GB261489A - Improvements in or relating to aeroplane-wings having metal frames - Google Patents

Improvements in or relating to aeroplane-wings having metal frames

Info

Publication number
GB261489A
GB261489A GB21743/25A GB2174325A GB261489A GB 261489 A GB261489 A GB 261489A GB 21743/25 A GB21743/25 A GB 21743/25A GB 2174325 A GB2174325 A GB 2174325A GB 261489 A GB261489 A GB 261489A
Authority
GB
United Kingdom
Prior art keywords
aeroplane
webs
wings
relating
metal frames
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
GB21743/25A
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 GB21743/25A priority Critical patent/GB261489A/en
Publication of GB261489A publication Critical patent/GB261489A/en
Expired legal-status Critical Current

Links

Classifications

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

Abstract

261,489. Mooney, D. J. Aug. 31, 1925. Planes, construction of; framework.-The ribs of an aeroplane are made in two parts secured respectively to the front and rear spars and joined together directly or to a third intermediate part at points other than at their connections to the spars. Fig. 1 shows a wing in which the leading and trailing portions of a rib are connected tc a central portion by overlapping joints. The edges of the overlapping webs of the ribs may be flanged, or flanges may be formed on the webs and the flanges secured together without having the webs overlapped.
GB21743/25A 1925-08-31 1925-08-31 Improvements in or relating to aeroplane-wings having metal frames Expired GB261489A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB21743/25A GB261489A (en) 1925-08-31 1925-08-31 Improvements in or relating to aeroplane-wings having metal frames

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21743/25A GB261489A (en) 1925-08-31 1925-08-31 Improvements in or relating to aeroplane-wings having metal frames

Publications (1)

Publication Number Publication Date
GB261489A true GB261489A (en) 1926-11-25

Family

ID=10168041

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21743/25A Expired GB261489A (en) 1925-08-31 1925-08-31 Improvements in or relating to aeroplane-wings having metal frames

Country Status (1)

Country Link
GB (1) GB261489A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2770072A (en) * 1952-02-27 1956-11-13 Nils F Testor Toy airplane construction
US4356616A (en) * 1980-02-25 1982-11-02 Rockwell International Corporation Method of making rib structures for an airfoil
US4481703A (en) * 1980-02-25 1984-11-13 Rockwell International Corporation Method of making rib structures for an airfoil

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2770072A (en) * 1952-02-27 1956-11-13 Nils F Testor Toy airplane construction
US4356616A (en) * 1980-02-25 1982-11-02 Rockwell International Corporation Method of making rib structures for an airfoil
US4481703A (en) * 1980-02-25 1984-11-13 Rockwell International Corporation Method of making rib structures for an airfoil

Similar Documents

Publication Publication Date Title
GB261489A (en) Improvements in or relating to aeroplane-wings having metal frames
GB733011A (en) Toy airplane construction
GB132153A (en) Improvements in Metal construction for Aeronautical Machines
GB151352A (en) Improvements in metal framework for aircraft
GB195235A (en) Improvements in or connected with the construction of wings and like parts of aeroplane flying machines and other aircraft
GB194516A (en) Improvements in or connected with the construction of wings and like parts of aeroplane flying machines and other aircraft
GB195916A (en) Improvements in ribs, cross members and the like for aircraft planes or wings
US2386522A (en) Airfoil construction
GB128770A (en) Improved Construction of Wings, Aerofoils and the like for Aeronautical Machines.
GB169623A (en) Improvements in jointing devices for connecting together the members of a framed structure
GB202761A (en) Improvements in or relating to spars for aircraft
GB200420A (en) Improvements in the construction of planes for aircraft
GB537445A (en) Improvements in or relating to the construction of metal skin covered wings for aircraft
GB242973A (en)
GB464249A (en) Improvements relating to metal aeroplane bodies
GB229389A (en) Improvements in metal construction for aeronautical machines
GB223670A (en) Improvements in or relating to metal spars and the like for aviation
GB241020A (en) Improvements in or relating to light metal structural members
GB188523A (en) Improvements in the construction of framework members of air craft, automobile, and other structures
GB167282A (en) Improvements in or relating to shovels and the like
GB122649A (en) Improvements in Airplane Ribs.
GB447520A (en) Improvements in or relating to spars for aircraft wings
GB220383A (en) Improvements in metal framework for aircraft
GB161063A (en) Improvements in metal construction of spars, longerons and the like for aircraft
GB155706A (en) Improvements in or relating to the wings of aeroplane flying machines