GB577705A - Improvements relating to re-inforced materials for aircraft and other structures - Google Patents

Improvements relating to re-inforced materials for aircraft and other structures

Info

Publication number
GB577705A
GB577705A GB3019138A GB3019138A GB577705A GB 577705 A GB577705 A GB 577705A GB 3019138 A GB3019138 A GB 3019138A GB 3019138 A GB3019138 A GB 3019138A GB 577705 A GB577705 A GB 577705A
Authority
GB
United Kingdom
Prior art keywords
skins
sheet
aircraft
skin
expanded
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
GB3019138A
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.)
ERNEST PLATTON KING
De Havilland Aircraft Co Ltd
Original Assignee
ERNEST PLATTON KING
De Havilland Aircraft Co 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 ERNEST PLATTON KING, De Havilland Aircraft Co Ltd filed Critical ERNEST PLATTON KING
Priority to GB3019138A priority Critical patent/GB577705A/en
Publication of GB577705A publication Critical patent/GB577705A/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)
  • Laminated Bodies (AREA)

Abstract

577,705. Compound sheet materials. DE HAVILLAND AIRCRAFT CO., Ltd., and KING, E. P. Oct. 18, 1938, No. 30191. [Class 140] [Also in Group XXXIII] Aircraft structures are formed with skins which resist tensile stresses and backings of relatively-light, mouldable, rigidly-setting material which give resistance to buckling or bending. The skins may be formed of wood veneer, which may be saturated with synthetic resin, reinforced fabric or sheet metal; and the backing may be expanded vulcanized rubber or synthtic resin. Reinforcements of metal or other sheets may be inserted in or formed on the backing. A ply-wood sheet 9, Fig. 3 may be reinforced by a corrugated metal sheet 10 and expanded rubber formed and vulcanized in the corrugations. The corrugated sheet may be between two outer skins, the whole spaces being filled with expanded rubber. The skins 16, 17, Fig. 5A may be separated by spacing ribs 18 which may be perforated. An aircraft wing is formed by attaching an inner plywood skin 25 to spars 23, 24, locating strips 26 of wood edge on to the skin, forming and vulcanizing expanded rubber in the spaces between the strips, and securing an outer skin 28 by a thermosetting glue. Reference has been directed by the Comptroller to Specifications 240,207, 252,257, [both in Class 140], 355,774, [Group XXXIII], 359,784, 434,191, 490,461 and 501,049.
GB3019138A 1938-10-18 1938-10-18 Improvements relating to re-inforced materials for aircraft and other structures Expired GB577705A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3019138A GB577705A (en) 1938-10-18 1938-10-18 Improvements relating to re-inforced materials for aircraft and other structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3019138A GB577705A (en) 1938-10-18 1938-10-18 Improvements relating to re-inforced materials for aircraft and other structures

Publications (1)

Publication Number Publication Date
GB577705A true GB577705A (en) 1946-05-29

Family

ID=10303721

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3019138A Expired GB577705A (en) 1938-10-18 1938-10-18 Improvements relating to re-inforced materials for aircraft and other structures

Country Status (1)

Country Link
GB (1) GB577705A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2700632A (en) * 1949-09-09 1955-01-25 Northrop Aircraft Inc Method of making a honeycomb sandwich
US2704587A (en) * 1955-03-22 Short radii bends in honeycomb
US2744042A (en) * 1951-06-21 1956-05-01 Goodyear Tire & Rubber Laminated panels
US2836267A (en) * 1955-07-26 1958-05-27 Boeing Co Lightweight structural body and process of fabricating the same
US2910396A (en) * 1952-11-12 1959-10-27 Bettinger Corp Structural reticulated webs or honeycombs and curtain wall panels made from same
US2973295A (en) * 1957-05-08 1961-02-28 Crown Zellerbach Corp Process of incorporating foamable materials in corrugated paperboard and the article derived therefrom
US3043730A (en) * 1957-09-03 1962-07-10 Dow Chemical Co Foamed construction element
US3099518A (en) * 1957-05-28 1963-07-30 Englander Co Inc Method of making an innerspring foam mattress
US3170828A (en) * 1959-09-25 1965-02-23 Robert L Irvine Method of making a storage vessel with a distended hemispherical roof
US4232093A (en) * 1973-10-29 1980-11-04 Summa Corporation High temperature skin construction
FR2653090A1 (en) * 1989-10-17 1991-04-19 Mitsubishi Heavy Ind Ltd Interior doubling plate for a fuselage wall

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2704587A (en) * 1955-03-22 Short radii bends in honeycomb
US2700632A (en) * 1949-09-09 1955-01-25 Northrop Aircraft Inc Method of making a honeycomb sandwich
US2744042A (en) * 1951-06-21 1956-05-01 Goodyear Tire & Rubber Laminated panels
US2910396A (en) * 1952-11-12 1959-10-27 Bettinger Corp Structural reticulated webs or honeycombs and curtain wall panels made from same
US2836267A (en) * 1955-07-26 1958-05-27 Boeing Co Lightweight structural body and process of fabricating the same
US2973295A (en) * 1957-05-08 1961-02-28 Crown Zellerbach Corp Process of incorporating foamable materials in corrugated paperboard and the article derived therefrom
US3099518A (en) * 1957-05-28 1963-07-30 Englander Co Inc Method of making an innerspring foam mattress
US3043730A (en) * 1957-09-03 1962-07-10 Dow Chemical Co Foamed construction element
US3170828A (en) * 1959-09-25 1965-02-23 Robert L Irvine Method of making a storage vessel with a distended hemispherical roof
US4232093A (en) * 1973-10-29 1980-11-04 Summa Corporation High temperature skin construction
FR2653090A1 (en) * 1989-10-17 1991-04-19 Mitsubishi Heavy Ind Ltd Interior doubling plate for a fuselage wall
US5165627A (en) * 1989-10-17 1992-11-24 Mitsubishi Jukogyo Kabushiki Kaisha Fuselage wall inner lining plate

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