Hsin-Tuan Liu - West Chester OH Brent Franklin Beacher - Hamilton OH Bryan Keith Doloresco - Cincinnati OH Gregory Todd Steinmetz - Cincinnati OH Kenneth William Krabacher - Hamilton OH
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 904
US Classification:
416228, 416235, 416243
Abstract:
A compressor stator includes an outer casing supporting a row of stator vanes extending radially inwardly therefrom. Each vane includes pressure and suction sides extending axially between leading and trailing edges and radially between a root and a tip. The root and tip are twisted relative to a pitch section disposed therebetween. Each vane tip is radially convex adjacent a leading edge for defining an axially concave outer flowpath in the casing for reducing peak velocity of airflow for enhanced efficiency.
Robert Proctor - West Chester OH Julius John Montgomery - Mason OH Michael Jay Epstein - Mason OH Roger Owen Barbe - Montgomery OH Hai Buu Sam - Hamilton OH James Bernar Ogzewalla - Maysville KY Andrew David Kemp - Loveland OH Bryan Keith Doloresco - Cincinnati OH
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 608
US Classification:
60785, 415144
Abstract:
A gas turbine engine includes a compressor including a casing and a stator assembly. The casing extends around the stator assembly, the stator assembly including a plurality of stator vanes, and a plurality of bleed scoops. Adjacent stator vanes define a static high-pressure region, the bleed scoops formed at least partially within the high pressure region.
Bryan Keith Doloresco - Cincinnati OH, US Peter John Wood - Loveland OH, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D005/14
US Classification:
416238, 416223 A, 416DIG 2, 416242, 416243
Abstract:
A compressor airfoil includes opposite pressure and suction sides joined together at leading and trailing edges and extending in span between a root and tip. The airfoil includes stagger increasing above the root and decreasing above a midspan pitch section thereof.
Hsin-Tuan Liu - West Chester OH Robert B. Dickman - Cincinnati OH Kenneth W. Krabacher - Hamilton OH Gregory T. Steinmetz - Cincinnati OH Brent F. Beacher - Hamilton OH Bryan K. Doloresco - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 514
US Classification:
416238
Abstract:
A compressor airfoil includes pressure and suction sides extending from root to tip and between leading and trailing edges. Transverse sections have respective chords and camber lines. Centers of gravity of the sections are aligned along a double bowed stacking axis for improving performance.
Bryan Doloresco <c:out value="1981" />graduate of Northwest High School in Cincinnati, OH is on Classmates.com. See pictures, plan your class reunion and get caught up with Bryan ...