WOLF ELBER
Pilots at Anne Burras Ln, Newport News, VA
License number
Virginia A0536424
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
213 Anne Burras Ln, Newport News, VA 23606
Professional information
Method Of Making A Partial Interlaminar Separation Composite System
US Patent:
4274901, Jun 23, 1981
Filed:
Feb 7, 1980
Appl. No.:
6/119337
Inventors:
Wolf Elber - Newport News VA
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
National Aeronautics and Space Administration - Washington DC
International Classification:
B32B 3120
US Classification:
156242
Abstract:
This invention relates to an interlaminar separation system for composites wherein a thin layer of a perforated foil film is interposed between adjacent laminae of a composite formed from prepreg tapes to thereby permit laminae adherence through the perforations and produce a composite structure having improved physical property characteristics.
Partial Interlaminar Separation System For Composites
US Patent:
4229473, Oct 21, 1980
Filed:
Mar 24, 1978
Appl. No.:
5/889671
Inventors:
Wolf Elber - Newport News VA
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
National Aeronautics and Space Administration - Washington DC
International Classification:
B32B 310, B32B 512, B32B 2712
US Classification:
428113
Abstract:
This invention relates to an interlaminar separation system for composites wherein a thin layer of a perforated foil film is interposed between adjacent laminae of a composite formed from prepreg tapes to thereby permit laminae adherence through the perforations and produce a composite structure having improved physical property characteristics.
Means For Controlling Aerodynamically Induced Twist
US Patent:
4330100, May 18, 1982
Filed:
Sep 28, 1979
Appl. No.:
6/079913
Inventors:
Wolf Elber - Newport News VA
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
National Aeronautics and Space Administration - Washington DC
International Classification:
B64C 352
US Classification:
244 48
Abstract:
A wing twist deformation control mechanism which provides active compensation for aerodynamically induced twist deformation of high aspect ratio wings. The twist deformation control mechanism consists of a torque tube, internal to each wing and rigidly attached near the tip of each wing, and moved by an actuator located in the aircraft fuselage. As changes in the aerodynamic loads on the wings occur the torque tube is rotated to compensate for the induced wing twist.