Lifting arrangement for lateral aircraft surfaces
OwnerManuel Munoz Saizinventor
Life of this patent
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Abstract
Lifting arrangement for lateral aircraft surfaces that consists of numerous lateral flutings, grooves, splines, flutes or riblets parallel to each other, arranged on the lateral surfaces of fuselages, fin units, pylons and gondolas of aircraft with a downward slope from the nose to the tail, with the flow of air passing through such flutings, grooves, etc., towards the rear and downwards, generating lifting by reaction, using small planes or fins to support the engines and flight control fins.
Claims16
A lifting arrangement for lateral aircraft surfaces comprising a plurality of lateral elements parallel to each other arranged on the lateral surfaces of an aircraft, wherein each said lateral element of said plurality of lateral elements has a substantially constant cross-section and wherein each said lateral element of said plurality of lateral elements has a downward slope from the nose to the tail and small wings or fins, with a flow of air passing through said plurality of lateral elements towards the rear and downwards, generating lift by reaction.
Dependencies are inferred from the claim text.