GB157310A - Improvements in airplane ribs - Google Patents

Improvements in airplane ribs

Info

Publication number
GB157310A
GB157310A GB1222/21A GB122221A GB157310A GB 157310 A GB157310 A GB 157310A GB 1222/21 A GB1222/21 A GB 1222/21A GB 122221 A GB122221 A GB 122221A GB 157310 A GB157310 A GB 157310A
Authority
GB
United Kingdom
Prior art keywords
webs
bent
flanges
section
airplane
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
GB1222/21A
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
Publication of GB157310A publication Critical patent/GB157310A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs

Abstract

157,310. Rapp, J. W., (Assignee of Vanorio, J.). Feb. 27, 1919, [Convention date]. Framework; planes, construction of.-A modified form of the aeroplane rib described in Specification 122,649, is made from a sheet-metal blank which is cut away at 4<1> to form flanges 5 connected by webs 4, the flanges being bent to form channels 3, 3<1>, and the webs 4 being bent into V-formation in cross-section. The V-section is formed by embossing the webs in one direction beyond their original plane, and by bending the edges beyond this plane in the opposite direction.
GB1222/21A 1919-02-27 1921-01-10 Improvements in airplane ribs Expired GB157310A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US157310XA 1919-02-27 1919-02-27

Publications (1)

Publication Number Publication Date
GB157310A true GB157310A (en) 1922-06-08

Family

ID=21773253

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1222/21A Expired GB157310A (en) 1919-02-27 1921-01-10 Improvements in airplane ribs

Country Status (1)

Country Link
GB (1) GB157310A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7578473B2 (en) 2003-12-23 2009-08-25 Airbus Uk Limited Rib for aircraft wing and methods for the manufacture thereof
US9296466B2 (en) 2013-06-21 2016-03-29 The Boeing Company Symmetric wing rib with center plane fastened shear ties
CN110287524A (en) * 2019-05-17 2019-09-27 陕西飞机工业（集团）有限公司 A kind of aircraft joint part improved method and aircraft joint part

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7578473B2 (en) 2003-12-23 2009-08-25 Airbus Uk Limited Rib for aircraft wing and methods for the manufacture thereof
US8001690B2 (en) 2003-12-23 2011-08-23 Airbus Uk Limited Rib for aircraft wing and methods for the manufacture thereof
US9296466B2 (en) 2013-06-21 2016-03-29 The Boeing Company Symmetric wing rib with center plane fastened shear ties
CN110287524A (en) * 2019-05-17 2019-09-27 陕西飞机工业（集团）有限公司 A kind of aircraft joint part improved method and aircraft joint part

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