KARL ROBERT KLINGEBIEL
Pilots at Country Clb Dr, Simi Valley, CA
License number
California A4242274
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
418 Country Club Dr APT C, Simi Valley, CA 93065
Professional information
Air Vehicle Flight Mechanism And Control Method
US Patent:
2012004, Mar 1, 2012
Filed:
Feb 9, 2011
Appl. No.:
13/023772
Inventors:
Matthew Todd Keennon - Simi Valley CA, US
Karl Robert Klingebiel - Simi Valley CA, US
Alexander Andryukov - Simi Valley CA, US
Bart Dean Hibbs - Simi Valley CA, US
Karl Robert Klingebiel - Simi Valley CA, US
Alexander Andryukov - Simi Valley CA, US
Bart Dean Hibbs - Simi Valley CA, US
International Classification:
B64C 33/02, B64C 33/00
US Classification:
244 22
Abstract:
Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
Air Vehicle Flight Mechanism And Control Method
US Patent:
8205823, Jun 26, 2012
Filed:
Jun 7, 2010
Appl. No.:
12/795539
Inventors:
Matthew Todd Keennon - Simi Valley CA, US
Karl Robert Klingebiel - Simi Valley CA, US
Alexander Andryukov - Simi Valley CA, US
Bart Dean Hibbs - Simi Valley CA, US
John Peter Zwaan - Simi Valley CA, US
Karl Robert Klingebiel - Simi Valley CA, US
Alexander Andryukov - Simi Valley CA, US
Bart Dean Hibbs - Simi Valley CA, US
John Peter Zwaan - Simi Valley CA, US
Assignee:
Aerovironment, Inc. - Monrovia CA
International Classification:
B64C 33/00
US Classification:
244 22, 244 11, 244 72
Abstract:
Heavier-than-air, aircraft having flapping wings, e. g. , ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
Aircraft Grounding System
US Patent:
8622343, Jan 7, 2014
Filed:
May 23, 2012
Appl. No.:
13/478560
Inventors:
Christopher E. Fisher - Simi Valley CA, US
John Peter Zwaan - Simi Valley CA, US
David R. Thompson - Simi Valley CA, US
Marc L. Schmalzel - Simi Valley CA, US
Karl R. Klingebiel - Simi Valley CA, US
Tyson R. Jensen - Simi Valley CA, US
Pavel Belik - Simi Valley CA, US
Eric James Aagaard - Simi Valley CA, US
John Peter Zwaan - Simi Valley CA, US
David R. Thompson - Simi Valley CA, US
Marc L. Schmalzel - Simi Valley CA, US
Karl R. Klingebiel - Simi Valley CA, US
Tyson R. Jensen - Simi Valley CA, US
Pavel Belik - Simi Valley CA, US
Eric James Aagaard - Simi Valley CA, US
International Classification:
B64F 1/00, B64F 1/12
US Classification:
244110R, 156 71, 156574
Abstract:
Liquid dispensing assemblies including adhesive anchoring assemblies configured to adhere to a support surface external to a device such as a vehicle. An air vehicle includes (a) a fluid adhesive container assembly detachably attached to the air vehicle, wherein the fluid adhesive container assembly comprises: (i) an adhesive container comprising fluid adhesive; and (ii) one or more fibers, wherein the one or more fibers are configured, or a brush of fibers, or a fabric of fibers, is configured to conduct the fluid adhesive and to structurally support an adhesive bond between the one or more fibers and a surface; and (b) means for dispensing the fluid adhesive from the fluid adhesive container, to the one or more fibers.
Air Vehicle Flight Mechanism And Control Method
US Patent:
2013016, Jul 4, 2013
Filed:
Jun 25, 2012
Appl. No.:
13/532699
Inventors:
Matthew Todd Keennon - Simi Valley CA, US
Karl Robert Klingebiel - Simi Valley CA, US
Alexander Andryukov - Simi Valley CA, US
Bart Dean Hibbs - Simi Valley CA, US
John Peter Zwaan - Simi Valley CA, US
Karl Robert Klingebiel - Simi Valley CA, US
Alexander Andryukov - Simi Valley CA, US
Bart Dean Hibbs - Simi Valley CA, US
John Peter Zwaan - Simi Valley CA, US
International Classification:
B64C 33/02
US Classification:
244 22, 244 39
Abstract:
Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.