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Timothy B Lauder

from Matthews, NC
Age ~56
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Also known as:
Tim B Lauder
Phone and address:
123 Southern Cross Ln, Matthews, NC 28105
(704) 708-5858
Related to:
Ardath Paige Jur, 45Paige Amanda Rubendall, 28
Connected to:
Ashley LauderbackBobbie J Lauderdale, 73Brittany Lauderdale, 38Earle C Lauderdale, 73Elizabeth A Lauderdale, 60Eva J LauderdaleIssis Y Lauderdale, 32Jane E Lauderdale, 62Lynn Lauderdale, 65Lynne A Lauderdale, 70

Timothy Lauder Phones & Addresses

  • 123 Southern Cross Ln, Matthews, NC 28105 (704) 708-5858 (704) 708-5859
  • Southport, NC
  • Charlotte, NC
  • Rocky Hill, CT
  • Fairfield, CT
  • 123 Southern Cross Ln, Matthews, NC 28105 (704) 635-1228

Work

Position: Production Occupations

Education

Degree: Bachelor's degree or higher

Resumes

Resumes

Timothy Lauder Photo 1

Svp - Home Loans And Insurance Process Improvement At Bank Of America

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Location:
Charlotte, North Carolina Area
Industry:
Banking
Timothy Lauder Photo 2

Svp At Bank Of America

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Location:
Charlotte, North Carolina Area
Industry:
Information Technology and Services

Publications

Us Patents

Rotary-Wing Aircraft With A Common Dynamic System/Backbone Structure

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US Patent:
D614559, Apr 27, 2010
Filed:
Sep 14, 2007
Appl. No.:
29/284739
Inventors:
Mark R. Alber - Milford CT, US
Benjamin Reed Hein - Milford CT, US
Alfred Russell Smiley - Marlborough CT, US
Timothy F. Lauder - Oxford CT, US
William J. Eadie - Cheshire CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
0912
US Classification:
D12326

Winch System For Vtol Aircraft

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US Patent:
7909308, Mar 22, 2011
Filed:
Apr 19, 2007
Appl. No.:
12/527612
Inventors:
Timothy F. Lauder - Oxford CT, US
Janiece M. Lorey - New Haven CT, US
Christopher M. Harrington - Milford CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B66D 3/00
B66D 1/26
B65H 75/18
US Classification:
254382, 254278, 254334, 242603
Abstract:
A winch system includes a cable storage system (), a drive system () and a deployment system to deploy a cable having a hook system attached thereto. A right angle sheave () guides the cable between the cable storage system and the drive system. The drive system includes a dual mode transmission that provides high speed capabilities when moderate to no load is being lifted, while also providing high torque for heavy lift operations at low speeds. The deployment system is rated to support a maximum hook load and is mounted to the airframe for pivotable movement about a deployment axis to enable large cable exit angles.

System And Method Of Damping A 1P Motion

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US Patent:
8038394, Oct 18, 2011
Filed:
Jan 16, 2008
Appl. No.:
12/015149
Inventors:
Brandon L. Stille - Cheshire CT, US
William A. Welsh - North Haven CT, US
Timothy Fred Lauder - Oxford CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
F01D 5/18
US Classification:
416 1, 416106, 416500
Abstract:
A rotor system includes a multiple of rotor blade yokes mounted to a rotor hub. A lead/lag damper is mounted to each of the rotor blade yokes and to a damper hub. An actuator system is operable to shift a damper hub axis of rotation relative the rotor axis of rotation to minimize 1P damper motions. A method of minimizing 1P damper motions within a rotor system includes shifting the damper hub axis of rotation relative the rotor axis of rotation to oscillate an inner connector of each lead/lag damper in phase with a 1P blade motion to minimize the 1P motion of the damper.

Rotary Wing Aircraft

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US Patent:
D665720, Aug 21, 2012
Filed:
Jan 11, 2012
Appl. No.:
29/410676
Inventors:
Brandon L. Stille - Cheshire CT, US
Ashley DeVito - Newtown CT, US
Benjamin Reed Hein - Milford CT, US
Timothy Fred Lauder - Oxford CT, US
Patrick Boyle - New Haven CT, US
Mark R. Alber - Milford CT, US
William J. Eadie - Cheshire CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
1207
US Classification:
D12326

Planetary De-Rotation System For A Shaft Fairing System

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US Patent:
8534596, Sep 17, 2013
Filed:
Jan 2, 2008
Appl. No.:
12/810186
Inventors:
Timothy Fred Lauder - Oxford CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B64C 27/00
US Classification:
244 1719, 244 1723, 416129
Abstract:
A de-rotation system includes a planetary gear set, and a fairing support structure mounted for rotation with a first ring gear.

Magnetic De-Rotation System For A Shaft Fairing System

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US Patent:
8584983, Nov 19, 2013
Filed:
Dec 3, 2007
Appl. No.:
12/745718
Inventors:
Jayant Sirohi - Milford CT, US
Timothy Fred Lauder - Oxford CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B64C 27/51
US Classification:
244 1727, 244 1723, 244 1725
Abstract:
A magnetic de-rotation system includes an inner ring which supports an eddy current ring and at least one inner ring magnet and an outer ring which supports at least one outer ring magnet, attraction between the at least one inner ring magnet and the at least one outer ring magnet produces a stable rotational position for a fairing.

Electric Powered Rotary-Wing Aircraft

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US Patent:
20090140095, Jun 4, 2009
Filed:
Jan 23, 2008
Appl. No.:
12/018217
Inventors:
Jayant Sirohi - Milford CT, US
Timothy Fred Lauder - Oxford CT, US
Mark R. Alber - Milford CT, US
Daniel Bazzani - Milford CT, US
International Classification:
B64C 27/04
B64C 19/00
US Classification:
244 1719, 244 1711, 244 751
Abstract:
A rotary-wing aircraft with an electric motor mounted along an axis of rotation to drive a rotor system about the axis of rotation.

Rotary Wing Aircraft Propulsion System

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US Patent:
20130228647, Sep 5, 2013
Filed:
Mar 5, 2012
Appl. No.:
13/411782
Inventors:
Joseph Simonetti - Southbury CT, US
Matthew J. Tarascio - Milford CT, US
Michael Peter Strauss - New Haven CT, US
Adam Kasprzyk - Shelton CT, US
Timothy Fred Lauder - Oxford CT, US
Assignee:
SIKORSKY AIRCRAFT CORPORATION - Stratford CT
International Classification:
B64C 27/82
B64D 37/00
B64D 13/08
B64D 41/00
B64D 15/00
US Classification:
244 1721, 244 58, 244134 R
Abstract:
A rotary wing aircraft propulsion system includes an engine, a heat exchanger cooling a fluid from the engine and a thermoelectric generator in thermal communication with the fluid to generate electrical power. The thermoelectric generator provides electrical power to at least one aircraft component.
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Timothy B Lauder from Matthews, NC, age ~56 Get Report