Elliot Matel 
Elliot MatelAn 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 ...
Dr Raj C Thiagarajan ATOA Scientific Technologies 
Dr Raj C Thiagarajan ATOA Scientific TechnologiesA 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 ...
Dr Raj C Thiagarajan ATOA Scientific Technologies Dr Raj C Thiagarajan ATOA Scientific TechnologiesEin 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 ...
Dr Raj C Thiagarajan ATOA Scientific Technologies Dr Raj C Thiagarajan ATOA Scientific TechnologiesEs 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.
Craig AllenThe 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 ...
Craig AllenFirst 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 ...
Craig AllenThe 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 ...
Craig AllenThird 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 ...
Craig AllenThe 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 ...
Craig AllenThird 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 ...
Click the thumbnails below to visualize the patent trend.
View Profile
