Lyndon Cox resumes & CV records
Resumes
Lyndon Cox
Lyndon Cox
Lyndon Sheridan Cox DeceasedChapel Hill, NC
Lyndon Cox Phones & Addresses
Chapel Hill, NC
Durham, NC
Schenectady, NY
Silver Spring, MD
Mentions for Lyndon Sheridan Cox
Publications & IP owners
Us Patents
Safing And Arming Signature For Fuzes
US Patent:
4275658, Jun 30, 1981
Filed:
Oct 12, 1979
Appl. No.:
6/084047
Inventors:
Richard N. Gottron - Rockville MD
Lyndon S. Cox - Silver Spring MD
Lyndon S. Cox - Silver Spring MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
F42C 1102
US Classification:
102210
Abstract:
A recess or cavity is formed on the exterior of a fuze ogive. A piezo-eleic tape is positioned within the cavity or recess. Fluctuations in the pressure within the recess, caused by air flow over the exterior of the fuze, will cause the piezo-electric tape to produce an electrical signal or current.
Control System For Pre-Inflation Of Pilot's G-Suit
US Patent:
3956772, May 18, 1976
Filed:
Jul 11, 1975
Appl. No.:
5/595210
Inventors:
Lyndon S. Cox - Silver Spring MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
B64D 2502
US Classification:
2 21A
Abstract:
In an electronic version of the present invention, the potentiometer is cected to an aircraft control stick for sensing the position thereof. The output is coupled to logic circuits that detect the position of the control stick, associated with a severe maneuver about the pitch axis. Such detection actuates a valve for preinflation of a G-suit. Additional logic circuits are provided for detecting when the rate of control stick movement exceeds a preselected threshold. This, also corresponds with a severe maneuver about the pitch axis of the aircraft and also serves to actuate the G-suit valve. Analogous fluidic components may be utilized to effectuate equivalent operation of the G-suit.
Null Adjustable Vortex Rate Sensor
US Patent:
3960022, Jun 1, 1976
Filed:
May 9, 1973
Appl. No.:
5/358421
Inventors:
Arthur J. Ostdiek - Wheaton MD
Lyndon S. Cox - Silver Spring MD
Lyndon S. Cox - Silver Spring MD
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
G01P 900
US Classification:
73505
Abstract:
A null adjustable vortex rate sensor which enables the precise control and elocation of the stagnation point of the fluid stream with respect to the null line of the pickoff located within said chamber. The null adjustable vortex rate sensor is a vortex rate sensor with a fixed position pickoff and a fixed position drain, a rod being concentrically located in the drain and extended from the drain into the chamber. The horizontal adjustability of this rod inside the drain controls the location of the stagnation point at the pickoff within the chamber very precisely thus enabling one to approximately choose the location of the pickoff member and by means of the rod mechanism located in the drain move and adjust the stagnation point to obtain a null output at the fixed position of the pickoff. The pickoff provides a differential pressure signal which is a function of the angular rate of rotation of the chamber in inertial space.
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