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GB264923A - Improvements in methods of affixing panels and eyelets in fabric surfaces, particularly for use in aircraft construction - Google Patents

Improvements in methods of affixing panels and eyelets in fabric surfaces, particularly for use in aircraft construction

Info

Publication number
GB264923A
GB264923A GB2699325A GB2699325A GB264923A GB 264923 A GB264923 A GB 264923A GB 2699325 A GB2699325 A GB 2699325A GB 2699325 A GB2699325 A GB 2699325A GB 264923 A GB264923 A GB 264923A
Authority
GB
United Kingdom
Prior art keywords
eyelets
fabric
methods
fabric surfaces
aircraft construction
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
GB2699325A
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 RUPERT WOODS
Original Assignee
LAURENCE RUPERT WOODS
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 RUPERT WOODS filed Critical LAURENCE RUPERT WOODS
Priority to GB2699325A priority Critical patent/GB264923A/en
Publication of GB264923A publication Critical patent/GB264923A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

264,923. Woods, L. R. Oct. 28, 1925. Drawings to Specification. Combining sheet material. - Inspection panel frames and ventilation and drainage eyelets for aircraft and other fabric surfaces are made of a material such as cellulose acetate which becomes adhesive when applied to the surface in process of being doped. The fabric within the frame or eyelet is then cut away, and in the case of an inspection panel is covered by a fabric patch secured by doping. This patch may have fringed edges.
GB2699325A 1925-10-28 1925-10-28 Improvements in methods of affixing panels and eyelets in fabric surfaces, particularly for use in aircraft construction Expired GB264923A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2699325A GB264923A (en) 1925-10-28 1925-10-28 Improvements in methods of affixing panels and eyelets in fabric surfaces, particularly for use in aircraft construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2699325A GB264923A (en) 1925-10-28 1925-10-28 Improvements in methods of affixing panels and eyelets in fabric surfaces, particularly for use in aircraft construction

Publications (1)

Publication Number Publication Date
GB264923A true GB264923A (en) 1927-01-28

Family

ID=10252432

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2699325A Expired GB264923A (en) 1925-10-28 1925-10-28 Improvements in methods of affixing panels and eyelets in fabric surfaces, particularly for use in aircraft construction

Country Status (1)

Country Link
GB (1) GB264923A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11066002B2 (en) 2018-10-12 2021-07-20 Trinity Bay Equipment Holdings, LLC Installation trailer for coiled flexible pipe and method of utilizing same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11066002B2 (en) 2018-10-12 2021-07-20 Trinity Bay Equipment Holdings, LLC Installation trailer for coiled flexible pipe and method of utilizing same

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