GB212993A - Improvements in the construction of supporting planes for flying machines - Google Patents

Improvements in the construction of supporting planes for flying machines

Info

Publication number
GB212993A
GB212993A GB34838/22A GB3483822A GB212993A GB 212993 A GB212993 A GB 212993A GB 34838/22 A GB34838/22 A GB 34838/22A GB 3483822 A GB3483822 A GB 3483822A GB 212993 A GB212993 A GB 212993A
Authority
GB
United Kingdom
Prior art keywords
wing
girder
construction
central part
tips
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
GB34838/22A
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.)
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 GB34838/22A priority Critical patent/GB212993A/en
Publication of GB212993A publication Critical patent/GB212993A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/28Leading or trailing edges attached to primary structures, e.g. forming fixed slots

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

212,993. Invernairn, (W. Beardmore), Lord, and Chorlton, A. E. L. Dec. 21. 1922. Planes, construction of.-In a wing built up in three parts with the central part constituted by a box girder, the stressed upper and lower metal surfaces of the girder are laminated, the number of superposed metal plates being decreased towards the wing tips as shown A, A<1>, A<2> and B, B<1> B<2>. The depth of the flanges D, E may also decrease towards the tips. The joints in the superposed layers may be arranged out of line as shown in Fig. 5. The innermost plates may be stiffened on the inner side by light metal trays. The front and rear former parts L, M of the wing may be hinged to the central part at their lower edges and be formed with open frames sufficiently elastic to be accommodated t'o the girder and fixed thereto at the upper edges by bolts passing through extensions N.
GB34838/22A 1922-12-21 1922-12-21 Improvements in the construction of supporting planes for flying machines Expired GB212993A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB34838/22A GB212993A (en) 1922-12-21 1922-12-21 Improvements in the construction of supporting planes for flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB34838/22A GB212993A (en) 1922-12-21 1922-12-21 Improvements in the construction of supporting planes for flying machines

Publications (1)

Publication Number Publication Date
GB212993A true GB212993A (en) 1924-03-21

Family

ID=10370517

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34838/22A Expired GB212993A (en) 1922-12-21 1922-12-21 Improvements in the construction of supporting planes for flying machines

Country Status (1)

Country Link
GB (1) GB212993A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3093219A (en) * 1961-04-06 1963-06-11 Monte Copter Inc Plural-section airfoils
US4749155A (en) * 1985-09-30 1988-06-07 The Boeing Company Method of making wing box cover panel
EP3421355A1 (en) * 2017-06-29 2019-01-02 Airbus Operations GmbH Aerofoil structure and method of assembly
CN111605716A (en) * 2019-02-22 2020-09-01 空中客车运营简化股份公司 Main structure of aircraft hanging rack and aircraft

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3093219A (en) * 1961-04-06 1963-06-11 Monte Copter Inc Plural-section airfoils
US4749155A (en) * 1985-09-30 1988-06-07 The Boeing Company Method of making wing box cover panel
EP3421355A1 (en) * 2017-06-29 2019-01-02 Airbus Operations GmbH Aerofoil structure and method of assembly
CN111605716A (en) * 2019-02-22 2020-09-01 空中客车运营简化股份公司 Main structure of aircraft hanging rack and aircraft
CN111605716B (en) * 2019-02-22 2024-02-20 空中客车运营简化股份公司 Main structure of aircraft hanging frame and aircraft

Similar Documents

Publication Publication Date Title
GB212993A (en) Improvements in the construction of supporting planes for flying machines
GB391809A (en) Improvements in or relating to knitting mechanisms
GB128131A (en) Improvements in Metal Construction for Aircraft.
GB191882A (en) Improvements in or relating to folding tables
GB130825A (en) Improvements in or relating to the Spars of Aeroplane Wings.
SU29507A1 (en) The way to strengthen the speaker cone
FR1160013A (en) Multiple articulated element rail vehicle with desmodromic transverse linkage coupled axles
SU34976A1 (en) Fairing for aircraft wheels
GB224298A (en) Improvements in metal girders of light construction for aircraft and the like
GB226191A (en) Staying floats on aircraft
FR747080A (en) Arrangement of machine guns in the wings of an airplane
GB405935A (en) Improvements in and relating to seamless containers moulded from fibre pulp
AU2878030A (en) Improvements in or connected with frame structures particularly suitable in aircraft construction
GR16618B (en) NEW ENGINE CONNECTION SYSTEM AFTER THE FRAMEWORK IN CARS MOVED BY FRONT DIFFERENTIAL.
AU580632A (en) Improvements relating to machines for grading eggs and the like
FI18106A (en) The centrifugal mills are equipped with and suitable for the project as a whole.
GB205049A (en)
ES105403A1 (en) A perfecting in the medias.
GB186039A (en) Improvements in sustaining and steering surfaces for aerial vessels
CA358051A (en) Endless track link
FR731824A (en) Means for reinforcing spars used in light construction, for example in aviation
GB156858A (en) An improved means for folding the planes of aircraft
CA324653A (en) Model aeroplane
ES121731A1 (en) Improvements in the acoustic horns.
FI17968A (en) Underlined with three axles for the first time