[특허]Adaptable launching system

Lockheed Martin Corporation

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특허 상세정보

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내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Adaptable launching system

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41F-003/04
미국특허분류(USC)	089/001.817;
출원번호	US-0274409 (2008-11-20)
등록번호	US-8397613 (2013-03-19)
발명자 / 주소	Skurdal, Daniel A. Fouts, Timothy R. Houston-Manchester, Jennifer L. Snediker, John
출원인 / 주소	Lockheed Martin Corporation
대리인 / 주소	Kaplan Breyer Schwarz & Ottesen, LLP
인용정보	피인용 횟수 : 2 인용 특허 : 10

초록

A launch system for use as a standalone munition launcher or as a guest launcher within a main battery host launcher.

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1. An apparatus comprising: a single cell vertical launch system that is suitable for: (i) use as a guest launcher within a host launcher, and(ii) launching one or more canistered munitions,the single cell vertical launch system comprising: (A) an enclosure having a sealing bulkhead that separates the enclosure into a munitions compartment and an electronics compartment, wherein the enclosure is dimensioned and arranged to be received by a cell within the host launcher;(B) a munitions adapter disposed in the munitions compartment, wherein the munitions adapter is munition-specific and receives the canistered munition(C) launch control electronics disposed at least in part in the electronics compartment, wherein the launch control electronics is munition-specific and coordinates at least some control and communications between the single cell vertical launch system and the host launcher. 2. The apparatus of claim 1 further comprising the host launcher, wherein the host launcher has a plurality of cells, and wherein the single cell vertical launch system is disposed in one of the cells. 3. The apparatus of claim 2 wherein the host launcher is one of a MK 41 VLS and a MK 57 VLS. 4. The apparatus of claim 2 wherein the electronics compartment comprises an access way, wherein the access way provides access to the electronics compartment when the launch system is installed in the cell of the host launcher. 5. The apparatus of claim 1 wherein a top of the launch system is open until the top seals against a hatch and deck assembly of the host launcher. 6. The apparatus of claim 1 wherein the canistered munition is a missile. 7. The apparatus of claim 1 wherein the canistered munition is an unmanned aerial vehicle. 8. The apparatus of claim 1 wherein the canistered munition is an active decoy. 9. The apparatus of claim 1 wherein the canistered munition is an all-up-round. 10. The apparatus of claim 6 wherein the missile is selected from the group consisting of a rolling airframe missile, a precision attack missile, and a Hellfire missile. 11. The apparatus of claim 1 wherein the launch control electronics comprises: munition-specific electronics for providing power, data, and ordnance activation to the munition and for performing at least some launch control functions; anda launch control module for coordinating communications between a weapon control system of the munition and the munition-specific electronics. 12. The apparatus of claim 1 wherein the received canistered munition is one of either (i) a first canistered munition or (ii) a second canistered munition that differ from one another in at least one characteristic selected from length, diameter, or shape, and further wherein the structure of the munitions adapter is changeable as a function of whether the received canistered munition is the first canistered munitions or the second canistered munition. 13. A single cell vertical launch system comprising: (A) an enclosure having a sealing bulkhead that physically segregates the enclosure into a munitions compartment and an electronics compartment, wherein the enclosure is dimensioned and arranged to be received by a cell within a host launcher;(B) a munitions adapter, wherein the munitions adapter is disposed in the munitions compartment, and wherein: (i) the munitions adapter receives canistered munitions; and(ii) a structure of the munitions adapter is configured as a function of whether the canistered munitions are first canistered munitions or second canistered munitions, wherein the first canistered munitions and the second canistered munitions differ from one another in at least one characteristic selected from length, diameter, or shape of the munition; and(C) launch control electronics adapted to coordinate at least some control and communications between the single cell vertical launch system and the host launcher, wherein the launch control electronics is disposed in the electronics compartment, and wherein the launch control electronics is configured as a function of whether the canistered munitions are first canistered munitions or second canistered munitions;wherein the single cell vertical launch system is suitable for: (i) use as a guest launcher within the host launcher, and(ii) launching one or more of the canistered munitions. 14. The single cell vertical launch system of claim 13 wherein: when the munitions adapter receives the first canistered munitions, the munitions adapter comprises a first munitions-specific frame assembly having a first configuration suitable for receiving the first canistered munitions; andwhen the munitions adapter receives the second canistered munitions, the munitions adapter comprises a second munitions-specific frame assembly having a second configuration suitable for receiving the second canistered munitions,wherein the first configuration and the second configuration are different from one another. 15. The single cell vertical launch system of claim 13 wherein the first canistered munitions and the second canistered munitions differ from one another in length, and further wherein: when the munitions adapter receives the first canistered munitions, the munitions adapter comprises a first munitions extension assembly having a first length related to the length of the first canistered munitions; andwhen the munitions adapter receives the second canistered munitions, the munitions adapter comprises a second munitions extension assembly having a second length related to the length of the second canistered munitions,wherein the first length and the second length are different from one another. 16. The single cell vertical launch system of claim 13 wherein: when the munitions adapter receives the first canistered munitions, the launch control electronics comprises a first instantiation that is suitable for controlling launch of the first canistered munitions; andwhen the munitions adapter receives the second canistered munitions, the launch control electronics comprises a second instantiation that is suitable for controlling launch of the second canistered munitions,wherein the first instantiation and the second instantiation differ from one another. 17. An apparatus comprising: a single cell vertical launch system that is suitable for: (i) use as a guest launcher within a host launcher, and(ii) launching one or more canistered munitions,the single cell vertical launch system comprising: (A) an enclosure having a sealing bulkhead that separates the enclosure into a munitions compartment and an electronics compartment, wherein the enclosure is dimensioned and arranged to be received by a cell within the host launcher;(B) a munitions adapter disposed in the munitions compartment, wherein the munitions adapter receives the canistered munition, and wherein the received canistered munition is one of either a first canistered munition or a second canistered munition that differ from one another in at least one characteristic selected from length, diameter, or shape, and further wherein the structure of the munitions adapter is changeable as a function of whether the received canistered munition is the first canistered munitions or the second canistered munition; and(C) launch control electronics that coordinates at least some control and communications between the launch system and the host launcher, wherein the launch control electronics is disposed in the electronics compartment and has a configuration that depends on whether the canistered munition is the first canistered munition or the second canistered munition. 18. The apparatus of claim 17 further comprising the host launcher, wherein the host launcher has a plurality of cells, and wherein the single cell vertical launch system is disposed in one of the cells.

이 특허에 인용된 특허 (10)

이 특허를 인용한 특허 피인용횟수: 2

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구성항목	관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
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특허 상세정보

Adaptable launching system

초록

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이 특허에 인용된 특허 (10)

이 특허를 인용한 특허 피인용횟수: 2

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특허 상세정보

Adaptable launching system

초록

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이 특허에 인용된 특허 (10)

이 특허를 인용한 특허 피인용횟수: 2

IPC 상위 출원인

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상세정보조회

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IPC 상세정보(version : 201201)

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