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Monte A Mcglaun

from Abilene, TX
Age ~74

Monte Mcglaun Phones & Addresses

  • 2118 Crestline Dr, Abilene, TX 79602 (325) 677-5766
  • Fries, VA

Work

Position: Machine Operators, Assemblers, and Inspectors Occupations

Emails

Publications

Us Patents

System For Heat Dissipation From An Internal Actuator In A Rotor Blade

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US Patent:
20130058793, Mar 7, 2013
Filed:
Sep 7, 2011
Appl. No.:
13/227181
Inventors:
Troy C. Schank - Keller TX, US
Monte A. McGlaun - Abilene TX, US
International Classification:
F01D 5/18
US Classification:
416 96 A
Abstract:
A rotor blade for an aircraft includes an airfoil skin, an active element, and an actuator configured to operate the active element. A heat pipe is configured to promote heat transfer from the actuator to the airfoil skin. The heat pipe has a slope gradient such that a centrifugal force generated during rotation of the rotor blade promotes travel of a condensed working fluid within the heat pipe to move from a condenser end of the heat pipe toward an evaporator end of the heat pipe.

Stretched Membrane Mirror And Method Of Making Same

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US Patent:
56802625, Oct 21, 1997
Filed:
May 26, 1995
Appl. No.:
8/452410
Inventors:
Patrick K. Soliday - Abilene TX
Gary W. Thomas - Abilene TX
Monte A. McGlaun - Abilene TX
Michael J. Taylor - Abilene TX
Assignee:
Cummins Power Generation, Inc. - Columbus IN
International Classification:
G02B 508
G02B 7188
US Classification:
359840
Abstract:
A method of fabricating a reflective stretched membrane mirror for use in the collection and focusing of solar energy includes a tensioning fixture to which a plurality of air-actuated cylinders are attached. The piston arm of each cylinder is in turn connected to an air-actuated clamp which is designed to hold a portion of the peripheral edge of the reflective film which is to be stretched. Depending upon the properties of the film and its tensioning characteristics, cylinders which need the same air pressure are connected in common to a single regulator. The regulators are then connected to an air compressor and the sheet of reflective film is tensioned to a desired level at which point it is adhesively bonded to a circular frame. Once a first reflective film is bonded to a top side of the frame, the process is repeated with a second reflective film bonded to the back or opposite side of the frame. Once both reflective films have been securely bonded to the frame surfaces, a vacuum is pulled on the interior space so as to create a parabolic contour in the film.

Method Of Making A Stretched Membrane Mirror From Film With Anistropy Properties

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US Patent:
55520065, Sep 3, 1996
Filed:
May 30, 1995
Appl. No.:
8/453993
Inventors:
Patrick K. Soliday - Abilene TX
Gary W. Thomas - Abilene TX
Monte A. McGlaun - Abilene TX
Michael J. Taylor - Abilene TX
Assignee:
Cummins Power Generation, Inc. - Columbus IN
International Classification:
B32B 714
B29D 1100
US Classification:
156160
Abstract:
A method of fabricating a reflective stretched membrane mirror for use in the collection and focusing of solar energy includes a tensioning fixture to which a plurality of air-actuated cylinders are attached. The piston arm of each cylinder is in turn connected to an air-actuated clamp which is designed to hold a portion of the peripheral edge of the reflective film which is to be stretched. Depending upon the properties of the film and its tensioning characteristics, cylinders which need the same air pressure are connected in common to a single regulator. The regulators are then connected to an air compressor and the sheet of reflective film is tensioned to a desired level at which point it is adhesively bonded to a circular frame. Once a first reflective film is bonded to a top side of the frame, the process is repeated with a second reflective film bonded to tile back or opposite side of the frame. Once both reflective films have been securely bonded to the frame surfaces, a vacuum is pulled on the interior space so as to create a parabolic contour in the film.

Aircraft Gaseous Cooling System

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US Patent:
20160025206, Jan 28, 2016
Filed:
Jul 24, 2014
Appl. No.:
14/340340
Inventors:
- Fort Worth TX, US
Monte McGlaun - Abilene TX, US
Travis Jurell - Fort Worth TX, US
International Classification:
F16H 57/04
Abstract:
One aspect of a cooling system includes a gas source connected to a component to be cooled. The gas source continuously supplies compressed gas to the component in response to an input. The cooling system also includes a controller connected to the gas source, the controller to provide the input to the gas source to continuously supply the compressed gas to the component.

Bearing Raceway Heat Distribution Using Heat Pipes

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US Patent:
20150316106, Nov 5, 2015
Filed:
May 1, 2014
Appl. No.:
14/266918
Inventors:
- Fort Worth TX, US
Monte Alan McGlaun - Abilene TX, US
Assignee:
BELL HELICOPTER TEXTRON INC. - Fort Worth TX
International Classification:
F16C 37/00
F28D 15/04
Abstract:
A system and method to cool a bearing. The system includes a heat pipe extending through a thickness of an inner ring of the bearing from a first surface to an opposing second surface and a cooling lubricant in fluid communication with the first surface. The method includes exposing the first surface of the roller bearing to lubricant and transferring heat energy through the heat pipes.

Non-Metallic Debris Monitoring System

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US Patent:
20150241328, Aug 27, 2015
Filed:
Feb 24, 2014
Appl. No.:
14/187409
Inventors:
- Fort Worth TX, US
Ryan Ehinger - Southlake TX, US
Joseph Gerardi - Dryden NY, US
Monte McGlaun - Abilene TX, US
Eric Olson - Fort Worth TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
G01N 15/06
G01N 29/02
Abstract:
A system and method to detect particles in a fluid stream. The system includes a separator configured to separate particles from bubbles passing through the fluid stream and a sensor configured to detect the particles. The method includes passing the fluid stream through the separator, separating the particles from bubbles passing through the fluid stream, and detecting the presence of the particles.

Passive Cooling Of Transmission Using Mast Mounted Heat Pipes

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US Patent:
20140116652, May 1, 2014
Filed:
Nov 14, 2012
Appl. No.:
13/676954
Inventors:
- Fort Worth TX, US
Monte A. McGlaun - Abilene TX, US
Assignee:
BELL HELICOPTER TEXTRON INC. - Fort Worth TX
International Classification:
F28D 15/02
US Classification:
16510421
Abstract:
A passive cooling system for an aircraft includes a rotor assembly and a closed heat pipe. The closed heat pipe is carried by the rotor assembly and configured to extract heat energy from a heat source positioned away from the rotor assembly and configured to dissipate the heat energy through the rotor assembly.
Monte A Mcglaun from Abilene, TX, age ~74 Get Report