DE3827590A1 - Flugkoerper - Google Patents
FlugkoerperInfo
- Publication number
- DE3827590A1 DE3827590A1 DE3827590A DE3827590A DE3827590A1 DE 3827590 A1 DE3827590 A1 DE 3827590A1 DE 3827590 A DE3827590 A DE 3827590A DE 3827590 A DE3827590 A DE 3827590A DE 3827590 A1 DE3827590 A1 DE 3827590A1
- Authority
- DE
- Germany
- Prior art keywords
- missile
- rudder
- angle
- rotor ring
- generators
- 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.)
- Granted
Links
- 238000005096 rolling process Methods 0.000 description 10
- 238000010586 diagram Methods 0.000 description 3
- 230000004308 accommodation Effects 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
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
- F42B10/60—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)
- Control Of Multiple Motors (AREA)
- Superconductive Dynamoelectric Machines (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE3827590A DE3827590A1 (de) | 1988-08-13 | 1988-08-13 | Flugkoerper |
| FR8909837A FR2637064B1 (fr) | 1988-08-13 | 1989-07-21 | Engin volant avec bague de rotor a gouverne orientable |
| US07/389,174 US4964593A (en) | 1988-08-13 | 1989-08-03 | Missile having rotor ring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE3827590A DE3827590A1 (de) | 1988-08-13 | 1988-08-13 | Flugkoerper |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE3827590A1 true DE3827590A1 (de) | 1990-02-22 |
| DE3827590C2 DE3827590C2 (enExample) | 1992-01-23 |
Family
ID=6360838
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE3827590A Granted DE3827590A1 (de) | 1988-08-13 | 1988-08-13 | Flugkoerper |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4964593A (enExample) |
| DE (1) | DE3827590A1 (enExample) |
| FR (1) | FR2637064B1 (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0834717A2 (de) | 1996-10-01 | 1998-04-08 | Daimler-Benz Aerospace Aktiengesellschaft | Ruderstellsystem für einen Lenkflugkörper |
| EP3163250A1 (de) * | 2015-10-27 | 2017-05-03 | I.S.L. Institut Franco-Allemand de Recherches de Saint-Louis | Vollkalibriges, drallstabilisiertes lenkgeschoss mit einer hohen reichweite |
Families Citing this family (68)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3915585A1 (de) * | 1989-05-12 | 1990-11-15 | Diehl Gmbh & Co | Submunitions-flugkoerper |
| FR2657703B1 (fr) * | 1990-01-26 | 1992-04-10 | Thomson Brandt Armements | Dispositif pour la commande d'attitude en roulis d'un projectile stabilise par empennage. |
| GB2244687B (en) * | 1990-06-06 | 1993-10-27 | British Aerospace | Stabilisation systems for aerodynamic bodies. |
| US5115742A (en) * | 1991-06-24 | 1992-05-26 | United States Of America As Represented By The Secretary Of The Navy | Integrated and mechanically aided warhead arming device |
| US5417393A (en) * | 1993-04-27 | 1995-05-23 | Hughes Aircraft Company | Rotationally mounted flexible band wing |
| US5449131A (en) * | 1994-01-28 | 1995-09-12 | Eidetics International, Inc. | Vertical nose strake for aircraft stability and control |
| US5452864A (en) * | 1994-03-31 | 1995-09-26 | Alliant Techsystems Inc. | Electro-mechanical roll control apparatus and method |
| US5654522A (en) * | 1995-06-27 | 1997-08-05 | Thiokol Corporation | Plume enhancement nozzle for achieving flare rotation |
| RU2125701C1 (ru) * | 1998-03-16 | 1999-01-27 | Государственное научно-производственное предприятие "Сплав" | Ракета |
| RU2146353C1 (ru) * | 1998-11-13 | 2000-03-10 | Машиностроительное конструкторское бюро "ФАКЕЛ" им.акад.П.Д.Грушина | Устройство для управления высокоманевренной ракетой |
| AU781698B2 (en) * | 1999-09-16 | 2005-06-09 | Tom Kusic | Spiralling missile- B |
| AUPR303501A0 (en) * | 2001-02-09 | 2001-03-08 | Kusic, Tom | Spiralling missile |
| US6699091B1 (en) | 1999-11-04 | 2004-03-02 | Jon A. Warner | Hand-launchable underwater projectile toy |
| US6708923B2 (en) | 2000-06-26 | 2004-03-23 | Tom Kusic | Aircraft spiralling mechanism |
| AU781621B2 (en) * | 2001-02-09 | 2005-06-02 | Tom Kusic | Spiralling missile - A |
| ITMI20010648A1 (it) | 2001-03-27 | 2002-09-27 | Finmeccanica S P A Alenia Dife | Gruppo di controllo per alette direzionali di missili e/o proiettili |
| AU2002331404B2 (en) * | 2001-06-20 | 2008-05-01 | Tom Kusic | Aircraft spiralling mechanism |
| AUPR583001A0 (en) | 2001-06-20 | 2001-07-12 | Kusic, Tom | Aircraft spiralling mechanism |
| US7635104B1 (en) | 2001-06-22 | 2009-12-22 | Tom Kusic | Aircraft spiraling mechanism with jet assistance—B |
| US7165742B2 (en) * | 2001-06-22 | 2007-01-23 | Tom Kusic | Aircraft spiralling mechanism - B |
| US7093791B2 (en) * | 2001-06-22 | 2006-08-22 | Tom Kusic | Aircraft spiralling mechanism—c |
| US7637453B2 (en) * | 2001-06-22 | 2009-12-29 | Tom Kusic | Aircraft spiraling mechanism with jet assistance - A |
| DE10134785A1 (de) * | 2001-07-17 | 2003-02-06 | Diehl Munitionssysteme Gmbh | Verfahren zur Flugbahnkorrektur ballistisch verschossener drallstabilisierter Artilleriemunition |
| US7231874B2 (en) * | 2001-09-05 | 2007-06-19 | Omnitek Partners Llc | Power supplies for projectiles and other devices |
| US6691948B1 (en) | 2003-04-10 | 2004-02-17 | The United States Of America As Represented By The Secretary Of The Navy | High torque rocket nozzle |
| US7412930B2 (en) * | 2004-09-30 | 2008-08-19 | General Dynamic Ordnance And Tactical Systems, Inc. | Frictional roll control apparatus for a spinning projectile |
| US8033890B2 (en) * | 2005-05-18 | 2011-10-11 | Warner Jon A | Self-propelled hydrodynamic underwater toy |
| WO2007030687A2 (en) * | 2005-09-09 | 2007-03-15 | General Dynamics Ordnance And Tactical Systems | Projectile trajectory control system |
| US10408587B1 (en) * | 2006-04-20 | 2019-09-10 | United States Of America As Represented By The Secretary Of The Army | On-board power generation for rolling motor missiles |
| US7431237B1 (en) * | 2006-08-10 | 2008-10-07 | Hr Textron, Inc. | Guided projectile with power and control mechanism |
| US7800032B1 (en) * | 2006-11-30 | 2010-09-21 | Raytheon Company | Detachable aerodynamic missile stabilizing system |
| DE102006057229B9 (de) * | 2006-12-05 | 2009-03-19 | Diehl Bgt Defence Gmbh & Co. Kg | Drallstabilisierte bahnkorrigierbare Artilleriemunition |
| US7963442B2 (en) * | 2006-12-14 | 2011-06-21 | Simmonds Precision Products, Inc. | Spin stabilized projectile trajectory control |
| US7755012B2 (en) * | 2007-01-10 | 2010-07-13 | Hr Textron, Inc. | Eccentric drive control actuation system |
| US7642491B2 (en) * | 2007-03-19 | 2010-01-05 | Tom Kusic | Aircraft spiraling mechanism with jet assistance—D |
| US7696459B2 (en) * | 2007-06-12 | 2010-04-13 | Hr Textron, Inc. | Techniques for articulating a nose member of a guidable projectile |
| US7791007B2 (en) * | 2007-06-21 | 2010-09-07 | Woodward Hrt, Inc. | Techniques for providing surface control to a guidable projectile |
| US9040885B2 (en) * | 2008-11-12 | 2015-05-26 | General Dynamics Ordnance And Tactical Systems, Inc. | Trajectory modification of a spinning projectile |
| CA2979232A1 (en) | 2009-02-02 | 2010-10-28 | Aerovironment | Multimode unmanned aerial vehicle |
| US8552351B2 (en) * | 2009-05-12 | 2013-10-08 | Raytheon Company | Projectile with deployable control surfaces |
| KR102111900B1 (ko) | 2009-09-09 | 2020-06-05 | 에어로바이론먼트, 인크. | 휴대용 rf 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치 |
| CN106800085B (zh) | 2009-09-09 | 2020-08-18 | 威罗门飞行公司 | 升降副翼控制系统 |
| US8443726B2 (en) * | 2010-02-10 | 2013-05-21 | Omnitek Partners, Llc | Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons |
| US8552349B1 (en) * | 2010-12-22 | 2013-10-08 | Interstate Electronics Corporation | Projectile guidance kit |
| US8426788B2 (en) * | 2011-01-12 | 2013-04-23 | Raytheon Company | Guidance control for spinning or rolling projectile |
| US8884202B2 (en) * | 2011-03-09 | 2014-11-11 | United Launch Alliance, Llc | Integrated vehicle fluids |
| US10717550B1 (en) | 2011-03-09 | 2020-07-21 | United Launch Alliance, L.L.C. | Integrated vehicle fluids |
| US8916810B2 (en) | 2011-03-30 | 2014-12-23 | Raytheon Company | Steerable spin-stabilized projectile |
| SE535991C2 (sv) * | 2011-07-07 | 2013-03-19 | Bae Systems Bofors Ab | Rotationsstabiliserad styrbar projektil och förfarande därför |
| US8993948B2 (en) * | 2011-08-23 | 2015-03-31 | Raytheon Company | Rolling vehicle having collar with passively controlled ailerons |
| US8698059B2 (en) | 2012-05-03 | 2014-04-15 | Raytheon Company | Deployable lifting surface for air vehicle |
| IL224075A (en) * | 2012-12-31 | 2017-11-30 | Bae Systems Rokar Int Ltd | Cheap shell kit and method of use |
| USD729896S1 (en) | 2013-12-19 | 2015-05-19 | Elio Martinez | Air vehicle rotatable wind-driven sleeve |
| US20160238358A1 (en) * | 2014-03-04 | 2016-08-18 | Andrey SOROKIN | Ammunition with electromotor |
| US9464876B2 (en) * | 2014-05-30 | 2016-10-11 | General Dynamics Ordnance and Tacital Systems, Inc. | Trajectory modification of a spinning projectile by controlling the roll orientation of a decoupled portion of the projectile that has actuated aerodynamic surfaces |
| FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
| FR3054030B1 (fr) * | 2016-07-18 | 2018-08-24 | Nexter Munitions | Projectile comprenant un dispositif de deploiement d'une voilure ou ailette |
| US10618668B2 (en) * | 2016-09-06 | 2020-04-14 | Analytical Mechanics Associates, Inc. | Systems and apparatus for controlling movement of objects through a fluid |
| US11555679B1 (en) | 2017-07-07 | 2023-01-17 | Northrop Grumman Systems Corporation | Active spin control |
| US12031802B2 (en) * | 2017-07-26 | 2024-07-09 | Northrop Grumman Systems Corporation | Despun wing control system for guided projectile maneuvers |
| US10996031B1 (en) * | 2017-07-26 | 2021-05-04 | U.S. Government As Represented By The Secretary Of The Army | Free spinning hub for mortar projectiles |
| US10718294B1 (en) | 2017-10-27 | 2020-07-21 | United Launch Alliance, L.L.C. | Integrated vehicle fluids |
| US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
| CN108801242B (zh) * | 2018-04-28 | 2021-06-29 | 沈阳理工大学 | 一种高动态环境下的组合式姿态测量方法 |
| IL263880B (en) * | 2018-12-20 | 2022-02-01 | Elbit Systems Rokar Ltd | Projectile fuze assembly and methods of assembling and use |
| US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
| US11619473B2 (en) * | 2021-01-11 | 2023-04-04 | Bae Systems Information And Electronic Systems Integration Inc. | Command mixing for roll stabilized guidance kit on gyroscopically stabilized projectile |
| US12313389B1 (en) | 2022-03-11 | 2025-05-27 | Northrop Grumman Systems Corporation | Tunable safe and arming devices and methods of manufacture |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3111088A (en) * | 1962-02-27 | 1963-11-19 | Martin Marietta Corp | Target seeking missile |
| US4512537A (en) * | 1973-08-10 | 1985-04-23 | Sanders Associates, Inc. | Canard control assembly for a projectile |
| DE3606423A1 (de) * | 1986-02-27 | 1987-09-03 | Messerschmitt Boelkow Blohm | Rotorsystem in verbindung mit flugkoerpersteuerungen |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4438893A (en) * | 1973-08-10 | 1984-03-27 | Sanders Associates, Inc. | Prime power source and control for a guided projectile |
| FR2321723A1 (fr) * | 1975-07-29 | 1977-03-18 | Thomson Brandt | Systeme de controle d'attitude et engin equipe d'un tel systeme |
| AU546338B2 (en) * | 1980-09-22 | 1985-08-29 | Commonwealth Of Australia, The | Stabilising rotating body |
| US4565340A (en) * | 1984-08-15 | 1986-01-21 | Ford Aerospace & Communications Corporation | Guided projectile flight control fin system |
-
1988
- 1988-08-13 DE DE3827590A patent/DE3827590A1/de active Granted
-
1989
- 1989-07-21 FR FR8909837A patent/FR2637064B1/fr not_active Expired - Fee Related
- 1989-08-03 US US07/389,174 patent/US4964593A/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3111088A (en) * | 1962-02-27 | 1963-11-19 | Martin Marietta Corp | Target seeking missile |
| US4512537A (en) * | 1973-08-10 | 1985-04-23 | Sanders Associates, Inc. | Canard control assembly for a projectile |
| DE3606423A1 (de) * | 1986-02-27 | 1987-09-03 | Messerschmitt Boelkow Blohm | Rotorsystem in verbindung mit flugkoerpersteuerungen |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0834717A2 (de) | 1996-10-01 | 1998-04-08 | Daimler-Benz Aerospace Aktiengesellschaft | Ruderstellsystem für einen Lenkflugkörper |
| EP0834717A3 (de) * | 1996-10-01 | 1999-05-06 | LFK Lenkflugkörpersysteme GmbH | Ruderstellsystem für einen Lenkflugkörper |
| US5975461A (en) * | 1996-10-01 | 1999-11-02 | Lfk-Lenkflugkorpersysteme Gmbh | Vane control system for a guided missile |
| EP3163250A1 (de) * | 2015-10-27 | 2017-05-03 | I.S.L. Institut Franco-Allemand de Recherches de Saint-Louis | Vollkalibriges, drallstabilisiertes lenkgeschoss mit einer hohen reichweite |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2637064A1 (fr) | 1990-03-30 |
| FR2637064B1 (fr) | 1994-05-13 |
| DE3827590C2 (enExample) | 1992-01-23 |
| US4964593A (en) | 1990-10-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OP8 | Request for examination as to paragraph 44 patent law | ||
| D2 | Grant after examination | ||
| 8364 | No opposition during term of opposition | ||
| 8327 | Change in the person/name/address of the patent owner |
Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE |
|
| 8327 | Change in the person/name/address of the patent owner |
Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M |
|
| 8339 | Ceased/non-payment of the annual fee |