TIMOTHY JOSEPH DALE
Pilots at Vernon St, Manchester, CT

License number
Connecticut A4461785
Issued Date
Jun 2012
Expiration Date
Jun 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
182 Vernon St W, Manchester, CT 06042
LicenseFiles verified this license of May 6, 2017 at the Federal Aviation Administration.

Professional information

Timothy Dale Photo 1

Flexible Seal For Gas Turbine Engine System

US Patent:
2012013, May 31, 2012
Filed:
Jun 30, 2011
Appl. No.:
13/173522
Inventors:
Jocelyn Charis Damgaard - Vernon CT, US
Steven D. Roberts - Moodus CT, US
Timothy Dale - Manchester CT, US
Richard W. Monahan - Farmington CT, US
David C. Pimenta - Rocky Hill CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F02C 7/20, B23P 11/00
US Classification:
60796, 29888
Abstract:
A system includes a gas turbine engine, a nozzle structure located adjacent to the gas turbine engine, a flexible annular seal linking the gas turbine engine and the nozzle structure, the flexible annular seal having a plurality of corrugate sections arranged about a centerline, and a connection device secured to the gas turbine engine and to the nozzle structure. The connection device is adjustable to select a length of the flexible annular seal measured along the centerline.

Timothy Dale Photo 2

Flexible Seal System For A Gas Turbine Engine

US Patent:
2013012, May 16, 2013
Filed:
Nov 16, 2011
Appl. No.:
13/297458
Inventors:
Jocelyn C. Damgaard - Vernon CT, US
Steven D. Roberts - Moodus CT, US
Timothy Dale - Manchester CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F03B 3/00, F16J 15/02
US Classification:
4151821, 277634
Abstract:
A flexible seal system for a gas turbine engine includes an annular mounting bracket, an annular support bracket, an annular flexible seal and a plurality of mounting spacers. The flexible seal extends axially between a first mounting segment and a second mounting segment. The first mounting segment is connected axially between the mounting bracket and the support bracket, and includes a plurality of mounting apertures that extend axially through the first mounting segment. Each of the mounting spacers is arranged within a respective one of the mounting apertures, and extends axially between the mounting bracket and the support bracket.

Timothy Dale Photo 3

Axial Non-C0Ntact Seal

US Patent:
2013025, Oct 3, 2013
Filed:
Apr 2, 2012
Appl. No.:
13/437058
Inventors:
Timothy Dale - Manchester CT, US
International Classification:
F04D 29/08
US Classification:
4151701
Abstract:
A gas turbine engine has a turbine section and an air moving section upstream of the turbine section. A seal is between a static surface and a rotating surface in at least one of the turbine section and air moving section. The seal includes a seal shoe which is biased at least in part by a spring force, with the spring force created by cuts formed to provide a gap to allow arms associated with the seal to provide the spring force. The movement of the shoe is along a direction having at least a component parallel to an axis of rotation of the gas turbine engine. In addition, an axially moving non-contact seal is claimed.

Timothy Dale Photo 4

Turbine Engine Support Assembly Including Self Anti-Rotating Bushing

US Patent:
2014005, Feb 27, 2014
Filed:
Aug 23, 2012
Appl. No.:
13/592391
Inventors:
Meggan Harris - Colchester CT, US
Jorge I. Farah - Hartford CT, US
Christopher Treat - Manchester CT, US
Timothy Dale - Manchester CT, US
International Classification:
F04D 29/52, B23P 11/00, F16B 39/28
US Classification:
4152141, 411166, 2988922
Abstract:
A turbine engine includes multiple tierod supports. Each of the tierod supports is connected to an inner frame case of the turbine engine via multiple fasteners and at least one self anti-rotating bushing component.

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