초록 ▼

This invention provides a system for launching aircraft into free flight regime regardless of runway conditions, wherein a sled of the self-powered air cushion vehicle type is configured in plan form so as to accept in temporarily locked relation thereupon and in combination therewith an airplane in

This invention provides a system for launching aircraft into free flight regime regardless of runway conditions, wherein a sled of the self-powered air cushion vehicle type is configured in plan form so as to accept in temporarily locked relation thereupon and in combination therewith an airplane in such manner that a successful take-off run in mutually aerodynamically compatible regime may be accomplished in spite of surface problems with the runway. Upon attainment of airborne speed, under control of the pilot the aircraft lifts off the sled into full free flight; and thus is airborne albeit the runway is at the time unusable by conventional wheel-geared aircraft; for example, as the result of a previous bombing attack on the runway by enemy aircraft. The sled incorporates self-propelling and directional guidance means for retrieval/reuse purposes, as well as a take-off abort control system.

대표청구항 ▼

An air cushion vehicle sled for allowing an aircraft to take-off from a damaged runway, said sled comprising: a hull having a generally T-shaped configuration in plan view to present a relatively narrow forward portion and laterally projecting rearward portions; a forward air cushion cell carried by

An air cushion vehicle sled for allowing an aircraft to take-off from a damaged runway, said sled comprising: a hull having a generally T-shaped configuration in plan view to present a relatively narrow forward portion and laterally projecting rearward portions; a forward air cushion cell carried by said hull below said forward portion and having a diameter substantially corresponding to the width of said forward portion of said hull; a pair of substantially identical rearward air cushion cells carried by said hull below said rearward portions thereof, said rearward cells being disposed in closely spaced, side-by-side relation and each having a diameter substantially greater than the diameter of said forward cell and sufficient to extend to the outer end of said rearward portion of said hull, said forward and rearward cells being relatively disposed such that the three wheels of a tricycle landing gear aircraft are adapted to be substantially centered over the respective cells when said aircraft is supported on said hull; retaining means on said hull centered above each of said cells for releasably holding the three wheels of the tricycle landing gear aircraft; mutually aligned wheel guide track means disposed of said hull and aligned with each of said retaining means for accommodating the wheels of the aircraft when mounting the sled and guiding the wheels into positions over said air cushion cells and adjacent said each retaining means; means located at the forward end of said forward portion of the hull for delivering pressurized air into said cells and including rearwardly directed and divergent nozzles located to either side of that retaining means centered above said forward cell, each nozzle having independently operable closure means for constraining the pressurized air to be fed to said cells when the closure means is closed and for by-passing flow of air to said cells and allowing it to pass through the nozzle when the closure means is open for use in directional control of the travel of said sled following aricraft separation; drag chute means carried adjacent the rear end of said rearward portion of the hull and normally stowed in housings mounted thereon, said chutes being releasably actuated automatically upon separation of said aircraft from said sled for retarding further travels of said sled; and means adapted to be controlled by aircraft personnel for releasing said retaining means to permit said aircraft to fly away from said sled.