[특허]Aircraft with interchangeable fuselage

Aircraft with interchangeable fuselage 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-001/00
출원번호	US-0014183 (1987-02-11)
발명자 / 주소	O\Quinn Russell P. (Long Beach CA) Culver Irven H. (Playa Del Rey CA)
출원인 / 주소	Flight Concepts Limited Partnership (Englewood CA 02)
인용정보	피인용 횟수 : 29 인용 특허 : 0

초록 ▼

An aircraft is set forth having a fuselage (22) which terminates at a forward bulkhead (38). Secured to the fuselage (22) to complete the aerodynamic shape of the aircraft is one or a number of interchangeable, mission specific nose modules (46). A plurality of sleeves (66) is disposed on the fuselage (22) at the forward bulkhead (38) and a like number of corresponding pins (106) are positioned at the nose module (46), reception of the pins (106) into the sleeves (66) as the nose module (46) is mated to the fuselage (22) providing for first gross positional alignment and, as the pins (106) approach full insertion into the sleeves (66), fine positional alignment for interconnection. Couplers (68, 70) are included to provide connection between any electronics in the nose module (46) and monitoring/control electronics disposed on the fuselage (22) and its cockpit (26). The couplers can accommodate six degrees of malalignment to receive the other fixed portion of the coupling for interconnection thereof. Upon mating of the nose module (46) to the fuselage (22), connectors such as over center clamps (112) afix the nose module (46) to its fuselage (22). If desired, the aircraft may also be provided with interchangeable tail modules (126) which include pins (106) and couplers (68, 70) like the nose modules (46) to facilitate their interconnection to and interchange between aircraft. The interchangeability of the tail and nose modules (126, 46) between aircraft gives a small contingent of such aircraft a wide variety of mission capabilities.

대표청구항 ▼

An aircraft with interchangeable sections of fuselage, said aircraft comprising: a basic fuselage having a longitudinal centerline and including a cockpit with controls, a wing structure and flight propulsion means, said basic fuselage having an internal load-bearing structure and an external skin and including at at least one end thereof a transverse, generally planar bulkhead and a structurally integral tongue axially extending from the bottom of said basic fuselage beyond said bulkhead; a set of at least two fuselage sections each having an internal load-bearing structure and an external skin and a transverse, generally planar bulkhead at a mating end thereof, each said section being interchangeably connectable at the mating end thereof to the one end of said basic fuselage and being so shaped to complete the aerodynamic configuration at said one end of said aircraft, said sections being adapted to operatively support different mission-specific equipment; first means for structurally connecting each said section with said one end, said first connecting means comprising notch means at the bottom of each said section for matingly receiving said tongue in supporting engagement with the load-bearing structure thereof, coupling means for defining and supporting each said section in predetermined mated relation with the one end of said basic fuselage, said coupling means including a radially-spaced array of elongated coupling elements fixed to the load-bearing structure of and axially extending through the bulkhead of one of said basic fuselage and sections and a radially-spaced array of elongated receiving elements fixed to the load-bearing structure of and open for cooperatively receiving said coupling elements through the bulkhead of the other of said basic fuselage and sections, said coupling and receiving elements cooperating to progressively align said sections with said one end during movement of said sections toward said one end and to support said sections in said mated relation, and means radially spaced from said coupling means for fixing said sections to said one end; and second means for operatively connecting said sections to said one end, said second connecting means comprising male and female electrical connectors mounted in cooperative relation in the respective bulkheads of said sections and said basic fuselege, at least one of said electrical connectors being resiliently mounted to accommodate six degrees of misalignment with said other electrical connector during movement of said sections into mated relation.

이 특허를 인용한 특허 (29)

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Mills,Christopher J., Overhead space access conversion monument and service area staircase and stowage system.
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Valasek, John; May, James Franklin; Beckett, Andrew; Rhodes, Jr., Cecil C., Un-manned aerial vehicle having adjustable wing module, tail, and landing gear.
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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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