GB357162A - Improvements in or relating to aircraft wings - Google Patents

Improvements in or relating to aircraft wings

Info

Publication number
GB357162A
GB357162A GB18304/30A GB1830430A GB357162A GB 357162 A GB357162 A GB 357162A GB 18304/30 A GB18304/30 A GB 18304/30A GB 1830430 A GB1830430 A GB 1830430A GB 357162 A GB357162 A GB 357162A
Authority
GB
United Kingdom
Prior art keywords
wing
tip
fuselage
navarro
swept
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
GB18304/30A
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 GB18304/30A priority Critical patent/GB357162A/en
Publication of GB357162A publication Critical patent/GB357162A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

357,162. Aircraft wings. NAVARRO, J. G. and NAVARRO, M. A., 21, Berrylands Road, Surbiton, Surrey. June 14, 1930, No. 18304. [Class 4.] An aeroplane wing having an inswept trailing edge c<1> at the root in combination with a swept-back rear edge at the outer portion of the wing is constructed with a swept-back spar 10. The wing is transversely horizontal. The spar 10 is pivoted to the fuselage at 11 to enable the wing and its bracing 13, 14 to be folded parallel to the fuselage after a flap c has been folded over the top of the wing. The bracing 13, 14 is pivoted to the fuselage at a point vertically beneath the point 11. The main part of the wing a is connected by a releasable bolt h to a fixed stub-wing e. The gap shown between the flap c and a wing tip g is occupied by an aileron. The tip g is upwardly inclined or the inner portion of the tip may be inclined downwards and the rest of the tip upwards. Specification 295,114, [Class 4, Aeronautics], is referred to.
GB18304/30A 1930-06-14 1930-06-14 Improvements in or relating to aircraft wings Expired GB357162A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18304/30A GB357162A (en) 1930-06-14 1930-06-14 Improvements in or relating to aircraft wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18304/30A GB357162A (en) 1930-06-14 1930-06-14 Improvements in or relating to aircraft wings

Publications (1)

Publication Number Publication Date
GB357162A true GB357162A (en) 1931-09-14

Family

ID=10110179

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18304/30A Expired GB357162A (en) 1930-06-14 1930-06-14 Improvements in or relating to aircraft wings

Country Status (1)

Country Link
GB (1) GB357162A (en)

Similar Documents

Publication Publication Date Title
GB192568A (en) Improvements in the wings and other aerofoils for aircraft
GB357162A (en) Improvements in or relating to aircraft wings
GB732657A (en) Improvements to rotary wing aircraft
GB437447A (en) Improvements in aeroplanes
GB460636A (en) Aeroplane stabilising means
GB346244A (en) Improvements in or relating to collapsible or folding aeroplane wings
GB350047A (en) Improvements in aeroplanes
GB357247A (en) Improvements in or relating to aeroplanes and like aircraft
GB556478A (en) Improvements in or relating to aircraft wings
GB359892A (en) Improvements in or relating to wings for aeroplanes and like aircraft
GB372344A (en) Improvements in or relating to aeroplane wings
GB450729A (en) Improved structure of wings or other parts of aircraft
US2014366A (en) Airplane
GB514145A (en) Improvements in and connected with aircraft
US1766376A (en) Method for attaching on fuselages wings having single spars
GB259995A (en) Improvements in and relating to aircraft wings
GB472642A (en) Improvements in or relating to aeroplanes convertible from monoplanes to biplanes, or vice versa
GB360951A (en) Improvements in engine mountings for aircraft
GB467357A (en) Improvements in or relating to aeroplane wings and propellers
GB366345A (en) Improvements in and connected with aeroplanes
GB193880A (en) Improvements in aircraft
GB454388A (en) Improvements relating to aeroplanes
GB450676A (en) Improvements in and relating to aeroplanes
GB335603A (en) Improvements in or connected with wing and aileron construction for aircraft
Butler et al. Low-speed tunnel tests of an aspect-ratio 9 jet-flap model, with ground simulation by moving-belt rig