GB229345A - Improvements in or relating to aerial machines - Google Patents

Improvements in or relating to aerial machines

Info

Publication number
GB229345A
GB229345A GB4244/25A GB424425A GB229345A GB 229345 A GB229345 A GB 229345A GB 4244/25 A GB4244/25 A GB 4244/25A GB 424425 A GB424425 A GB 424425A GB 229345 A GB229345 A GB 229345A
Authority
GB
United Kingdom
Prior art keywords
bands
relating
wing
surface covering
aerial machines
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
GB4244/25A
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.)
ALFRED RENARD
Original Assignee
ALFRED RENARD
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 ALFRED RENARD filed Critical ALFRED RENARD
Publication of GB229345A publication Critical patent/GB229345A/en
Expired legal-status Critical Current

Links

Classifications

    • 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)
  • Insertion Pins And Rivets (AREA)

Abstract

229,345. Renard, A. Feb. 16, 1924, [Convention date]. Planes and the like, construction of.-In a metal wing the rib elements A, A' to the front and rear of, and between, the longitudinal spars L, L', are held together and reinforced by a metal band B which passes round the outside of the wing and also serves to cover the joints between the panels P forming the surface covering. The bands B are secured by rivets. The Specification as open to inspection under Sect. 91 (3) (a) states that a cement may be introduced between the bands B and the surface covering. This subject-matter does not appear in the Specification as accepted.
GB4244/25A 1924-02-16 1925-02-16 Improvements in or relating to aerial machines Expired GB229345A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE229345X 1924-02-16

Publications (1)

Publication Number Publication Date
GB229345A true GB229345A (en) 1925-07-02

Family

ID=3866229

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4244/25A Expired GB229345A (en) 1924-02-16 1925-02-16 Improvements in or relating to aerial machines

Country Status (1)

Country Link
GB (1) GB229345A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160167764A1 (en) * 2011-10-19 2016-06-16 The Boeing Company Wing airfoil stiffening for solar powered aircraft
CN106167088A (en) * 2015-05-22 2016-11-30 空中客车西班牙运营有限责任公司 Multiple wing beam type torsion box structure

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160167764A1 (en) * 2011-10-19 2016-06-16 The Boeing Company Wing airfoil stiffening for solar powered aircraft
US10640221B2 (en) * 2011-10-19 2020-05-05 The Boeing Company Wing airfoil stiffening for solar powered aircraft
CN106167088A (en) * 2015-05-22 2016-11-30 空中客车西班牙运营有限责任公司 Multiple wing beam type torsion box structure

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