Jason L Burdette

US Patent:

20220282391, Sep 8, 2022

Filed:

Mar 4, 2021

Appl. No.:

17/192027

Inventors:

- Jacksonville FL, US
Dattu GV Jonnalagadda - Ponnur, IN
Michael Ralph Storage - Beavercreek OH, US
Emily Marie Phelps - Xenia OH, US
Jason Levi Burdette - Dayton OH, US

International Classification:

C25D 5/00
F28G 9/00
C25D 1/02
C25D 5/34
C25D 5/48

Abstract:

A method of electroforming can be used to prepare a heat exchanger by electroforming the heat exchanger on a mandrel having a smooth and conductive surface. The mandrel is in the shape of at least part of the heat exchanger, and is removed from the electroformed heat exchanger.

US Patent:

20210372547, Dec 2, 2021

Filed:

Aug 9, 2021

Appl. No.:

17/396908

Inventors:

- Jacksonville FL, US
Michael Thomas Kenworthy - Gilbert AZ, US
Dattu GV Jonnalagadda - Ponnur, IN
Jason L. Burdette - Beavercreek OH, US

International Classification:

F16L 27/02
F16L 27/08
F02C 7/00
F04D 27/00

Abstract:

A duct assembly may include a first duct, a second duct, and a flexible joint assembly coupling the first duct to the second duct. The flexible joint assembly may include a bellows having a first end and a second end and a plurality of convolutions located therebetween, and a gimbaled joint assembly. The gimbaled joint assembly may include a first support surrounding the first end of the bellows and a first portion of the plurality of convolutions, a second support surrounding the second end of the bellows and a second portion of the plurality of convolutions, and a gimbal ring assembly operably coupled to the first support and the second support. The gimbal ring assembly may include a ring body and a plurality of flexure hinges interconnected with the ring body.

US Patent:

20190195137, Jun 27, 2019

Filed:

Dec 21, 2017

Appl. No.:

15/850644

Inventors:

- Jacksonville FL, US
Jason Levi BURDETTE - Beavercreek OH, US
Derek Thomas DREISCHARF - Bellbrook OH, US

International Classification:

F02C 7/32
F02C 7/14
F04D 29/40
B64D 33/08
B64D 33/02

Abstract:

A surface cooler assembly includes at least one surface cooler comprising surface cooler hook rails extending circumferentially the length of the surface cooler and including axially extending and radially extending portions. The surface cooler assembly also includes at least one support bracket comprising bracket hook rails extending circumferentially the length of the support bracket and including axially extending and radially extending portions. The support bracket and surface cooler are contoured in a circumferential direction. Each of the surface cooler hook rails contacts a bracket hook rail.

US Patent:

20180320801, Nov 8, 2018

Filed:

May 2, 2017

Appl. No.:

15/584739

Inventors:

- Jacksonville FL, US
Daniel Dyer - Dayton OH, US
Armando Bringas - Querétaro, MX
Jason Levi Burdette - Beavercreek OH, US
Gordon Tajiri - Allentown PA, US
Dattu GV Jonnalagadda - Ponnur, IN
Michael Thomas Kenworthy - Gilbert AZ, US

International Classification:

F16L 9/00
B22F 5/00

Abstract:

A duct for a turbine engine, such as a gas turbine engine, can be utilized to carry a fluid from one portion of the engine to another. The duct can include a metallic tubular element having one of a varying wall thickness, a varying cross section, or a tight bend. Such a duct can be formed utilizing additive manufacturing or metal deposition on an additively manufactured mandrel.

US Patent:

20180245605, Aug 30, 2018

Filed:

Feb 28, 2017

Appl. No.:

15/445240

Inventors:

- Jacksonville FL, US
Jason Levi Burdette - Beavercreek OH, US
Walter Arthur Hundley - Enon OH, US
Bernard Albert Luschek - Lebanon OH, US

International Classification:

F04D 29/64
F04D 29/52
F04D 29/66
F04D 29/58

Abstract:

A turbine engine for an aircraft can includes a casing. The casing can be a fan casing surrounding a fan assembly for drawing air into the turbine engine. The fan casing can have a peripheral wall. A surface cooler can be provided in the turbine engine confronting the peripheral wall of the fan casing. The surface cooler can have a mounting bracket for mounting the surface cooler to the fan casing.

US Patent:

20180209569, Jul 26, 2018

Filed:

Jan 25, 2017

Appl. No.:

15/415083

Inventors:

- Jacksonville FL, US
Michael Thomas Kenworthy - Gilbert AZ, US
Dattu GV Jonnalagadda - Ponnur, IN
Jason Levi Burdette - Beavercreek OH, US

International Classification:

F16L 27/11
F02C 6/08

Abstract:

A flexible joint assembly for a joint between a first duct and a second duct for providing a flow of fluid, such as bleed air in an aviation implementation. The flexible joint includes a bellows supported by a mounting assembly having a first support and a second support, each surrounding a portion of the bellows. A set of rod assemblies can operably couple the first support and the second support.

US Patent:

20180209570, Jul 26, 2018

Filed:

Jan 25, 2017

Appl. No.:

15/415109

Inventors:

- Jacksonville FL, US
Michael Thomas Kenworthy - Gilbert AZ, US
Dattu GV Jonnalagadda - Ponnur, IN
Jason Levi Burdette - Beavercreek OH, US

International Classification:

F16L 27/111
F04D 27/00
F04D 29/54
F02C 9/18

Abstract:

A flexible joint assembly for a joint between a first duct and a second duct for providing a flow of fluid, such as bleed air in an aviation implementation. The flexible joint includes a bellows supported by a mounting assembly having a first support and a second support, provided within the interior of the bellows. A rod assembly can operably couple the first support and the second support.

US Patent:

20180202589, Jul 19, 2018

Filed:

Jan 13, 2017

Appl. No.:

15/406123

Inventors:

- Jacksonville FL, US
Michael Thomas Kenworthy - Gilbert AZ, US
Dattu GV Jonnalagadda - Ponnur, IN
Jason L. Burdette - Beavercreek OH, US

International Classification:

F16L 27/02
F04D 27/00

Abstract:

A flexible joint assembly for a joint between a first duct and a second duct for providing a flow of fluid, such as bleed air in an aviation implementation. The flexible joint includes a bellows supported by a mounting assembly having a first support and a second support, each surrounding a portion of the bellows. A set of flexures provided on a joint ring of the joint assemblies can operably couple the first support and the second support.