GB626382A - A device for closing small holes in metal sheets such as in the surface of an aircraft fuselage or control member - Google Patents

A device for closing small holes in metal sheets such as in the surface of an aircraft fuselage or control member

Info

Publication number
GB626382A
GB626382A GB485747A GB485747A GB626382A GB 626382 A GB626382 A GB 626382A GB 485747 A GB485747 A GB 485747A GB 485747 A GB485747 A GB 485747A GB 626382 A GB626382 A GB 626382A
Authority
GB
United Kingdom
Prior art keywords
hole
control member
small holes
metal sheets
aircraft fuselage
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
GB485747A
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.)
Blackburn Aircraft Ltd
Original Assignee
Blackburn Aircraft Ltd
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 Blackburn Aircraft Ltd filed Critical Blackburn Aircraft Ltd
Priority to GB485747A priority Critical patent/GB626382A/en
Publication of GB626382A publication Critical patent/GB626382A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/06—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips
    • F16B5/0607—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other
    • F16B5/0621—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other in parallel relationship
    • F16B5/0642—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other in parallel relationship the plates being arranged one on top of the other and in full close contact with each other
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

626,382. Covers for bolt holes. BLACKBURN AIRCRAFT, Ltd., and THIRSK, W. H. Feb. 19, 1947, No. 4857. [Class 89 (i)] [Also in Groups X and XVII] A device for closing holes such as access holes in the outer skin of an aeroplane comprises a disc &c. 1 of size and thickness to fill the hole united as by rivets to an elongated backing piece 3 having one dimension small enough to enable the device to be passed through the hole when tilted. The rivets also attach a smaller plate 5 for securing a compression spring 6 that abuts a nut 7 or other internal fitting. If the hole be of elongated form more than one spring or a leaf spring may be fitted.
GB485747A 1947-02-19 1947-02-19 A device for closing small holes in metal sheets such as in the surface of an aircraft fuselage or control member Expired GB626382A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB485747A GB626382A (en) 1947-02-19 1947-02-19 A device for closing small holes in metal sheets such as in the surface of an aircraft fuselage or control member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB485747A GB626382A (en) 1947-02-19 1947-02-19 A device for closing small holes in metal sheets such as in the surface of an aircraft fuselage or control member

Publications (1)

Publication Number Publication Date
GB626382A true GB626382A (en) 1949-07-14

Family

ID=9785112

Family Applications (1)

Application Number Title Priority Date Filing Date
GB485747A Expired GB626382A (en) 1947-02-19 1947-02-19 A device for closing small holes in metal sheets such as in the surface of an aircraft fuselage or control member

Country Status (1)

Country Link
GB (1) GB626382A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2143555A (en) * 1983-07-16 1985-02-13 Firsteel Metal Prod Access panel
CN113335556A (en) * 2021-05-25 2021-09-03 中国航空工业集团公司沈阳飞机设计研究所 Skin repairing method and repairing structure thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2143555A (en) * 1983-07-16 1985-02-13 Firsteel Metal Prod Access panel
CN113335556A (en) * 2021-05-25 2021-09-03 中国航空工业集团公司沈阳飞机设计研究所 Skin repairing method and repairing structure thereof

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