James Kevin Mount - Cincinnati OH, US Richard Walker Nicholson - Cincinnati OH, US Duane Howard Anstead - Fairfield OH, US Robert Proctor - West Chester OH, US Pradeep Hemant Sangli - Bangalore, IN Prasad Laxman Kane - Pune, IN Mark Leonard Hopper - West Chester OH, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
B05B 12/00
US Classification:
184 611, 138 89, 60 3908
Abstract:
The present invention provides an air-oil separator comprising a first region having a mixture of air and oil, a second region wherein separation of at least some of the oil from the air-oil mixture occurs and at least one multi-directional injector plug located on a rotating component in flow communication with the first region and the second region, the multi-directional injector plug having a discharge head that is oriented such that at least a part of the air-oil mixture discharged therefrom has a component of velocity that is tangential to the direction of rotation of the rotating component.
James Kevin Mount - Cincinnati OH, US Richard Walker Nicholson - Cincinnati OH, US Duane Howard Anstead - Fairfield OH, US Robert Proctor - West Chester OH, US Pradeep Hemant Sangli - Bangalore, IN Prasad Laxman Kane - Pune, IN Mark Leonard Hopper - West Chester OH, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F16L 55/10
US Classification:
138 89, 138 90
Abstract:
The present invention provides an air-oil separator comprising a first region having a mixture of air and oil, a second region wherein separation of at least some of the oil from the air-oil mixture occurs and at least one multi-directional injector plug located on a rotating component in flow communication with the first region and the second region, the multi-directional injector plug having a discharge head that is oriented such that at least a part of the air-oil mixture discharged therefrom has a component of velocity that is tangential to the direction of rotation of the rotating component.
Kenneth Lee Fisher - Blue Ash OH, US Richard Walker Nicholson - Cincinnati OH, US Mark Hopper - West Chester OH, US Gary Paul Moscarino - Cincinnati OH, US Steven Alan Ross - Cincinnati OH, US Michael Slusher - Hamilton OH, US
International Classification:
F16C 33/41 F16C 33/38
US Classification:
384531, 384523
Abstract:
A bearing retainer having an inner portion, an outer portion spaced apart from said inner portion, and an intermediate portion connecting the inner portion and the outer portion, such that the inner portion and the outer portion are radially spaced apart and define a space therebetween, and a contact surface on at least one of the inner portion and the outer portion for engaging a component of a bearing assembly disposed in the space.
Duane H. Anstead - Fairfield OH, US Mark E. Zentgraf - Cincinnati OH, US Daniel Clautice - Mason OH, US Charles R. Granitz - Loveland OH, US Joshua D. Smith - Cincinnati OH, US Mark Hopper - West Chester OH, US
International Classification:
B65B 3/04 B65D 47/00 F16K 24/00
US Classification:
141326, 137587, 220 861
Abstract:
An apparatus for filling an oil tank may include one or more valves that may be arranged and/or sized in such a way as to assist in venting the oil tank during a fill operation and assure that the tank may be filled within a reasonable time.
Mark Leonard Hopper - West Chester OH, US Joshua Dean Smith - Cincinnati OH, US
International Classification:
F16F 9/14 F16F 15/16
US Classification:
188297
Abstract:
An annular dashpot damper is utilized to provide flow resistance from viscous shear to an orifice or gap which provides flow metering. This is accomplished by dividing the flow channel into circumferential segments or damping cavities which are sealed and limit rotational flow of the fluid.
Gas Turbine Engine With An Engine Rotor Element Turning Device
- Schenectady NY, US Raymond Floyd Martell - Wyoming OH, US Mark Leonard Hopper - West Chester OH, US Scott Douglas Waun - Loveland OH, US
International Classification:
F02C 6/18 F02C 3/04 F02C 7/36
Abstract:
A turbine engine has a core with a compressor, combustor, and turbine sections in axial flow arrangement and with corresponding rotating elements mounted to a shaft defining engine rotor elements. The turbine engine has a rotary driver operably coupled to the engine rotor elements. The turbine engine has at least one thermoelectric generator in thermal communication with the core and in electrical communication with the rotary driver to provide power to the rotary driver to turn the engine rotor elements.
Aspirating Face Seal Starter Tooth Abradable Pocket
- Schenectady NY, US John David Bibler - Kings Mills OH, US Mark Leonard Hopper - West Chester OH, US
International Classification:
F01D 11/12 F01D 11/02 F04D 29/08
Abstract:
Aspirating face seal between high and low pressure regions of turbomachine between rotatable and non-rotatable members of turbomachine includes gas bearing rotatable and non-rotatable face surfaces, starter tooth mounted on the rotatable member operable to sealingly engage abradable starter seal land on the non-rotatable member, and annular pocket in an abradable coating or other abradable material of starter seal land. Abradable material may be in radially inwardly facing groove extending into non-rotatable member. Pocket may extend radially outwardly from a cylindrical radially outer abradable surface to pocket bottom which includes thin abradable material layer groove surface along the non-rotatable member. Pocket may extend axially aftwardly from annular forward groove side surface into abradable coating. Pocket may be bounded axially by abradable material. Pocket may be tapered having taper decreasing axially aftwardly away from annular forward groove side surface.
Bearing Outer Race Retention During High Load Events
- Schenectady NY, US Shivakumar Basavanna - Mullur, IN Jacob Patrick Miller - Blue Ash OH, US Charles Andrew Corman - Milford OH, US Mark Leonard Hopper - West Chester OH, US
A housing for retention of the outer race of a bearing of a gas turbine engine includes an arrangement of spring fingers that yields a lightweight housing capable of withstanding very high radial loads combined with very high torsional windup and axial thrust load. Controlled circumferential gaps on both sides of each spring finger limit the deflection and self-arrest the distortion of the housing. The spring fingers define at least one side edge that extends at an angle relative to the axial direction. An axial gap is created on the aft end by a portion of the spring finger beam structure that opposes an axial face of the housing and limits the axial distortion. A radial gap created between interface hardware of the housing and the inner retention housing also acts to retain the spring finger housing under load in a radial direction.