GB167602A - Improvements in airplane supporting planes or wings - Google Patents

Improvements in airplane supporting planes or wings

Info

Publication number
GB167602A
GB167602A GB13537/20A GB1353720A GB167602A GB 167602 A GB167602 A GB 167602A GB 13537/20 A GB13537/20 A GB 13537/20A GB 1353720 A GB1353720 A GB 1353720A GB 167602 A GB167602 A GB 167602A
Authority
GB
United Kingdom
Prior art keywords
sheets
wings
planes
bars
supporting planes
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
GB13537/20A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB13537/20A priority Critical patent/GB167602A/en
Publication of GB167602A publication Critical patent/GB167602A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Abstract

167,602. Eggleston, T. L. May 17, 1920. Planes, arrangement and construction of; framework.-An aeroplane wing structure comprises inclined sheets 10 with interlocking bevelled tenons 11 locked together by bars 13, 14 of wood or metal and bolts 15. Additional sheets 20 with bevelled tenons may be secured by locking-bars 22, 23 between the junctions of the inclined sheets to form upper and lower planes. The sheets may be of fibre board with reinforcing metal strips 19, or may be fabric-covered frames. The structure may be reinforced by wire trusses 25 and stays 26.
GB13537/20A 1920-05-17 1920-05-17 Improvements in airplane supporting planes or wings Expired GB167602A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13537/20A GB167602A (en) 1920-05-17 1920-05-17 Improvements in airplane supporting planes or wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13537/20A GB167602A (en) 1920-05-17 1920-05-17 Improvements in airplane supporting planes or wings

Publications (1)

Publication Number Publication Date
GB167602A true GB167602A (en) 1921-08-17

Family

ID=10024761

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13537/20A Expired GB167602A (en) 1920-05-17 1920-05-17 Improvements in airplane supporting planes or wings

Country Status (1)

Country Link
GB (1) GB167602A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5637520A (en) * 1993-02-11 1997-06-10 Sgs-Thomson Microelectronics S.R.L. Process for fabricating integrated devices including flash-EEPROM memories and transistors
CN111395210A (en) * 2020-04-07 2020-07-10 浙江大学 Method for improving bearing capacity of truss girder bridge by using external prestressed tendons

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5637520A (en) * 1993-02-11 1997-06-10 Sgs-Thomson Microelectronics S.R.L. Process for fabricating integrated devices including flash-EEPROM memories and transistors
CN111395210A (en) * 2020-04-07 2020-07-10 浙江大学 Method for improving bearing capacity of truss girder bridge by using external prestressed tendons

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