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특허 상세정보

Systems and methods for air vehicles

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-039/00    B64D-039/04    B64D-039/06   
출원번호 US-0467602 (2012-05-09)
등록번호 US-9150311 (2015-10-06)
우선권정보 IL-217364 (2012-01-04); IL-217365 (2012-01-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Oliff PLC
인용정보 피인용 횟수 : 3  인용 특허 : 64
초록

A refueling device for use in in-flight refueling operation between a tanker aircraft and a receiver aircraft includes a selectively steerable body and a controller. The selectively steerable body configured for being towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and includes a boom member having a boom axis and configured to enable fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during the in-flight refueling operation. The controller is configured for selectively steering the body t...

대표
청구항

1. A refueling device for use in in-flight refueling operation, comprising: (a) a body having a longitudinal axis and configured for being towed by a tanker aircraft via a fuel hose at least during in-flight refueling operation, and comprising a boom member having a boom axis and configured to enable fuel to be transferred from said fuel hose to a receiver aircraft along said boom axis during said in-flight refueling operation;(b) spatial control system configured for selectively ensuring maintaining a desired non-zero angular disposition between said bo...

이 특허에 인용된 특허 (64)

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