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Ashish K Sareen

from Southlake, TX
Age ~62
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Also known as:
Ashish Kumar Sareen, Ashish K Sarcer, Ashish K Kochhar
Phone and address:
809 Boston Dr, Grapevine, TX 76092
(713) 962-4502
Related to:
Aneet Sareen, 59
Connected to:
Anita J Sareen, 52Deepti Sareen, 43Himanshu Sareen, 116Preeti Sareen, 41Rohit Sareen, 50Sameer Sareen, 40Sushma R Sareen, 73Andrew Sarega, 37Nilofar Sareh, 64Ali Y Sareini, 36

Ashish Sareen Phones & Addresses

  • 809 Boston Dr, Southlake, TX 76092 (713) 962-4502
  • 105 Parkcrest Ct, Southlake, TX 76092 (817) 912-1214
  • South Lake, TX
  • Downingtown, PA
  • Sugar Land, TX
  • Amarillo, TX
  • Euless, TX
  • Houston, TX
  • Fort Worth, TX
  • South Lake, TX

Public records

Vehicle Records

Ashish Sareen

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Address:
105 Parkcrest Dr, Southlake, TX 76092
VIN:
2T2GK31U37C018256
Make:
LEXUS
Model:
RX 350
Year:
2007

Resumes

Resumes

Ashish Sareen Photo 1

Ashish Sareen

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Location:
United States

Publications

Us Patents

Stiffness De-Coupled Skid Landing Gear

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US Patent:
6427942, Aug 6, 2002
Filed:
Jun 8, 2001
Appl. No.:
09/877428
Inventors:
John V. Howard - Arlington TX
Ramesh Thiagarajan - Plano TX
Michael R. Smith - Colleyville TX
Ashish K. Sareen - Euless TX
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64C 2552
US Classification:
244 1717, 244104 R, 244108
Abstract:
A skid landing gear for a helicopter, in which the directional stiffnesses of the cross members of the skid landing gear have been de-coupled from one another, such that optimization of the longitudinal stiffniess of the cross members may be performed independently of the optimization of the vertical stiffniess and fatigue life of the cross members. In order to de-couple the stiffnesses in the skid type landing gear, two approaches are employed. In the first approach, the skid landing gear has non-symmetric-section cross members and/or distribution of different materials within the cross-section for de-coupling the vertical stiffness of the cross members from the longitudinal stiffness, such that placement of the ground resonance frequency may be optimized, while retaining the vertical stiffness properties essential for optimizing vertical energy attenuation and fatigue life. In the second approach, mounting devices are employed that provide compliance in selected directions, thereby de-coupling the directional stiffnesses.

Cleaning And Inspecting Apparatus For Wind Turbine And Related Methods

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US Patent:
8641374, Feb 4, 2014
Filed:
Jun 30, 2010
Appl. No.:
12/827482
Inventors:
Chakradhar Byreddy - Spring TX, US
Robert Bowyer - London, GB
Ashish Sareen - Sugar Land TX, US
Assignee:
Vestas Wind Systems A/S - Aarhus N.
International Classification:
F03D 11/00
US Classification:
415232, 416 61, 416146 R
Abstract:
A maintenance apparatus is provided for use with a wind turbine that has a tower, a hub supported by the tower, and a plurality of blades extending outwardly from the hub. The maintenance apparatus has a mounting element that is configured to be secured to the tower and to be selectively movable along the length thereof. A robotic arm is coupled to the mounting element, and a blade-engaging device is coupled to the robotic arm and is configured to engage one of the blades to effect a maintenance task thereon.

Method, System, And Computer Program Product For Sensor Data Collection In A Wind Turbine

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US Patent:
20120029843, Feb 2, 2012
Filed:
Jul 30, 2010
Appl. No.:
12/847750
Inventors:
Chakradhar Byreddy - Spring TX, US
Robert Bowyer - Fulham, GB
Ashish Sareen - Sugar Land TX, US
Assignee:
VESTAS WIND SYSTEMS A/S - Randers SV
International Classification:
G01L 1/22
US Classification:
702 42
Abstract:
Method, system, and computer program product for collecting sensor readings from a component of a wind turbine. The system includes a data collection system coupled in communication with a sensor. The data collection unit includes a processor configured to direct the sensor readings from the sensor to a buffer for temporary storage and to identify a triggering event by comparing the sensor readings received from the sensor with a reference value. In response to the identification of the triggering event, the sensor readings are transferred from the buffer to the mass storage device and stored in a non-volatile form by the mass storage device.

Control Of Wind Turbines In A Wind Park

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US Patent:
20130103202, Apr 25, 2013
Filed:
Jun 19, 2011
Appl. No.:
13/806110
Inventors:
Robert Bowyer - London, GB
Ashish Sareen - Sugar Land TX, US
Chakradhar Byreddy - Spring TX, US
International Classification:
G05B 11/01
US Classification:
700275
Abstract:
A wind park comprises a plurality of wind turbines with a least one wind turbine downstream of at least one upstream turbine. The downstream turbine includes a Lidar or other device for sensing characteristics of the wake produced by the upstream turbine and for providing an output to a turbine or wind park controller indicative of the measured wake. The controller controls parameters of the downstream turbine an possibly adjacent turbines in accordance with the wake indicative signals. The control may include overrating the downstream turbine if the wake indicative signal indicates that there is a low risk of fatigue damage to components of the downstream turbine.

Stiffness De-Coupled Skid Landing Gear

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US Patent:
62445383, Jun 12, 2001
Filed:
May 19, 1999
Appl. No.:
9/314399
Inventors:
John V. Howard - Arlington TX
Ramesh Thiagarajan - Plano TX
Michael R. Smith - Colleyville TX
Ashish K. Sareen - Euless TX
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64C 2552
US Classification:
244 1717
Abstract:
A skid landing gear for a helicopter, in which the directional stiffnesses of the cross members of the skid landing gear have been de-coupled from one another, such that optimization of the longitudinal stiffness of the cross members may be performed independently of the optimization of the vertical stiffness and fatigue life of the cross members. In order to de-couple the stiffnesses in the skid type landing gear, two approaches are employed. In the first approach, the skid landing gear has non-symmetric-section cross members and/or distribution of different materials within the cross-section for de-coupling the vertical stiffness of the cross members from the longitudinal stiffness, such that placement of the ground resonance frequency may be optimized, while retaining the vertical stiffness properties essential for optimizing vertical energy attenuation and fatigue life. In the second approach, mounting devices are employed that provide compliance in selected directions, thereby de-coupling the directional stiffnesses.
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Ashish K Sareen from Southlake, TX, age ~62 Get Report