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Edmund Hall Hindle

from Palm Beach Gardens, FL
Age ~64
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Also known as:
Edmund H Hindle, Edmund Rd Hindle, Heidi K Hindle, Heidi Kathleen Hindle, Ed H Hindle, Heide Hindle, Edmond Hindle
Related to:
Hunter P Hindle, 33
Connected to:
Brian B Hindle, 35Philip A Hindle, 75Carl Hindley, 66Damian A Hindley, 46Joshua A Hindley, 42Michele A Hindley, 53Ann M Hindman, 79Bob J Hindman, 87Erica L Hindman, 37Jake W Hindman, 38

Edmund Hindle Phones & Addresses

  • Palm Beach Gardens, FL
  • Las Vegas, NV
  • Destin, FL
  • Miamisburg, OH
  • Broken Arrow, OK
  • Saint Petersburg, FL
  • West Chester, OH
  • Dunedin, FL
  • Port Saint Lucie, FL
  • Mendon, NY

Publications

Us Patents

Blade Lock Screw

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US Patent:
H12580, Dec 7, 1993
Filed:
Sep 16, 1992
Appl. No.:
7/945552
Inventors:
Edmund H. Hindle - North Palm Beach FL
Assignee:
The United States of America as represented by the Secretary of the Air
Force - Washington DC
International Classification:
F01D 532
US Classification:
416215
Abstract:
This disclosure relates to the blade lock that serves to secure the blades to the drum rotor of a compressor in a gas turbine engine that is characterized by its ease of removal upon disassembly. The blade lock consists of two components, a locking member that engages the surface of a shoulder formed in the drum of the drum rotor and a screw threadably engaging a threaded central bore formed in the locking member having a platen engaging the bottom surface of the recess to urge the locking member to bear against the shoulder and where the screw carries three equally spaced longitudinal slots formed around the periphery of the threaded portion of the threads of the screw.

Method And Apparatus For Determining Engine Part Life Usage

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US Patent:
20060265183, Nov 23, 2006
Filed:
May 10, 2005
Appl. No.:
11/126100
Inventors:
Kenneth Jacques - West Chester OH, US
Mark Butz - Loveland OH, US
Edmund Hindle - West Chester OH, US
Robert Van Stone - Cincinnati OH, US
International Classification:
G06F 17/18
US Classification:
702181000
Abstract:
A method for determining an engine part life usage of a gas turbine engine life limited part used on an aircraft. The method includes operating a gas turbine engine that includes a plurality of rotating components and a plurality of sensors configured to monitor a plurality of gas turbine engine operating parameters, obtaining outputs from the plurality of sensors, and utilizing at least some of the outputs to calculate the life usage of at least one life limited part to facilitate tracking the life-usage of an individual life limited part on the gas turbine engine that is consumed on a flight by flight basis.
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Edmund Hall Hindle from Palm Beach Gardens, FL, age ~64 Get Report