GB199005A - Improvements in the construction of flying machines - Google Patents

Improvements in the construction of flying machines

Info

Publication number
GB199005A
GB199005A GB12899/23A GB1289923A GB199005A GB 199005 A GB199005 A GB 199005A GB 12899/23 A GB12899/23 A GB 12899/23A GB 1289923 A GB1289923 A GB 1289923A GB 199005 A GB199005 A GB 199005A
Authority
GB
United Kingdom
Prior art keywords
forward unit
planes
machine
shows
bars
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
GB12899/23A
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.)
NIEUPORT ASTRA SA
Original Assignee
NIEUPORT ASTRA SA
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 NIEUPORT ASTRA SA filed Critical NIEUPORT ASTRA SA
Publication of GB199005A publication Critical patent/GB199005A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Jib Cranes (AREA)

Abstract

199,005. Soc. Anon. Nieuport-Astra. June 10, 1922, [Convention date]. Aeroplanes; fuselages; planes, connecting to machine.-An aeroplane comprises a forward unit carrying the motor, pilot's cockpit, lifting- planes and landing chassis, and provided with a braced framework to which any desired body can be removably attached. Fig. 1 shows a forward unit connected to either of the alternative forms of body shown by means of bars 9, 10 secured on each side of the body and detachably connected to the forward unit at 11, 12. Transverse bars brace together the connections on the two sides of the machine. Fig. 5 shows the bracing of a forward unit modified to enable a direct connection to be made with the ends 11, 12 of the longerons of the body, which are braced together at these points by transverse bars. Specification 169,547 is referred to.
GB12899/23A 1922-06-10 1923-05-14 Improvements in the construction of flying machines Expired GB199005A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR199005X 1922-06-10

Publications (1)

Publication Number Publication Date
GB199005A true GB199005A (en) 1924-08-14

Family

ID=8879818

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12899/23A Expired GB199005A (en) 1922-06-10 1923-05-14 Improvements in the construction of flying machines

Country Status (1)

Country Link
GB (1) GB199005A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986001175A1 (en) * 1984-08-10 1986-02-27 Flight Concepts Limited Partnership Aircraft with interchangeable fuselage modules
RU2572507C1 (en) * 2014-07-02 2016-01-10 Публичное акционерное общество "Научно-производственная корпорация "Иркут" School aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986001175A1 (en) * 1984-08-10 1986-02-27 Flight Concepts Limited Partnership Aircraft with interchangeable fuselage modules
RU2572507C1 (en) * 2014-07-02 2016-01-10 Публичное акционерное общество "Научно-производственная корпорация "Иркут" School aircraft

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