GB472546A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB472546A
GB472546A GB875836A GB875836A GB472546A GB 472546 A GB472546 A GB 472546A GB 875836 A GB875836 A GB 875836A GB 875836 A GB875836 A GB 875836A GB 472546 A GB472546 A GB 472546A
Authority
GB
United Kingdom
Prior art keywords
component
aircraft
link
detachment
fuel
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.)
Expired
Application number
GB875836A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB875836A priority Critical patent/GB472546A/en
Publication of GB472546A publication Critical patent/GB472546A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D39/00—Refuelling during flight

Abstract

472,546. Composite aircraft. MAYO, R. H. March 24, 1936, No. 8758. [Class 4] In a composite aircraft comprising component aircraft 5, 7, mounted one on top of the other and secured together by releasable locking means a flexible link 8 is provided which continues to interconnect the components after detachment has taken place, link 8 consisting either of a pipe line through which fuel can be transferred after detachment from component 5 to component 7 or of a cable or the like by means of which a pipe line connection may be established between the two detached components. The fuel may be transferred by gravity in which case component 7 is arranged to fly below component 5 after separation or pumps may be installed in one or other component. One or other component also includes retracting means for link S. Specifications 400,292, 402,895, 402,951, and 402,997 are referred to.
GB875836A 1936-03-24 1936-03-24 Improvements in or relating to aircraft Expired GB472546A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB875836A GB472546A (en) 1936-03-24 1936-03-24 Improvements in or relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB875836A GB472546A (en) 1936-03-24 1936-03-24 Improvements in or relating to aircraft

Publications (1)

Publication Number Publication Date
GB472546A true GB472546A (en) 1937-09-24

Family

ID=9858707

Family Applications (1)

Application Number Title Priority Date Filing Date
GB875836A Expired GB472546A (en) 1936-03-24 1936-03-24 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB472546A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2373488A (en) * 2001-03-21 2002-09-25 Bae Systems Plc Launching, refuelling and recovering an aircraft
CN110040256A (en) * 2019-03-01 2019-07-23 清华大学 The vertical take-off and landing unmanned flying platform of combined type

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2373488A (en) * 2001-03-21 2002-09-25 Bae Systems Plc Launching, refuelling and recovering an aircraft
CN110040256A (en) * 2019-03-01 2019-07-23 清华大学 The vertical take-off and landing unmanned flying platform of combined type

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