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Darren Michael Wind

from Glastonbury, CT
Age ~48

Darren Wind Phones & Addresses

  • 164 Chimney Sweep Hill Rd, Glastonbury, CT 06033 (860) 659-4265
  • 150 Pearl St, Middletown, CT 06457 (860) 346-7433
  • 1189 Washington St, Middletown, CT 06457 (860) 346-7433
  • 465 Buckland Hills Dr, Manchester, CT 06040 (860) 648-9006
  • 626 Castle Meadows Ct, Ballwin, MO 63021 (636) 207-0157
  • West Palm Beach, FL
  • Waterford, NY

Work

Position: Professional/Technical

Education

Degree: Associate degree or higher

Publications

Us Patents

Determination Of A Clearance And A Position Of A Target

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US Patent:
20190353473, Nov 21, 2019
Filed:
May 16, 2018
Appl. No.:
15/981112
Inventors:
- Farmington CT, US
Ian F. Agoos - Boston MA, US
Darren M. Wind - Glastonbury CT, US
International Classification:
G01B 11/14
Abstract:
Disclosed is a first transmitter that transmits a first optical signal towards a target, a plurality of receivers that receive the first optical signal after the first optical signal is reflected by the target and each provides a respective received optical signal, at least one photodetector that receives the received optical signals and provides at least a first electrical signal, and a processor that receives the first electrical signal to compute a position of the target relative to a baseline position based on: a first position of a first receiver of the plurality of receivers, a second position of a second receiver of the plurality of receivers, the first electrical signal. The processor computes a clearance between the target and a component based on a third position of a third receiver, a fourth position of a fourth receiver and a second electrical signal.

Wear Indicator For Gas Turbine Engine

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US Patent:
20180252117, Sep 6, 2018
Filed:
Mar 6, 2017
Appl. No.:
15/450939
Inventors:
- Farmington CT, US
Darren M. Wind - Glastonbury CT, US
Ian Alexander Fielder Agoos - Boston MA, US
International Classification:
F01D 21/00
G01B 21/16
Abstract:
In combination a wear indicator and a component of a gas turbine engine is provided. The wear indicator is secured to a surface of the component of the gas turbine engine. The wear indicator comprising: a first side delaminates when impacted by a blade of the gas turbine engine; a second side parallel to the first side, the second side being secured to a surface of the component of the gas turbine engine; a mid-section interposed between the first side and the second side; and a reference dimension remains constant when the first side delaminates.

Multiple Laser Time Of Arrival Probe

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US Patent:
20140268100, Sep 18, 2014
Filed:
Dec 19, 2013
Appl. No.:
14/134452
Inventors:
- Hartford CT, US
Robert Kujawa - Stuart FL, US
Darren M. Wind - Glastonbury CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
G01B 11/16
US Classification:
356 32
Abstract:
A system and method for performing stress measurement on rotating parts is disclosed. The system may include a laser assembly configured to emit a plurality of laser beams having different wavelengths, and a probe assembly mounted proximal to a rotatable part in a device. The probe assembly may be configured to output a reflected laser beam onto a first target on the rotatable part. The probe assembly may be configured to output another reflected laser beam onto a second target on the rotatable part. The probe assembly may include a redirector, and a lens assembly mounted proximal to the redirector and configured to converge the laser beams. The redirector may be configured to change the direction of each emitted laser beam.

Traversing Time Of Arrival Probe

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US Patent:
20140165736, Jun 19, 2014
Filed:
Dec 19, 2012
Appl. No.:
13/719575
Inventors:
- Hartford CT, US
Robert Kujawa - Stuart FL, US
Darren M. Wind - Glastonbury CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
G01L 1/24
US Classification:
73760, 356445
Abstract:
A system and method for performing stress measurement on rotating parts is disclosed. The system may include a laser assembly configured to emit a laser beam, and a probe assembly mounted proximal to a rotatable part in a device. The probe assembly may be configured to output a reflected laser beam onto a first target on the rotatable part. The probe assembly may further be configured to move the reflected laser beam from the first target to a second target on the rotatable part. The probe assembly may include a redirector moveable from a first position to a second position, and a lens mounted proximal to the redirector and configured to focus the laser beam. The redirector may be configured to change the laser beam direction from a first direction to a second direction when moved from the first position to the second position.
Darren Michael Wind from Glastonbury, CT, age ~48 Get Report