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Class 244/3.29 - Radially rotating


Subclass of Class 244 - Aeronautics and astronautics
Definition: Subject matter wherein the stabilizing surface rotates about
No. of applications: 6
Last issue date: 12/22/2011


Application No.Application TitleIssue Date
20110308418Projectile Having Deployable Fin
A supercavitating projectile is disclosed that has deployable fins. The fins are pivotally coupled to the body of the projectile. The fins have two primary states: stowed within a recess at the surface of the projectile and deployed to a radially-extended position relat...
12/22/2011
20100282895LOW COST DEPLOYMENT SYSTEM AND METHOD FOR AIRBORNE OBJECT
A deployment system is provided for utilization onboard an airborne object including a deployable element. In one embodiment, the deployment system includes a circumferential restraint and a release mechanism mounted to the airborne object. The circumferential restraint...
11/11/2010
20100276534CANARD-CENTRIC MISSILE SUPPORT
A canard includes a first section and a second section. The first section is configured for the coupling of radial forces to a fuselage of an air vehicle, and the first section is coupled to the second section via a hinge somewhere along the radial extent of the canard....
11/04/2010
20070152097Exhaust assembly for mass ejection drive system
The present invention discloses a system, device and method for providing an exhaust assembly adapted for use with a mass ejection drive system to produce rotational torque about the principle axis of the drive system. Representative features generally include a vane su...
07/05/2007
20070045466Foldable, lockable control surface and method of using same
A foldable, lockable control surface includes an inner control surface member and an outer control surface member hingedly attached along a hinge line to the inner control surface member. The control surface further includes a biasing assembly disposed on the hinge line...
03/01/2007
20060108469ARTICULATED FOLDING WING STRUCTURE AND METHOD
An articulated wing (20) is readily deployable from a stowed configuration that occupies minimal volume to an extended configuration for flight. The wing (20) includes a frame (24) having a pair of beams (30) spaced by one or more ribs (36...
05/25/2006
 
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