondere fuer Raketengeschosse
US4106727A (en) * 1977-05-09 1978-08-15 Teledyne Brown Engineering, A Division Of Teledyne Industries, Inc. Aircraft folding airfoil system

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US17312A (en) 1857-05-19 Improvement in projectiles
US3273500A (en) 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin
GB1597098A (en) * 1971-06-23 1981-09-03 British Aerospace Missiles
DE3038158A1 (de) * 1979-10-09 1981-04-23 Aktiebolaget Bofors, 69180 Bofors Herausklappbare leitflaeche
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
DE3533994A1 (de) 1984-09-25 1986-04-30 Rheinmetall GmbH, 4000 Düsseldorf Leitwerk mit entfaltbaren fluegeln
US4778127A (en) 1986-09-02 1988-10-18 United Technologies Corporation Missile fin deployment device
US4796835A (en) 1986-12-17 1989-01-10 The Marquardt Company Projectile
DE3838735A1 (de) * 1988-11-15 1990-05-31 Diehl Gmbh & Co Klapp-fluegel, insbesondere fuer ein geschoss
DE102015004703A1 (de) 2014-12-11 2016-06-16 Mbda Deutschland Gmbh Klappflügelsystem

Also Published As

Publication number Publication date
ES2775423T3 (es) 2020-07-27
EP3392603B1 (de) 2020-01-08
EP3392603A1 (de) 2018-10-24

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R012 Request for examination validly filed
R002 Refusal decision in examination/registration proceedings
R003 Refusal decision now final