JEFFREY RYAN GRAVES
Pharmacy at Nott St, Schenectady, NY

License number
New York 059010-1
Category
Pharmacy
Type
Pharmacist
License number
New York 033.0101708
Category
Pharmacy
Type
Pharmacist
License number
New York 7000548-01701
Category
Pharmacy
Type
Pharmacist
Address
Address 2
461 Nott St, Schenectady, NY 12308
544 Lakeview Rd, Broadalbin, NY 12025
Phone
(518) 355-5000
(801) 803-1819

Personal information

See more information about JEFFREY RYAN GRAVES at radaris.com
Name
Address
Phone
Jeffrey Graves, age 45
439 Dick Rd, Depew, NY 14043
(716) 681-7056
Jeffrey Graves
52 Skyline Dr, Akron, NY 14001
(716) 472-3784
Jeffrey Graves, age 44
330 Elmendorf Dr, Hurley, NY 12443
(845) 331-2582
Jeffrey Graves, age 63
3617 James Dr, Endicott, NY 13760
(607) 437-3249
Jeffrey Graves, age 35
114 E 122Nd St APT 5F, New York, NY 10035

Professional information

See more information about JEFFREY RYAN GRAVES at trustoria.com
Jeffrey Graves Photo 1
Combustor For A Gas Turbine With Cooling Structure

Combustor For A Gas Turbine With Cooling Structure

US Patent:
5724816, Mar 10, 1998
Filed:
Apr 10, 1996
Appl. No.:
8/627807
Inventors:
Ann Melinda Ritter - Albany NY
Robert Patrick Campbell - Loudonville NY
Melvin Robert Jackson - Niskayuna NY
Ross Anthony McLean - Ballston Spa NY
Mitchell Reuben Cohen - Troy NY
Nesim Abuaf - Schenectady NY
Sanjay Marc Correa - Niskayuna NY
Lance Gordon Peterson - Ballston Spa NY
Myron Clyde Muth - West Charlton NY
Adrian Maurice Beltran - Ballston Spa NY
Constantinos Minas - Slingerlands NY
David Robert Schumacher - Scotia NY
Jeffrey Alan Graves - Niskayuna NY
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 100
US Classification:
60752
Abstract:
A combustor/transition piece for a gas turbine including a double walled structure having a plurality of cooling channels, both axially and, in some cases, circumferential cross-flow passages positioned between the structure's inner member and the outer member to provide cooling air thereto, are formed in the area between the inner member of the combustor and the outer member thereof. The passages preferably extend both axially and circumferentially with respect to the direction of flow through the combustor/transition piece. The axial passages extend completely from one end to the other and the circumferential passages extend around the circumference of the combustor/transition piece. The addition of a circumferential cross-flow passage connecting axial flow coolant passages in double wall turbine components can prevent combustor/transition piece part failure due to axial passage inlet blockage without affecting normal, unblocked cooling. Double wall cooling structures are constructed using two unbonded members.