KENNETH KINNAN, MD
Anesthesiologist Assistant at Ross Ave, El Centro, CA

License number
California A22729
Category
Osteopathic Medicine
Type
Anesthesiology
Address
Address 2
1415 Ross Ave, El Centro, CA 92243
PO Box 969096, San Diego, CA 92196
Phone
(760) 339-7100
(760) 339-7389 (Fax)
(858) 495-0971

Organization information

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Kenneth Kinnan MD

1415 Ross Ave, El Centro, CA 92243

Industry:
Anesthesiology
Phone:
(760) 339-7100 (Phone)
Kenneth Warren Kinnan

Professional information

Kenneth Warren Kinnan Photo 1

Kenneth Warren Kinnan, El Centro CA

Specialties:
Anesthesiology
Work:
El Centro Regional Medical Center
1415 Ross Ave, El Centro, CA 92243
Education:
McGill University Faculty Of Medicine (1965)


Kenneth Kinnan Photo 2

Dr. Kenneth Kinnan, El Centro CA - MD (Doctor of Medicine)

Specialties:
Anesthesiology, Other
Address:
1415 Ross Ave, El Centro 92243
(760) 339-7100 (Phone), (760) 339-7389 (Fax)
Languages:
English
Hospitals:
1415 Ross Ave, El Centro 92243
El Centro Regional Medical Center
1415 Ross Ave, El Centro 92243
Education:
Medical School
McGill University / Faculty of Medicine


Kenneth Kinnan Photo 3

Kenneth Kinnan, El Centro CA

Specialties:
Anesthesiologist
Address:
1415 Ross Ave, El Centro, CA 92243


Kenneth Kinnan Photo 4

Lift Augmentation System For Aircraft

US Patent:
5244167, Sep 14, 1993
Filed:
Aug 20, 1991
Appl. No.:
7/747515
Inventors:
John Turk - San Diego CA
Kenneth W. Kinnan - San Diego CA
Charles Kamanski - Coronado CA
International Classification:
B64C 2900
US Classification:
244 121
Abstract:
A lift augmentation system for aircraft which comprises a plurality of propellers parallel to an aircraft wing and inset parallel to and at the trailing edge of the wing. The propellers function to both directly produce vertical lift in the manner of helicopter blades and to augment air circulation over the wing to enhance lift produced by the wing. The propellers are set into the trailing edge of the wing along the length of the wing, with the inboard propellers preferably closely spaced to the fuselage to force air flow over the reducing taper of the fuselage. Each propeller is tiltable in all directions about a vertical axis through the propeller hub and the assembly of engine and propeller is hinged to the wing for pivoting in a plane substantially parallel to the aircraft axis.