Peter E Voyer from 103 Shore Rd, Ellington, CT 06029, age 89, Phone: 8608717737

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Peter E. Voyer
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103 W Shr Rd, Ellington, CT 06029
8608750112

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Process For Welding Flanges To A Cylindrical Engine Casing Having A Plurality Of Spaced Rails And Ribs
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US Patent:

42087740, Jun 24, 1980
Filed:

Nov 27, 1978
Appl. No.:

5/964104
Inventors:

Peter E. Voyer - Tolland CT
Thomas C. Walsh - New Britain CT
Joseph Grzyb - Manchester CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

B23P 1500
US Classification:

291564R
Abstract:

The method disclosed herein is the improved construction of an engine split case by electron beam welding the mating flanges to the split case cylinder where the outer diameter of the case includes "L" shaped rails and radial circumferential flanges.

Rotor Blade Assembly
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US Patent:

44512058, May 29, 1984
Filed:

Feb 22, 1982
Appl. No.:

6/351061
Inventors:

Keith T. Honda - Manchester CT
Stephen L. Smith - South Windsor CT
Peter E. Voyer - Tolland CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F01D 530
F01D 522
F01D 532
US Classification:

416219R
Abstract:

Rotor blade and disk structures enabling the disassembly and reassembly of a single rotor blade are disclosed. The concepts are particularly suited to configurations employing interlocking mid-span shrouds which inhibit the withdrawal of a single blade from a disk. In one specific geometry the rotor blade root section (20) and the disk attachment slot (24) are contoured to provide increasing clearance between the bottom of the blade root section and the attachment slot as the blade is withdrawn axially from the slot. Rocking of the blade within the provided clearance enables withdrawal of the blade around the shroud segments (30,32) and airfoil sections (16) of the adjacent blades (12).

Self-Actuating Rotor Seal
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US Patent:

44640960, Aug 7, 1984
Filed:

Nov 1, 1979
Appl. No.:

6/090189
Inventors:

Edmund D. Trousdell - Tolland CT
Peter E. Voyer - Tolland CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F01D 530
US Classification:

416215
Abstract:

A rim seal for blocking the leakage of working medium gases between an array of rotor blades and a rotor disk is disclosed. Various construction details which provide positive contact between the seal and the disk are developed. The rim seal of the present invention is of the ladder-type having application to a disk adapted by a circumferential groove to receive the rotor blades.

Rotor Assembly Having A Multistage Disk
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US Patent:

43102867, Jan 12, 1982
Filed:

May 17, 1979
Appl. No.:

6/040010
Inventors:

Gary P. Peters - Lebanon CT
Robert L. Rowley - Glastonbury CT
Peter E. Voyer - Tolland CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F01D 506
US Classification:

416198A
Abstract:

A lightweight, rotor assembly for a gas turbine engine having a critical speed characteristic well above the operating speed is disclosed. Various construction details which enhance the axial stiffness of the rotor assembly and which shield a portion of the disk from working medium gases are developed. The rotor assembly employs a frustoconical member to connect a shaft to the disk.

Method For Manufacturing A Split Engine Casing From A Cylinder
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US Patent:

42087775, Jun 24, 1980
Filed:

Nov 27, 1978
Appl. No.:

5/964103
Inventors:

Thomas C. Walsh - New Britain CT
Peter E. Voyer - Tolland CT
Francis J. Wallace - Windsor CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

B23P 1500
US Classification:

29418
Abstract:

The method of fabricating a jet engine casing into two removable halves is disclosed. The method includes turning a cylindrical blank to obtain the radial structural ribs, diametrically slotting axially the outer diameter to receive two mating flanges and boring the inside diameter to remove sufficient material to expose the inner edge of the mating flanges whereby the casing is split along the axial axis.

Abradable Rub Strip
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US Patent:

43493130, Sep 14, 1982
Filed:

Dec 26, 1979
Appl. No.:

6/106582
Inventors:

Alan D. Munroe - Glastonbury CT
Peter E. Voyer - Tolland CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F01D 1108
US Classification:

415174
Abstract:

An abradable rub strip for use in the compression section of a gas turbine engine is disclosed. Various construction details are developed for limiting penetration of the abradable rub strip by an array of rotor blades. A ring formed of metallic material is embedded in the abradable rub strip.

Rotor Blade Assembly
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US Patent:

RE339547, Jun 9, 1992
Filed:

Dec 24, 1990
Appl. No.:

7/656337
Inventors:

Keith T. Honda - Manchester CT
Stephen L. Smith - South Windsor CT
Peter E. Voyer - Tolland CT
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F01D 530
US Classification:

416219R
Abstract:

Rotor blade and disk structures enabling the disassembly and reassembly of a single rotor blade are disclosed. The concepts are particularly suited to configurations employing interlocking mid-span shrouds which inhibit the withdrawal of a single blade from a disk. In one specific geometry the rotor blade root section (20) and the disk attachment slot (24) are contoured to provide increasing clearance between the bottom of the blade root section and the attachment slot as the blade is withdrawn axially from the slot. Rocking of the blade within the provided clearance enables withdrawal of the blade around the shroud segments (30,32) and airfoil sections (16) of the adjacent blades (12).