GB722857A - Improvements relating to the construction of hollow bodies of streamline form - Google Patents

Improvements relating to the construction of hollow bodies of streamline form

Info

Publication number
GB722857A
GB722857A GB2510452A GB2510452A GB722857A GB 722857 A GB722857 A GB 722857A GB 2510452 A GB2510452 A GB 2510452A GB 2510452 A GB2510452 A GB 2510452A GB 722857 A GB722857 A GB 722857A
Authority
GB
United Kingdom
Prior art keywords
longitudinally divided
stiffeners
stringers
construction
parent specification
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
GB2510452A
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 GB2510452A priority Critical patent/GB722857A/en
Publication of GB722857A publication Critical patent/GB722857A/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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

722,857. Aircraft framework. HEAL, L. C. March 20, 1951, No. 25104/52. Divided out of and Addition to 702,981, [Group XXII]. Class 4. [Also in Group XXII] An improvement in or modification of the invention claimed in the parent Specification comprises a longitudinally divided hollow structure constituted by separately-made longitudinally curved sections which are subsequently joined together, each of said sections being a hollow body constructed as claimed in the parent Specification. An aircraft fuselage comprises longitudinally divided halves 1, 1A wherein profiled skin strips are secured to one another and to internally disposed permanently attached stiffeners and stringers. In a further embodiment Fig. 2 (not shown), the structure of an engine nacelle comprises longitudinally divided halves, each having inner and outer skins of interconnected strip form having stiffeners and stringers located in the annular cavity between the skins on the opposed faces thereof.
GB2510452A 1951-03-20 1951-03-20 Improvements relating to the construction of hollow bodies of streamline form Expired GB722857A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2510452A GB722857A (en) 1951-03-20 1951-03-20 Improvements relating to the construction of hollow bodies of streamline form

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2510452A GB722857A (en) 1951-03-20 1951-03-20 Improvements relating to the construction of hollow bodies of streamline form

Publications (1)

Publication Number Publication Date
GB722857A true GB722857A (en) 1955-02-02

Family

ID=10222282

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2510452A Expired GB722857A (en) 1951-03-20 1951-03-20 Improvements relating to the construction of hollow bodies of streamline form

Country Status (1)

Country Link
GB (1) GB722857A (en)

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