An improved ram air canopy is disclosed having a top skin formed of a plurality of substantially rectangular top skin pieces. Each top skin piece has areas of reduced width at predetermined locations. The areas of reduced width result in a specific tension pattern of the top skin so as to reduce distortion. The increased tension pattern of the top skin better maintains the modeled desired airfoil shape of the canopy.

 
Web www.patentalert.com

< Derivative aircraft and methods for their manufacture

< High altitude platform control system

> Non-jamming, fail safe flight control system with non-symmetric load alleviation capability

> Device for the recognition of residual synchronization errors of multiple slats of flaps placed next to each other in aircraft

~ 00200