MICHAEL PATRICK GARRY
Pilots at James Ave, Rockford, IL

License number
Illinois A2352989
Issued Date
Aug 2016
Expiration Date
Aug 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
525 James Ave, Rockford, IL 61107

Personal information

See more information about MICHAEL PATRICK GARRY at radaris.com
Name
Address
Phone
Michael Garry
525 James Ave, Rockford, IL 61107
(815) 210-5975
Michael Garry
682 Bent Ridge Ln, Barrington, IL 60010
(217) 561-5600
Michael Garry
1911 Overdene Ave, Rockford, IL 61103
(773) 963-9860
Michael Garry
1656 Durham Dr, Palatine, IL 60067
(847) 533-8851
Michael Garry
1708 Charles St, Rockford, IL 61104

Professional information

Michael Garry Photo 1

Integral Plus Proportional Dual Pump Switching System

US Patent:
2012004, Feb 23, 2012
Filed:
Aug 23, 2010
Appl. No.:
12/860971
Inventors:
Michael P. Garry - Rockford IL, US
Assignee:
WOODWARD GOVERNOR COMPANY - Fort Collins CO
International Classification:
F04B 49/035
US Classification:
417302, 417304
Abstract:
A dual-pump fluid distribution system that includes a first pump having an inlet and an outlet, and configured to supply a first flow of fluid, and a second pump having an inlet and an outlet, and configured to supply a second flow of fluid. In an embodiment, a bypass flow valve with a four-way hydraulic bridge is configured to initiate the switch between single-pump mode and dual-pump mode based on fluid flow demand. The bypass flow valve is configured such that the position of the bypass flow valve member relative to the four-way hydraulic bridge operates a pump selector valve. In an embodiment, the pump selector valve has a valve member, a biasing element, and a pressure switching port, and is configured such that the position of the valve member determines whether the second flow of fluid is combined with the first flow of fluid.


Michael Garry Photo 2

Staged Cooling Flow Nozzle Valve

US Patent:
2013004, Feb 21, 2013
Filed:
Aug 17, 2012
Appl. No.:
13/588355
Inventors:
Brett Jay Snodgrass - Byron IL, US
Charlie Carson - Grand Rapids MI, US
Carthel C. Baker - Oregon IL, US
Michael P. Garry - Rockford IL, US
Assignee:
Woodward, Inc. - Fort Collins CO
International Classification:
B05B 1/30
US Classification:
239574
Abstract:
A fuel split control arrangement is provided. The arrangement includes a staged cooling flow control valve and cooling check valve. The staged cooling flow control valve and cooling check valve is connected between the primary and secondary tips of a nozzle in a turbine engine. The staged cooling flow control valve and cooling check valve includes a valve member arrangement operable to prevent fuel flow from the secondary fuel supply manifold to the secondary tip and simultaneously allow fuel flow from the secondary fuel supply manifold to the primary tip such that the primary tip receives fuel flow from both the secondary fuel supply manifold and the primary fuel supply manifold.


Michael Garry Photo 3

Split Control Unit

US Patent:
2013004, Feb 21, 2013
Filed:
Aug 17, 2012
Appl. No.:
13/588767
Inventors:
Brett Jay Snodgrass - Byron IL, US
Charlie Carson - Grand Rapids MI, US
Carthel C. Baker - Oregon IL, US
Michael P. Garry - Rockford IL, US
Assignee:
Woodward, Inc. - Fort Collins CO
International Classification:
F16K 11/00
US Classification:
137 1, 137861
Abstract:
A split control unit in a distributed flow unit includes a flow inlet configured to receive a fuel flow, a first manifold having flow lines to supply fuel to one or more primary nozzles, and a second manifold having flow lines to supply fuel to one or more secondary nozzles. In an embodiment, the second manifold is in fluid communication with the flow inlet. A metering valve has a first port in fluid communication with the flow inlet and with the second manifold. The metering valve is configured to supply a metered fuel flow to the first manifold. A flow passage is in fluid communication with, and runs between, a flow line of the first manifold and a flow line of the second manifold to allow for a continuous cooling flow in the second manifold when all of the one or more secondary nozzles are closed.