Search

Dinesh N Taneja

from Tavares, FL
Age ~75

Dinesh Taneja Phones & Addresses

  • 377 David Walker Dr, Tavares, FL 32778 (937) 657-2018
  • 230 Timberwind Ln, Vandalia, OH 45377 (937) 454-5367
  • Erie, PA
  • Montgomery, OH
  • 230 Timberwind Ln, Vandalia, OH 45377 (937) 657-2018

Work

Position: Professional/Technical

Education

Degree: Graduate or professional degree

Emails

Publications

Us Patents

System For Powering A Vehicle

View page
US Patent:
8561413, Oct 22, 2013
Filed:
Dec 29, 2010
Appl. No.:
12/981044
Inventors:
Dinesh Nath Taneja - Vandalia OH, US
Assignee:
GE Aviation Systems, LLC - Grand Rapids MI
International Classification:
F02C 7/275
US Classification:
60788, 60 39091
Abstract:
A method and system operating an aircraft system are provided. The gas turbine engine system includes a low-pressure (LP) shaft, a high-pressure (HP) shaft, a constant speed mechanical drive assembly having an input and an output, the input mechanically coupled to the LP shaft, the output mechanically coupled to a constant frequency (CF) electrical generator, and an accessory gearbox assembly having an input and an output, the input mechanically coupled to the HP shaft, the output mechanically coupled to a variable frequency (VF) electrical generator.

Dual-Structured Aircraft Engine Starter/Generator

View page
US Patent:
20080093850, Apr 24, 2008
Filed:
May 3, 2007
Appl. No.:
11/797451
Inventors:
Dinesh Taneja - Vandalia OH, US
Hao Huang - Troy OH, US
Gary Padgett - Kettering OH, US
Jan Zywot - Centerville OH, US
Paul Wirsch - Springboro OH, US
Mohamed Abbas - Huber Heights OH, US
International Classification:
B64D 31/02
F02N 11/04
US Classification:
29003600R, 24405300A, 290047000
Abstract:
An aircraft starting and generating system includes a first starter/main machine assembly that includes a first exciter and a first main machine, and second starter/main machine assembly that includes a second exciter and a second main machine. The system also includes a permanent magnet generator (PMG) that is connected to the first and second starter/main machine assemblies. The system further includes a first inverter/converter/controller (ICC) that is connected to the first starter/main machine assembly and to the PMG, and a second ICC that is connected to the second starter/main machine assembly and to the PMG. The first and second ICCs generate AC power to respective drive the first and second starter/main machine assemblies in a start mode of the starting and generating system for starting a prime mover of the aircraft, and the first and second ICCs convert AC power, respectively obtained from the PMG after the prime mover has been started, to DC power in a generate mode of the starting and generating system.

Method And Apparatus For Extracting Electrical Power From A Gas Turbine Engine

View page
US Patent:
20130062885, Mar 14, 2013
Filed:
Sep 8, 2011
Appl. No.:
13/227597
Inventors:
Dinesh Nath Taneja - Vandalia OH, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
H02K 7/18
B60L 1/00
H02K 23/52
US Classification:
290 1 A, 290 46, 307 91
Abstract:
A method and apparatus for powering an aircraft by extracting power from both the high pressure and low pressure spools of a gas turbine engine. DC power can be generated using the high pressure spool and AC power can be generated using the low pressure spool.

Ram Air Turbine With Integrated Heat Exchanger

View page
US Patent:
20130071232, Mar 21, 2013
Filed:
Sep 21, 2011
Appl. No.:
13/238880
Inventors:
Dinesh Nath Taneja - Vandalia OH, US
John Andrew Layer - East Aurora NY, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
F01D 15/12
US Classification:
4151221
Abstract:
A ram air turbine system for generating electrical power in an aircraft when the system is exposed to an airstream exterior of the aircraft. The ram air turbine system includes a turbine, a housing defining an interior, a gearbox having a speed-increasing gear train, and a generator.

Method For Conditioning A Power Supply For Starting A Jet Engine

View page
US Patent:
20140020401, Jan 23, 2014
Filed:
Jul 18, 2012
Appl. No.:
13/552071
Inventors:
Dinesh Nath Taneja - Vandalia OH, US
Krishna Jonnalagadda - Mason OH, US
Pranav N. Patel - West Chester OH, US
Assignee:
GE AVIATION SYSTEMS LLC - Grand Rapids MI
International Classification:
F02C 7/26
US Classification:
60778
Abstract:
Method for conditioning a power supply for starting a jet engine having an electrical starting system with an auxiliary power unit in parallel with a DC power supply.
Dinesh N Taneja from Tavares, FL, age ~75 Get Report