George Mccoubrey resumes & CV records
Resumes
George A Mccoubrey Deceased3 Crawford Dr, Westfield, MA 01085
George Mccoubrey Phones & Addresses
Westfield, MA
106 Chester Rd, Blandford, MA 01008 413-8460153 413-8480153
Stanwood, WA
3 Crawford Dr, Westfield, MA 01085 413-8965783
Social networks
George A Mccoubrey
Linkedin
Work
Position:
Administrative Support Occupations, Including Clerical Occupations
Education
Degree:
High school graduate or higher
Mentions for George A Mccoubrey
Publications & IP owners
Us Patents
Compensating Structure For Circulation Control Rotor Pneumatic Valve
US Patent:
4242044, Dec 30, 1980
Filed:
Jul 11, 1979
Appl. No.:
6/056590
Inventors:
George A. McCoubrey - Westfield MA
Assignee:
The United States of America as represented by the Secretary of the Navy - Washington DC
International Classification:
B64C 2718
US Classification:
416 20A
Abstract:
Structure for minimizing gap changes in a circulation control pneumatic ve. A flat, flexible ring is located below and adjacent to the plane of the nozzle of blade ducts. The flat, flexible ring is supported from beneath by an array of actuators. In one embodiment, the nozzles are immobilized relative to hub-induced displacements and thus eliminate any feedback due to hub flexing. In another embodiment, the nozzle is pivotally attached to a rotating carrier and feedback is reversed so that feedback becomes negative.
Adjustable Blowing Slot For Circulation Control Airfoil
US Patent:
4137008, Jan 30, 1979
Filed:
Sep 21, 1977
Appl. No.:
5/835125
Inventors:
James B. Grant - Windsor CT
George A. McCoubrey - Westfield MA
George A. McCoubrey - Westfield MA
Assignee:
The United States of America as represented by the Secretary of the Navy - Washington DC
International Classification:
B64C 2108
US Classification:
416 20R
Abstract:
A circulation control airfoil having an edge slot formed by upper and lower uct panels. A plurality of struts are spaced along the length of the edge slot and are adjustably attached to the upper and lower duct to maintain the edge slot height. A reinforcing saddle is provided at each attachment position on the panels for distributing load applied to the struts over a large area of the duct panels. Each strut is provided with a differential lead thread system which provides high resolution adjustment capability for the edge slot.
Rotor Hub For A Helicopter
US Patent:
4189283, Feb 19, 1980
Filed:
Jul 12, 1978
Appl. No.:
5/924024
Inventors:
George A. McCoubrey - Westfield MA
Assignee:
The United States of America as represented by the Secretary of the Navy - Washington DC
International Classification:
B64C 2104
B64C 1106
B64C 1106
US Classification:
416 20A
Abstract:
A rotor hub for a helicopter having a hum member rotatably mounted to a rr mast stationarily attached to the fuselage of a helicopter and forming an air plenum for circulation control. A shaft, which is driven from a transmission, drives a torque plate which is attached to the top of the hub member. A flexible hub plate is attached to a flange on the hub member and has a plurality of axles to which the rotor blades are individually attached. Air from inside the plenum is piped to the rotor blades through flexible ducts. The flexible hub plate is designed to provide a high degree of stiffness in the plane of rotation and a lesser degree of stiffness in a plane normal to the plane of rotation.
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