GB560580A - Improvements in or relating to the construction of streamlined panel structures - Google Patents

Improvements in or relating to the construction of streamlined panel structures

Info

Publication number
GB560580A
GB560580A GB1605842A GB1605842A GB560580A GB 560580 A GB560580 A GB 560580A GB 1605842 A GB1605842 A GB 1605842A GB 1605842 A GB1605842 A GB 1605842A GB 560580 A GB560580 A GB 560580A
Authority
GB
United Kingdom
Prior art keywords
radius
basic element
lines
construction
angle
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
GB1605842A
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.)
LAURENCE RACHARD MORPHEW
Original Assignee
LAURENCE RACHARD MORPHEW
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 LAURENCE RACHARD MORPHEW filed Critical LAURENCE RACHARD MORPHEW
Priority to GB1605842A priority Critical patent/GB560580A/en
Publication of GB560580A publication Critical patent/GB560580A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Landscapes

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

Abstract

560,580. Aircraft framework. MORPHEW, L. R. Nov. 13, 1942, No. 16058. [Class 4] In a streamlined structure, such as a fuselage for an aircraft, having a skin carried by transverse frames one or a few basic elements of standard profile are used to make the transverse frames. The basic element shown in Fig. 1 comprises a circular part 11 of radius r integral with a circular part 12 of larger radius R, the part 11 subtending an angle of 180‹ and the part 12 an angle of 90‹. In Fig. 3 is shown an oval transverse frame made out of two similar parts each obtained by cutting a basic element at the line J, X indicating the lines of junction of the circular arcs constituting the basic elements. A geometrical construction for drawing the lines J is given in the Specification. In Fig. 8 is shown a channel-shaped basic element 31 with a flange 33 formed on a radius so as to adapt it to the skin 32 lying at various inclinations to the longitudinal axis of the structure.
GB1605842A 1942-11-13 1942-11-13 Improvements in or relating to the construction of streamlined panel structures Expired GB560580A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1605842A GB560580A (en) 1942-11-13 1942-11-13 Improvements in or relating to the construction of streamlined panel structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1605842A GB560580A (en) 1942-11-13 1942-11-13 Improvements in or relating to the construction of streamlined panel structures

Publications (1)

Publication Number Publication Date
GB560580A true GB560580A (en) 1944-04-11

Family

ID=10070388

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1605842A Expired GB560580A (en) 1942-11-13 1942-11-13 Improvements in or relating to the construction of streamlined panel structures

Country Status (1)

Country Link
GB (1) GB560580A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8757545B2 (en) 2010-09-16 2014-06-24 Airbus Operations Gmbh Segment of a fuselage of an aircraft
WO2021019487A1 (en) * 2019-08-01 2021-02-04 Research And Enginnering Company Llc (Nik) Fuselage of a lightweight transport aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8757545B2 (en) 2010-09-16 2014-06-24 Airbus Operations Gmbh Segment of a fuselage of an aircraft
DE102010045588B4 (en) * 2010-09-16 2017-04-06 Airbus Operations Gmbh Fuselage segment for an aircraft
WO2021019487A1 (en) * 2019-08-01 2021-02-04 Research And Enginnering Company Llc (Nik) Fuselage of a lightweight transport aircraft

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