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
GB2564068A
Inventor
James Richard Bede
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Individual
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Individual
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Priority to GB2564068ApriorityCriticalpatent/GB1212445A/en
Publication of GB1212445ApublicationCriticalpatent/GB1212445A/en
B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Abstract
1,212,445. Aircraft wing structures. J. R. BEDE. 29 May, 1968, No. 25640/68. Heading B7W. An aircraft wing comprises a plurality of integral rib- and skin-forming sections 4 disposed longitudinally about a spar 2, the sections being joined adhesively with each other and with the spar. The sections may be moulded of glass fibres in a resinous base and may be additionally secured to each other by screws or rivets and to the spar by clamps. A secondary aileron supporting spar may be moulded into the sections 4 or inserted at trimmed-away trailing edges thereof.
GB2564068A1968-05-291968-05-29Improved airfoil construction
ExpiredGB1212445A
(en)
Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine airplane(Full scale wind tunnel investigation of static longitudinal and lateral stability and control characteristics of light single-engine low-wing monoplane)
Canada has a word for it- STOL(Canadian R and D on fixed wing civil STOL aircraft, discussing augmentor wing concept using jet powered lift augmentor system)
A parametric study of the subsonic characteristics of low-aspect-ratio reentry wings(Parametric study of subsonic characteristics of low-aspect-ratio delta wings, noting role of airfoil thickness and free vortices above wing surface)
The effect of wing twist distortion on glider static longitudinal stability with stick fixed(Wing twist distortion effect on glider static longitudinal stability with stick fixed)