EP0186903B1 - Klappleitwerk für flügelstabilisierte Raketengeschosse - Google Patents

Klappleitwerk für flügelstabilisierte Raketengeschosse Download PDF

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Publication number
EP0186903B1
EP0186903B1 EP19850116566 EP85116566A EP0186903B1 EP 0186903 B1 EP0186903 B1 EP 0186903B1 EP 19850116566 EP19850116566 EP 19850116566 EP 85116566 A EP85116566 A EP 85116566A EP 0186903 B1 EP0186903 B1 EP 0186903B1
Authority
EP
European Patent Office
Prior art keywords
wings
journal
annular groove
fin
bearing
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 - Lifetime
Application number
EP19850116566
Other languages
German (de)
English (en)
French (fr)
Other versions
EP0186903A1 (de
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.)
JOSEF LUBIG GMBH
Original Assignee
Josef Lubig 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 Josef Lubig GmbH filed Critical Josef Lubig GmbH
Publication of EP0186903A1 publication Critical patent/EP0186903A1/de
Application granted granted Critical
Publication of EP0186903B1 publication Critical patent/EP0186903B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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

Definitions

  • the installation process can be automated and the journals can be straight, as a result of which a much better mounting of the wings is achieved than would be possible with curved axes, which are required for accommodating a plurality of wings.

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Toys (AREA)
  • Support Of The Bearing (AREA)
EP19850116566 1984-12-31 1985-12-24 Klappleitwerk für flügelstabilisierte Raketengeschosse Expired - Lifetime EP0186903B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3447852 1984-12-31
DE19843447852 DE3447852A1 (de) 1984-12-31 1984-12-31 Klappleitwerk fuer fluegelstabilisierte raketengeschosse

Publications (2)

Publication Number Publication Date
EP0186903A1 EP0186903A1 (de) 1986-07-09
EP0186903B1 true EP0186903B1 (de) 1993-07-21

Family

ID=6254146

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19850116566 Expired - Lifetime EP0186903B1 (de) 1984-12-31 1985-12-24 Klappleitwerk für flügelstabilisierte Raketengeschosse

Country Status (2)

Country Link
EP (1) EP0186903B1 (enrdf_load_stackoverflow)
DE (2) DE3447852A1 (enrdf_load_stackoverflow)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19906969B4 (de) * 1999-02-19 2004-10-14 Rheinmetall W & M Gmbh Aus einem Waffenrohr verschießbares leitwerkstabilisiertes Geschoß

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4691880A (en) * 1985-11-14 1987-09-08 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
DE3937743A1 (de) * 1989-11-13 1991-05-16 Deutsch Franz Forsch Inst Flugkoerper
DE102007002948B4 (de) 2007-01-19 2009-04-02 Diehl Bgt Defence Gmbh & Co. Kg Vorrichtung zur Tragflächenentfaltung
CN114322677B (zh) * 2021-12-29 2024-05-28 西安现代控制技术研究所 一种适应舱体的弹翼、滑块精准安装结构

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE224404C (de) * 1909-04-20 1910-07-19 Zeiss Carl Stativ bestehend aus einem Kopf und drei Beinen die je durch ein Gelenk von fester Achse mit dem Kopf verbunden sind
US2430896A (en) * 1944-01-08 1947-11-18 Edward G Uhl Rocket stabilizing fins
NL295319A (enrdf_load_stackoverflow) * 1960-07-11
FR1351422A (fr) * 1962-10-05 1964-02-07 Soc Tech De Rech Ind Perfectionnements aux roquettes
DE1578222A1 (de) * 1966-02-04 1972-02-10 Ind & Mecaniques S T R I M Sich entfaltendes Leitwerk,insbesondere fuer Raketen Societe Technique de Recherches
FR2070389A5 (enrdf_load_stackoverflow) * 1969-12-03 1971-09-10 Serat
BE759788A (fr) * 1969-12-05 1971-06-03 Sarmac Sa Projectile autopropulse empenne
DE2342783C2 (de) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Mit einem Leitwerk versehenes Geschoß

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19906969B4 (de) * 1999-02-19 2004-10-14 Rheinmetall W & M Gmbh Aus einem Waffenrohr verschießbares leitwerkstabilisiertes Geschoß

Also Published As

Publication number Publication date
DE3447852A1 (de) 1986-08-28
DE3447852C2 (enrdf_load_stackoverflow) 1991-02-28
EP0186903A1 (de) 1986-07-09
DE3587471D1 (de) 1993-08-26

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