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GB534810A - Stressed skin panels - Google Patents

Stressed skin panels

Info

Publication number
GB534810A
GB534810A GB789539A GB789539A GB534810A GB 534810 A GB534810 A GB 534810A GB 789539 A GB789539 A GB 789539A GB 789539 A GB789539 A GB 789539A GB 534810 A GB534810 A GB 534810A
Authority
GB
United Kingdom
Prior art keywords
stressed skin
skin panels
aircraft
constructional
panels
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
GB789539A
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.)
DAVID HENDERSON SANDILANDS
Original Assignee
DAVID HENDERSON SANDILANDS
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 DAVID HENDERSON SANDILANDS filed Critical DAVID HENDERSON SANDILANDS
Priority to GB789539A priority Critical patent/GB534810A/en
Publication of GB534810A publication Critical patent/GB534810A/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)
  • Body Structure For Vehicles (AREA)

Abstract

534,810. Constructional panels for aircraft &c. SANDILANDS, D. H. Feb. 26, 1940, No. 7895. Drawings to Specification. [Class 4] A constructional panel for the fuselages and wings of aircraft &c. is formed as an inner panel in one piece having spaced swages or corrugations forming a lattice pattern and secured to a stressed skin to stiffen and strengthen the latter.
GB789539A 1940-02-26 1940-02-26 Stressed skin panels Expired GB534810A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB789539A GB534810A (en) 1940-02-26 1940-02-26 Stressed skin panels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB789539A GB534810A (en) 1940-02-26 1940-02-26 Stressed skin panels

Publications (1)

Publication Number Publication Date
GB534810A true GB534810A (en) 1941-03-19

Family

ID=9841867

Family Applications (1)

Application Number Title Priority Date Filing Date
GB789539A Expired GB534810A (en) 1940-02-26 1940-02-26 Stressed skin panels

Country Status (1)

Country Link
GB (1) GB534810A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2224000A (en) * 1988-11-10 1990-04-25 Genrikh Vasilievich Novozhilov Fuselage or pressure vessel structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2224000A (en) * 1988-11-10 1990-04-25 Genrikh Vasilievich Novozhilov Fuselage or pressure vessel structure
GB2224000B (en) * 1988-11-10 1992-05-27 Genrikh Vasilievich Novozhilov Aircraft fuselage or other pressure vessel.

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