1
Elliot Matel Elliot Matel
Feist Jeffrey P, Matel Elliot, Nagel Matthew J: Exhaust deflector for a muffler. Briggs And Stratton Corporation, Feist Jeffrey P, Matel Elliot, Nagel Matthew J, LASKA Casimir F, December 21, 2007: WO/2007/146770

An exhaust deflector (200) is attachable to a muffler. The exhaust deflector includes a single-piece housing (205) having a flange (225) that defines an inlet aperture (230), an outlet wall (245) that defines an outlet aperture (255), and an intermediate wall (266) that interconnects the flange and ...


2
Dr Raj C Thiagarajan ATOA Scientific Technologies Dr Raj C Thiagarajan ATOA Scientific Technologies
Hayagreeva Rao K V, Prashant Shukla, Adi Narayana Namburi, Chinniah Thiagarajan: Steam turbine exhaust hood and method of fabricating the same. General Electric Company, Armstrong Teasdale, August 31, 2010: US07785068 (1 worldwide citation)

A method of fabricating an exhaust hood is provided for use with a turbine engine. The method includes providing an upper shell casing wherein the upper shell casing is fabricated from a composite material, and coupling the upper shell casing to a lower shell casing such that a turbine is housed wit ...


3
Dr Raj C Thiagarajan ATOA Scientific Technologies Dr Raj C Thiagarajan ATOA Scientific Technologies
Namburi Adi Narayana, Rao Hayagreeva, Thiagarajan Chinniah: Verbundmaterial für turbinen-tragestruktur. Gen Electric, December 5, 2008: FR2916675-A1

Ein Verbundmaterial (10) zum Einsatz in Turbinen-Tragestrukturen (35). Das Verbundmaterial (10) kann ein erstes Material (11) mit einem positiven Koeffizienten der thermischen Ausdehnung und ein zweites Material (12) mit einem negativen Koeffizienten der thermischen Ausdehnung, einem negativen Poiss ...


4
Dr Raj C Thiagarajan ATOA Scientific Technologies Dr Raj C Thiagarajan ATOA Scientific Technologies
Rao Kv Hayagreeva, Shukla Prashant, Namburi Adi Narayana, Thiagarajan Chinniah: Dampfturbinenauslasshaube und verfahren zur herstellung derselben. Gen Electric, November 21, 2008: FR2916224-A1

Es wird eine Turbinenabdampfhaube geschaffen. Die Turbinen-Abdampfhaube umfasst eine Gehäuseschale (150), die so bemessen ist, dass eine Turbine (32) darin zumindest partiell untergebracht ist. Die Gehäuseschale ist aus einem Verbundmaterial hergestellt.


5
Craig Allen
Craig Allen Bielek, Thanh Vo, Frederick James Brunner: Second-stage turbine nozzle airfoil. General Electric Company, Nixon & Vanderhye, January 7, 2003: US06503054 (51 worldwide citation)

The second-stage nozzles have vanes comprising airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I with the X, Y and Z values commencing at the radially innermost aerodynamic section of the airfoil and then made relative to that ...


6
Craig Allen
Robert Alan Brittingham, Edward Durell Benjamin, Jacob Charles Perry II, Craig Allen Bielek: Airfoil shape for a turbine bucket. General Electric Company, Nixon & Vanderhye, August 24, 2004: US06779980 (40 worldwide citation)

First stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z values ...


7
Craig Allen
Craig Allen Bielek, Robert Alan Brittingham, Jeff Brian Thompson, Benjamin Arnette Lagrange, Robert Walter Coign: Airfoil shape for a turbine bucket. General Electric Company, Nixon & Vanderhye, May 25, 2004: US06739838 (37 worldwide citation)

Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z values ...


8
Craig Allen
Curtis John Jacks, Craig Allen Bielek, Robert Walter Coign, Randall Gill: First stage turbine nozzle airfoil. General Electric Company, Sutherland Asbill & Brennan, May 18, 2004: US06736599 (37 worldwide citation)

The first stage nozzles have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table 1. The X and Y values are in inches and the Z value is non-dimensional along the nozzle-stacking axis coincident with a turbine radius and convertible to a Z dista ...


9
Craig Allen
David John Humanchuk, Craig Allen Bielek, Robert Alan Brittingham, James Tyson Balkcum, Andrew Jones Jr: Second stage turbine bucket airfoil. General Electric Company, Nixon & Vanderhye, February 3, 2004: US06685434 (37 worldwide citation)

The second stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z value is non-dimensional along the bucket centerline coincident with a turbine radius and convertible to a Z dist ...


10
Craig Allen
Jon Robert DeLong, Craig Allen Bielek, Tommy Dee Hayes, Benjamin Arnette Lagrange, Scott F Johnson: Airfoil shape for a turbine bucket and turbine incorporating same. General Electric Company, Nixon & Vanderhye PC, June 8, 2010: US07731483 (16 worldwide citation)

Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z′ set forth Table I wherein X and Y values are in inches and the Z′ values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z′ val ...



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