DE502006000632D1 - Flügelanordnung sowie Flugkörper - Google Patents

Flügelanordnung sowie Flugkörper

Info

Publication number: DE502006000632D1
Authority: DE; Germany
Prior art keywords: missile; wing arrangement; wing; arrangement
Prior art date: 2005-06-07
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.): Active

Application number

DE502006000632T

Other languages

English (en)

Inventor

Peter Gerd Fisch

Alexander Stengele

Gerd Elsner

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.)

Diehl Defence GmbH and Co KG

Original Assignee

Diehl BGT Defence GmbH and Co KG

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.)

2005-06-07

Filing date

2006-05-16

Publication date

2008-05-29

2006-05-16 Application filed by Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG

2008-05-29 Publication of DE502006000632D1 publication Critical patent/DE502006000632D1/de

Status Active legal-status Critical Current

2026-05-17 Anticipated expiration legal-status Critical

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
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail 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)

DE502006000632T 2005-06-07 2006-05-16 Flügelanordnung sowie Flugkörper Active DE502006000632D1 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
DE102005026070A DE102005026070B4 (de)	2005-06-07	2005-06-07	Flügelanordnung sowie Flugkörper

Publications (1)

Publication Number	Publication Date
DE502006000632D1 true DE502006000632D1 (de)	2008-05-29

Family

ID=36942557

Family Applications (2)

Application Number	Title	Priority Date	Filing Date
DE102005026070A Expired - Fee Related DE102005026070B4 (de)	2005-06-07	2005-06-07	Flügelanordnung sowie Flugkörper
DE502006000632T Active DE502006000632D1 (de)	2005-06-07	2006-05-16	Flügelanordnung sowie Flugkörper

Family Applications Before (1)

Application Number	Title	Priority Date	Filing Date
DE102005026070A Expired - Fee Related DE102005026070B4 (de)	2005-06-07	2005-06-07	Flügelanordnung sowie Flugkörper

Country Status (3)

Country	Link
US (1)	US20070075183A1 (de)
EP (1)	EP1731871B1 (de)
DE (2)	DE102005026070B4 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US7800032B1 (en) *	2006-11-30	2010-09-21	Raytheon Company	Detachable aerodynamic missile stabilizing system
DE102010025174A1 (de) *	2010-06-25	2011-12-29	Rheinmetall Waffe Munition Gmbh	Flugkörper, insbesondere Mörsergranate
US12050092B2 (en)	2022-09-22	2024-07-30	Raytheon Company	Mechanism for attachment and detachment of an airfoil to an airframe
CN115615258B (zh) *	2022-10-31	2025-11-11	湖南光华防务科技集团有限公司	一种弹翼结构及其安装方法
CN116878340B (zh) *	2023-09-07	2023-12-29	北京爱思达航天科技有限公司	一种大承载轻质复合材料飞行翼及其制备方法
KR102724855B1 (ko) *	2024-05-27	2024-11-01	주식회사 유에이엠테크	유도 미사일 타입의 무인 비행체

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US1509336A (en) *	1922-06-27	1924-09-23	William A Borden	Stabilizer or fin assembly of a bomb
US1515705A (en) *	1923-05-04	1924-11-18	Short Frank	Bomb
US2597703A (en) *	1946-02-07	1952-05-20	Us Navy	Rocket fin
US2771842A (en) *	1953-08-21	1956-11-27	Hillmer Willy	Toggle clamp fin retaining band
DE1116577B (de) *	1959-11-21	1961-11-02	Kunststofftechnische Studienge	Leitwerksfluegel aus Kunststoff fuer Raketen
FR1307270A (fr) *	1961-06-08	1962-10-26	Le Ministre Des Armees Terre D	Empennage pour projectile et son procédé d'assemblage
DE1897816U (de) *	1964-04-21	1964-07-30	J G W Berckholtz Fa	Stabilisierhuelse fuer flugkoerper, insbesondere raketen.
US3374969A (en) *	1966-07-28	1968-03-26	Army Usa	Stabilized projectile
SE339646B (de) *	1970-01-08	1971-10-11	Bofors Ab
US3633846A (en) *	1970-05-28	1972-01-11	Us Navy	Expandable aerodynamic fin
US4708304A (en) *	1985-12-27	1987-11-24	General Dynamics, Pomona Division	Ring-wing
FR2630502B1 (fr) *	1988-04-25	1990-08-31	Europ Propulsion	Propulseur composite a ailes composites integrees et son procede de fabrication
DE8901940U1 (de) *	1989-02-18	1989-05-11	Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn	Flugkörper mit Leitwerksflossen
DE3927798A1 (de) *	1989-08-23	1991-03-14	Rheinmetall Gmbh	Fluegelstabilisiertes geschoss
US5927643A (en) *	1997-11-05	1999-07-27	Atlantic Research Corporation	Self-deploying airfoil for missile or the like

2005
- 2005-06-07 DE DE102005026070A patent/DE102005026070B4/de not_active Expired - Fee Related
2006
- 2006-05-16 US US11/434,712 patent/US20070075183A1/en not_active Abandoned
- 2006-05-16 EP EP06010013A patent/EP1731871B1/de not_active Ceased
- 2006-05-16 DE DE502006000632T patent/DE502006000632D1/de active Active

Also Published As

Publication number	Publication date
EP1731871B1 (de)	2008-04-16
DE102005026070A1 (de)	2006-12-14
US20070075183A1 (en)	2007-04-05
EP1731871A1 (de)	2006-12-13
DE102005026070B4 (de)	2009-07-09

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DE602007010795D1 (de)	2011-01-05	Blattsauger und -häcksler
DK1954140T3 (da)	2013-06-17	Glycerollevulinatketaler og deres anvendelse
EP1913800A4 (de)	2016-09-21	Nanoelektromechanische und mikroelektromechanische sensoren und analysierer
DK1979612T3 (da)	2013-05-21	Vindturbinesamling og relateret fremgangsmåde
DE102004001078B8 (de)	2013-06-13	Flugzeugrumpf
DE602006011217D1 (de)	2010-01-28	Erweiterte dekompressionsklappenanordnung
DE502006002383D1 (de)	2009-01-29	Turbinenrad
ITMI20050119A1 (it)	2006-07-29	Struttura di pannello e relativo procedimento di realizzazione
FI20055682A0 (fi)	2005-12-20	Läpivientiosa sekä menetelmä
ATE534012T1 (de)	2011-12-15	Unterkalibriges geschoss
DE502006000632D1 (de)	2008-05-29	Flügelanordnung sowie Flugkörper
DE502005004418D1 (de)	2008-07-24	Turbolader
DE502006000665D1 (de)	2008-06-05	Penetrator
DE112007002194A5 (de)	2009-07-02	Flügelanordnung
FI6964U1 (fi)	2006-02-13	Kiinnityslaite
DE502005009943D1 (de)	2010-09-02	Flugkörper
DE112005000940A5 (de)	2007-05-24	Flugkörper
NO20052966D0 (no)	2005-06-16	Monsterkodede ordboker
ATA9842004A (de)	2005-10-15	Flügel
ES1059550Y (es)	2005-08-16	Cohete pirotecnico mejorado
FI20055138A0 (fi)	2005-03-29	Yhdistetty metsänhakkuu- ja korjuukone
NO20051063L (no)	2006-08-28	Ballistisk beskyttelse
AT504332B8 (de)	2008-09-15	Chokerseil und chokerseilsystem
ITUD20050049A1 (it)	2006-10-02	Aeroplano

Legal Events

Date	Code	Title	Description
2009-05-07	8364	No opposition during term of opposition