Rotationally mounted flexible band wing

Details Rotationally mounted flexible band wing Rotationally mounted flexible band wing

B - Operations, Transporting

64

C

B64C 3/38 (2006.01) B64C 3/56 (2006.01) F42B 15/10 (2006.01)

Patent

CA 2121740

ROTATIONALLY MOUNTED FLEXIBLE BAND WING ABSTRACT OF THE DISCLOSURE A vehicle such as a missile (20) includes an aerodynamically shaped missile body (22) having a longitudinal centerline, a set of control surfaces (26) joined to the missile body (22), and, preferably, a propulsion system (28) operable to drive the missile body (22) forwardly. A cylindrical rotational bearing (32) is mounted on the missile body (22) with its cylindrical axis parallel to the longitudinal centerline (24) of the missile body. A flexible band wing (38) is supported from the rotational bearing (32). The flexible band wing (38) may rotate about the centerline (24) of the missile body (22) responsive to aerodynamic forces exerted on the missile body (22) and the flexible band wing (38) to aid in making maneuvers without requiring the missile (20) to bank to align the flexible band wing (38) with the direction of the maneuver.

Affiliated with

Also associated with

Rating

Rotationally mounted flexible band wing does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rotationally mounted flexible band wing, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotationally mounted flexible band wing will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1342062