DANIEL JAMES TRACY
Pilots in Maple Valley, WA

License number
Washington A4364909
Issued Date
Sep 2015
Expiration Date
Sep 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
PO Box 244, Maple Valley, WA 98038

Professional information

Daniel Tracy Photo 1

Variable Wide Angle Conical Scanning Antenna

US Patent:
4862185, Aug 29, 1989
Filed:
Apr 5, 1988
Appl. No.:
7/177966
Inventors:
George S. Andrews - Kent WA
Bernard J. Lamberty - Kent WA
Daniel J. Tracy - Maple Valley WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
H01Q 320
US Classification:
343761
Abstract:
Disclosed is a variable angle conical scanning antenna that employs an offset paraboloidal reflector which is rotated about an axis that extends through the focus of the paraboloid of revolution that defines the reflector. Electromagnetic energy is supplied to the reflector by an antenna feed that is mounted at the focus of the paraboloid of revolution and directed along the axis of rotation. In this arrangement the electromagnetic energy that is reflected from the offset paraboloidal reflector forms an angle between the axis of rotation and the beam of reflected electromagnetic energy that is equal to the angle between the axis of rotation and the focal axis of the paraboloid of revolution that defines the reflector. Thus, conical scanning at a cone angle that is equal to twice the angle between the axis of rotation and the reflected beam of electromagnetic energy is achieved as the offset paraboloidal reflector is rotated. Variable angle scanning (i. e.


Daniel Tracy Photo 2

Remotely Piloted Vehicle

US Patent:
4194708, Mar 25, 1980
Filed:
Sep 21, 1978
Appl. No.:
5/944441
Inventors:
Daniel J. Tracy - Maple Valley WA
John P. Palmer - Seattle WA
Daniel J. O'Brien - Kirkland WA
Assignee:
The United States of America as represented by the Secretray of the Air
Force - Washington DC
International Classification:
B64C 1502, B64D 106
US Classification:
244 15
Abstract:
A recoverable remotely piloted vehicle (RPV) having: a deflectable canard/elevator placed very close to the nose tip; a constant (cross) section fuselage; wings mounted low and well aft on the fuselage; elevons; a centrally positioned weapons/payload bay, with doors, located internal of the upper portion of the fuselage; and, inflatable landing skids. The weapon/payload is dropped from the RVP, while the RVP is in flight in an inverted position.