George T Drakeley Deceased1401 Ellendale Ave, Dallas, OR 97338
George Drakeley Phones & Addresses
1401 Ellendale Ave, Dallas, OR 97338 503-6233671 503-6235660 503-6237061
Bellevue, WA
Oak Harbor, WA
Mentions for George T Drakeley
Publications & IP owners
Us Patents
Fuselage Tail Jet Engine Thrust Reverser And Method
US Patent:
RE31591, May 29, 1984
Filed:
Nov 30, 1981
Appl. No.:
6/325706
Inventors:
George T. Drakeley - Bellevue WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64D 3304
US Classification:
244110B
Abstract:
Production of a downwardly and forwardly directed reverse thrust discharged from a reverse-thrust duct is controlled. Iadd. during landing. Iaddend. by a door in the rearward-discharge duct having its rearward portion pivotally mounted for swinging of its forward portion between a position lodged in a recess in the side of the rearward-discharge duct and a position in which the forward edge of the door is spaced from the recess and the door is inclined to deflect jet exhaust from the rearward-discharge duct into the reverse-thrust duct branching from the rearward-discharge duct. The discharge end of the reverse-thrust duct can be closed by a second door and actuating. [. means. ]. . Iadd. mechanism. Iaddend. interconnecting the two doors can move them simultaneously through proportionate degrees of movement.
Fuselage Tail Jet Engine Thrust Reverser
US Patent:
3997134, Dec 14, 1976
Filed:
Mar 27, 1975
Appl. No.:
5/562587
Inventors:
George T. Drakeley - Bellevue WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64D 3304
US Classification:
244110B
Abstract:
Production of a downwardly and forwardly directed reverse thrust discharged from a reverse-thrust duct is controlled by a door in the rearward-discharge duct having its rearward portion pivotally mounted for swinging of its forward portion between a position lodged in a recess in the side of the rearward-discharge duct and a position in which the forward edge of the door is spaced from the recess and the door is inclined to deflect jet exhaust from the rearward-discharge duct into the reverse-thrust duct branching from the rearward-discharge duct. The discharge end of the reverse-thrust duct can be closed by a second door and actuating means interconnecting the two doors can move them simultaneously through proportionate degrees of movement.
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