[특허]Airborne guided shell

Airborne guided shell 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41G-007/00 F42B-015/01 F42B-010/62 F42B-015/00 F42B-010/60
출원번호	US-0375654 (2007-10-23)
등록번호	US-8278611 (2012-10-02)
우선권정보	IL-178840 (2006-10-24)
국제출원번호	PCT/IL2007/001267 (2007-10-23)
§371/§102 date	20091001 (20091001)
국제공개번호	WO2008/050322 (2008-05-02)
발명자 / 주소	Shpund, Zalman Shlomo Sahar, David
출원인 / 주소	Rafael Advanced Defense Systems Ltd.
대리인 / 주소	Merchant & Gould P.C.
인용정보	피인용 횟수 : 0 인용 특허 : 33

초록 ▼

A kit for upgrading a non-guided shell to an airborne guided shell includes a device to couple the kit to the body of the non-guided shell. A fastener provides for fastening the resulting airborne shell to an aircraft and for detaching it there from. The kit also provides for causing the trajectory of the shell to change once detached from the aircraft according to instructions received in the kit; for determining the position of the shell; and for transferring data from the carrying platform to the guidance kit.

대표청구항 ▼

1. An airborne guided shell, comprising a non-guided artillery shell, coupled with a guiding kit, said guiding kit comprising means for receiving at least navigation data from a carrying platform, and means at said guiding kit for causing the trajectory of the guided shell once detached from the carrying platform to change based on said at least navigation data as received from said carrying platform. 2. A shell according to claim 1, wherein the guiding kit is securely coupled to the body of the shell. 3. A shell according to claim 1, wherein the non-guided artillery shell is a 155 mm shell. 4. A shell according to claim 1, wherein the non-guided artillery shell is a mortar shell. 5. An airborne guided shell according to claim 1, wherein means for receiving at least navigation data from the carrying platform is selected from the group consisting of: mission data, flight direction, and electric power. 6. A kit for upgrading a non-guidable shell to an airborne guidable shell, comprising: means for coupling said kit to the body of said non-guidable shell;means for fastening the airborne guidable shell to an aircraft and for detaching the airborne guidable shell therefrom;means for causing the trajectory of the airborne guidable shell to change, once detached from the aircraft, according to instructions received in the kit; andmeans for determining the position of the airborne guidable shell;means for receiving at least navigation data from the carrying platform. 7. A kit according to claim 6, wherein the means for causing the trajectory of the airborne guidable shell to change comprise one or more flaps, each flap being movable by a servo mechanism. 8. A kit according to claim 6, wherein the means for determining the position of the airborne guidable shell comprise a GPS system. 9. A method for adapting a non-guided artillery shell that allows a shell to be guided, said method comprising coupling said non-guided artillery shell with a guiding kit, said guiding kit comprising means for receiving at least navigation data from a carrying platform, and means at said guiding kit for causing the trajectory of said adapted shell to change once detached from the platform based on said at least navigation data. 10. A method according to claim 9, comprising coupling the guiding kit to the body of the shell. 11. A method according to claim 9, further comprising: coupling said kit to the body of said non-guided shell;fastening the adapted airborne shell to an aircraft or detaching said adapted airborne shell there from;causing the trajectory of the adapted airborne shell to change, once detached from the aircraft, according to instructions received in the kit;determining the position of the adapted airborne shell; andtransferring at least navigation data from the carrying platform to the guidance kit. 12. A method according to claim 11, wherein the means for causing the trajectory of the shell to change comprise one or more flaps, each flap being movable by a servo mechanism. 13. A method according to claim 11, wherein the means for determining the position of the shell comprise a GPS system. 14. A method according to claim 9, wherein the non-guided artillery shell is a 155 mm shell. 15. A method according to claim 9, wherein the non-guided artillery shell is a mortar shell.

이 특허에 인용된 특허 (33)

Linick James M. (P.O. Box 1512 La Quinta CA 92253), Apparatus and method for remote guidance of cannon-launched projectiles.
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Fortunko Chris M. (Newport Beach CA), Apparatus for transmititng data to a projectile positioned within a gun tube.
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Steuer Raimar (Leinburg DEX), Artillery rocket.
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Abbott Anthony Steven, GPS guided munition.
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Bardash ; Manuel L. ; Clasen ; Carl P. ; Scudder ; Robert M. ; Simon ; L awrence H. ; Sorkin ; Charles S. ; Yavne ; Raphael O. ; Ekis ; Robert W . ; Mintzer ; Alfred I., Ground-controlled guided-missile system.
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Vig John R. ; Waugh Steven W., Guided artillery projectile and method.
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Schneider, Arthur J., Guided kinetic penetrator.
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Friedrich, William A.; Johnson, Lyle H.; Conrad, Mark K., Integration of a semi-active laser seeker into the DSU-33 proximity sensor.
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Arnold Keith P. (Canoga Park CA) Humm Lawrence A. (West Hills CA) Pan Han S. (Newbury Park CA) Yu I-Ping (Thousand Oaks CA) Rosen Robert (Granada Hill CA), Launcher control system.
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Stubbs David W. (Tuscon AZ) Laney William P. (Camarillo CA) Rosen Robert (Granada Hills CA) McCaman Brock G. (Chatsworth CA), Launcher control system for surface launched active radar missiles.
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Siering Erik R. (Woodland Hills CA), Method and apparatus for a reprogrammable program missile memory.
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Yaacov Frucht IL, Method and system for guiding submunitions.
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Terzian John (Winchester MA), Microprogram controlled digital processor having addressable flip/flop section.
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Feld Charles M. (Canoga Park CA) Griggs Darrin C. (Canoga Park CA) Humm Larry A. (West Hills CA), Missile interface unit.
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McGlynn Maureen P. (Huntingdon Valley PA) Meiklejohn William D. (Warminster PA), Multiple smart weapons employment mechanism.
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Mayersak Joseph R., Precision guidance system for aircraft launched bombs.
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Mayersak Joseph R., Precision guidance system for aircraft launched bombs.
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Mayersak Joseph R. (Ashburn VA), Precision guidance system for aircraft launched bombs.
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Mayersak Joseph R. (Ashburn VA), Precision guidance system for aircraft launched bombs.
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Ratkovic, Joseph A., Projectile guidance with accelerometers and a GPS receiver.
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Ratkovic, Joseph A.; Brockstein, Allan J.; Buchler, Robert J., Projectile guidance with accelerometers and a GPS receiver.
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Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX), Projectile with correctable trajectory.
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Krikorian,Kapriel V.; Rosen,Robert A., Pseudo GPS aided multiple projectile bistatic guidance.
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Oaks Richard W. (Tucson AZ), Retrofit digital electronics unit for a tube-launched missile.
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Paley Isadore R. (Rockaway NJ), Steerable artillery projectile.
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Hsu Hui-Pin (Northridge CA), Switching control for multiple fiber-guided missile systems.
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Moshe Shnaps IL, System and method for munition impact assessment.
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Mayersak, Joseph R.; Benedict, Lance H.; Krass, Robert M., System for clearing buried and surface mines.
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Thomas, Steve H.; Hager, James R., Systems and methods for guiding munitions.
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Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L., Trajectory correction kit.
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Levita Gideon (Haifa ILX), Upgrading fire control systems.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Airborne guided shell 원문보기

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