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Kenneth A Allard

from Chicopee, MA
Age ~60

Kenneth Allard Phones & Addresses

  • Chicopee, MA
  • 46 Canterbury Rd, Springfield, MA 01118 (413) 782-8737
  • 42 Canterbury Rd, Springfield, MA 01118
  • Spfld, MA
  • 365 Cedar Swamp Rd, Monson, MA 01057 (413) 267-4216
  • Wilbraham, MA
  • Pleasantville, NY
  • 19 Tinkham Gln, Wilbraham, MA 01095

Work

Position: Sales Occupations

Education

Degree: High school graduate or higher

Professional Records

License Records

Kenneth N Allard

Address:
Chicopee, MA 01020
License #:
18566 - Active
Issued Date:
Apr 27, 1970
Expiration Date:
Jul 31, 2019
Type:
Journeyman Electrician

Resumes

Resumes

Kenneth Allard Photo 1

Kenneth Allard

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Kenneth Allard Photo 2

Kenneth Allard

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Work:
United States
Kenneth Allard Photo 3

Director, Engineering Operations At Cb Richard Ellis / Ne

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Location:
Springfield, Massachusetts Area
Industry:
Real Estate
Kenneth Allard Photo 4

Asst. Manager At The Bell / Simons Co

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Location:
Springfield, Massachusetts Area
Industry:
Oil & Energy

Publications

Isbn (Books And Publications)

Somalia Operations: Lessons Learned

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Author

Kenneth Allard

ISBN #

0160455774

Somalia Operations: Lessons Learned

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Author

Kenneth Allard

ISBN #

0788146629

Somalia Operations: Lessons Learned

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Author

Kenneth Allard

ISBN #

0898758858

Us Patents

High Load Capacity Bi-Directional Tapered Roller Bearing

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US Patent:
6464401, Oct 15, 2002
Filed:
Jan 26, 2001
Appl. No.:
09/771194
Inventors:
Kenneth L. Allard - Wilbraham MA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F16C 3358
US Classification:
384571, 384561
Abstract:
The present invention is a bi-directional tapered roller bearing having a first cone rib ring thrust face âCâ adjacent and facing the small diameter end faces of the roller elements, a second cone rib ring thrust face âBâ adjacent and facing the large diameter end faces of the roller elements, and a cup rib ring thrust face âAâ adjacent and facing the large diameter end faces of the roller elements. The bearing components are arranged such that, during primary thrust load operation, there is a gap between thrust face C and the small diameter end faces of the roller elements, a gap between thrust face A and the large diameter end faces of the roller elements, and contact between thrust face B and the large diameter end faces of the roller elements. With this arrangement, bearing roller element centrifugal loads act to reduce the contact forces between the roller elements and the bearing races.

Bifurcated Oil Scavenge System For A Gas Turbine Engine

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US Patent:
6996968, Feb 14, 2006
Filed:
Dec 17, 2003
Appl. No.:
10/738354
Inventors:
Robert E. Peters - Portland CT, US
Dwayne Messerschmidt - Columbia CT, US
J. Axel Glahn - Manchester CT, US
Kenneth L. Allard - Wilbraham MA, US
Hsianmin F. Jen - Woodbridge CT, US
Larry W. Spires - Unionville CT, US
Roger M. Barnsby - Manchester CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 7/06
US Classification:
60 3908
Abstract:
An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

Method Of Scavenging Oil Within A Gas Turbine Engine

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US Patent:
7373780, May 20, 2008
Filed:
Oct 25, 2005
Appl. No.:
11/257689
Inventors:
Robert E. Peters - Portland CT, US
Dwayne Messerschmidt - Columbia CT, US
J. Axel Glahn - Manchester CT, US
Kenneth L. Allard - Wilbraham MA, US
Hsianmin F. Jen - Woodbridge CT, US
Larry W. Spires - Unionville CT, US
Roger M. Barnsby - Manchester CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 7/00
US Classification:
60772, 60 3908, 184 611
Abstract:
An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

Bifurcated Oil Scavenging Bearing Compartment Within A Gas Turbine Engine

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US Patent:
7430850, Oct 7, 2008
Filed:
Oct 25, 2005
Appl. No.:
11/257940
Inventors:
Robert E. Peters - Portland CT, US
Dwayne Messerschmidt - Columbia CT, US
J. Axel Glahn - Manchester CT, US
Kenneth L. Allard - Wilbraham MA, US
Larry W. Spires - Unionville CT, US
Roger M. Barnsby - Manchester CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 7/06
US Classification:
60 3908, 184 611
Abstract:
An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

Bifurcated Oil Scavenging Bearing Compartment Within A Gas Turbine Engine

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US Patent:
7625126, Dec 1, 2009
Filed:
Apr 15, 2008
Appl. No.:
12/102997
Inventors:
Robert E. Peters - Portland CT, US
Dwayne Messerschmidt - Columbia CT, US
J. Axel Glahn - Manchester CT, US
Kenneth L. Allard - Wilbraham MA, US
Larry W. Spires - Unionville CT, US
Roger M. Barnsby - Manchester CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F16C 33/66
US Classification:
384473, 384462, 384474
Abstract:
An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

Active Clearance Control

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US Patent:
45765472, Mar 18, 1986
Filed:
Nov 3, 1983
Appl. No.:
6/548466
Inventors:
Harvey I. Weiner - South Windsor CT
Kenneth L. Allard - Wilbraham MA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 716
US Classification:
415116
Abstract:
The bore of the compressor for a gas turbine engine is heated by selectively bleeding compressor air from downstream stages so that heating only occurs at discreet times during the engine operating envelope. The bled air is admitted into the bore at the mid-stage station of the compressor wherein the compressor disks are scrubbed so as to expand and close the gap between the outer air seal and tips of the compressor blades during cruise of the aircraft and prevented from heating the disks during the high powered operations of the engine.
Kenneth A Allard from Chicopee, MA, age ~60 Get Report