KENNETH E TAYLOR
Engineering in Springfield, MA

License number
Massachusetts 30355
Issued Date
Feb 27, 1981
Expiration Date
Jun 30, 2018
Type
Mechanical Engineer
Address
Address
Springfield, MA 01106

Personal information

See more information about KENNETH E TAYLOR at radaris.com
Name
Address
Phone
Kenneth Taylor
48 Alpine St, Somerville, MA 02144
(617) 605-2201
Kenneth Taylor
507 Main St APT 1108, Worcester, MA 01608
Kenneth Taylor
44 Central Ave, Plymouth, MA 02360
(508) 759-3158

Professional information

See more information about KENNETH E TAYLOR at trustoria.com
Kenneth Taylor Photo 1
Mold With Starter And Selector Sections For Directional Solidification Casting

Mold With Starter And Selector Sections For Directional Solidification Casting

US Patent:
4548255, Oct 22, 1985
Filed:
Jul 23, 1984
Appl. No.:
6/633071
Inventors:
Martin J. Reiner - South Windsor CT
Kenneth E. Taylor - Longmeadow MA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B22C 902
US Classification:
164361
Abstract:
Directional solidification of a single crystal superalloy article may be accomplished using a mold with a starter section, and a selector section to convert columnar growth from the starter into single crystal growth. In such a process, the deviation of [001] crystallographic orientation with respect to the longitudinal axis of the article being formed is reduced from 9 degrees to 5 degrees by controlling the heat transfer in the starter section. A stepped starter section, wherein the lower subsection has a volume of 52-98% of the total starter volume, and wherein the upper subsection is relatively small in lateral dimension, has been found most useful. When the solidification interface moves into the smaller width upper subsection, it becomes more nearly planar, and results in improved columnar growth in the starter, and in reduction in the crystallographic deviation of the article.


Kenneth Taylor Photo 2
Method For Making A Turbine Blade Having A Wear Resistant Layer Sintered To The Blade Tip Surface

Method For Making A Turbine Blade Having A Wear Resistant Layer Sintered To The Blade Tip Surface

US Patent:
4851188, Jul 25, 1989
Filed:
Dec 21, 1987
Appl. No.:
7/135956
Inventors:
Robert P. Schaefer - East Hartford CT
Walter F. Gustafson - Manchester CT
David A. Rutz - Glastonbury CT
Kenneth E. Taylor - Longmeadow MA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B22F 700
US Classification:
419 19
Abstract:
An abrasive, wear resistant layer is applied to the tip surface of a superalloy gas turbine blade by high temperature sintering operation which produces a high strength bond between the layer and the blade, minimizes gamma prime phase growth, and prevents recrystallization in the blade. Important features of the invention include removing plastic strain damage from the tip surface prior to the sintering operation, using induction heating techniques to sinter a layer of metal powder particles and ceramic particulates to the blade tip surface, and shielding the airfoil and root portion of the blade from the radiant heating source during the sintering operation while at the same time, conductively removing heat from the blade.


Kenneth Taylor Photo 3
Induction Furnace Having Improved Thermal Profile

Induction Furnace Having Improved Thermal Profile

US Patent:
4409451, Oct 11, 1983
Filed:
Aug 31, 1981
Appl. No.:
6/297900
Inventors:
Kenneth E. Taylor - Longmeadow MA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
H05B 630, H05B 640
US Classification:
219 1049R
Abstract:
Apparatus for casting directionally solidified articles is disclosed. Concepts for obtaining a desired temperature profile in an induction furnace are discussed. An induction furnace 10 has increased heating capacity at the withdrawal end 32 of the susceptor 28. A hot zone baffle 42 is disposed at the withdrawal end to inhibit the radiation of heat energy from the hot zone 12. A plurality of grooves 34 are formed about the interior of the susceptor at the withdrawal end to inhibit the conduction of heat energy out of the susceptor. A preferred thermal profile in the operating furnace with a peak temperature in close proximity to the withdrawal end results.