GB212006A - Improvements in metal wings or the like for aircraft - Google Patents

Improvements in metal wings or the like for aircraft

Info

Publication number
GB212006A
GB212006A GB34569/22A GB3456922A GB212006A GB 212006 A GB212006 A GB 212006A GB 34569/22 A GB34569/22 A GB 34569/22A GB 3456922 A GB3456922 A GB 3456922A GB 212006 A GB212006 A GB 212006A
Authority
GB
United Kingdom
Prior art keywords
spar
struts
rib
abutments
engage
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
GB34569/22A
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB34569/22A priority Critical patent/GB212006A/en
Publication of GB212006A publication Critical patent/GB212006A/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

212,006. Armstrong Siddeley Motors, Ltd., and Wylie, H. N. Dec. 19, 1922. Planes, construction of.-For connecting a rib to a spar in the framework of an aeroplane wing devices mounted on the rib are arranged to engage the spar solely by clamping action. Abutments 9, secured to or integral with struts 5 connecting the booms 1, 2 of the rib, engage the spar 3 by a clamping action at the junctions of the flange and web portions of the spar. The abutments 9 are preferably strips of spring steel folded as shown and' formed with tongues 13 engaging the sides of the struts, a single rivet serving to secure each abutment to the strut. Preferably one of the struts is adapted to be swung out about one end as shown to facilitate the assembling of the parts. Specification 144,828 is referred to.
GB34569/22A 1922-12-19 1922-12-19 Improvements in metal wings or the like for aircraft Expired GB212006A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB34569/22A GB212006A (en) 1922-12-19 1922-12-19 Improvements in metal wings or the like for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB34569/22A GB212006A (en) 1922-12-19 1922-12-19 Improvements in metal wings or the like for aircraft

Publications (1)

Publication Number Publication Date
GB212006A true GB212006A (en) 1924-03-06

Family

ID=10367251

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34569/22A Expired GB212006A (en) 1922-12-19 1922-12-19 Improvements in metal wings or the like for aircraft

Country Status (1)

Country Link
GB (1) GB212006A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4535958A (en) * 1982-12-13 1985-08-20 Hutchison Gary A Aluminum composite spar wing structure and method of assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4535958A (en) * 1982-12-13 1985-08-20 Hutchison Gary A Aluminum composite spar wing structure and method of assembly

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