Abstract: A synchronizing ring assembly includes a synchronizing ring portion that has a first and a second distal end, the first and the second distal end each form an integrated surge bumper.
Type:
Application
Filed:
September 5, 2019
Publication date:
March 11, 2021
Applicant:
United Technologies Corporation
Inventors:
William S. Pratt, Ryan M. Stanley, Adam Hart
Abstract: A diffuser for an oil drainback system drain tube includes a flow chamber configured for attachment to an open end of a drain tube, wherein the flow chamber has a side wall and an end wall, and openings in at least the side wall.
Type:
Application
Filed:
September 17, 2019
Publication date:
March 11, 2021
Applicant:
United Technologies Corporation
Inventors:
Andrew V. Schwendenmann, Francis Parnin, Matthew Gomes
Abstract: The present disclosure provides methods and systems for the characterization of a potential microtexture region (MTR) of a sample, component, or the like. The methods may include determining a threshold width of spatial correlation coefficient and/or a threshold spatial correlation coefficient slope for an actual MTR, characterizing a potential MTR as an actual MTR or a defect, characterizing an actual MTR as an acceptable MTR or not, and/or characterizing various components with potential MTRs as defective or not. The characterization may include calculating a width of spatial correlation coefficient and/or a spatial correlation coefficient slope of the potential MTR and comparing the width of spatial correlation coefficient to a threshold width of spatial correlation coefficient and/or comparing the spatial correlation coefficient slope to a threshold spatial correlation coefficient slope for the potential MTR to be characterized as an actual MTR or a defect (crack).
Abstract: The present disclosure provides methods and systems for the characterization of a microtexture of a sample, component, or the like. The methods may include methods of determining a service life limiting region of a component, determining a treatment method for a component, and/or selecting components from a batch of components for use in production. The characterization may include calculating a microtexture level indicator from ultrasonic C-scan images for various samples, regions, components, or the like. The microtexture level indicator may include at least one of an average peak factor, a standard deviation of peak amplitude, and/or a baseband bandwidth.
Abstract: A seal assembly for a gas turbine engine, having a seal formed of a carbon material; and a seal seat positioned for rotation relative to the seal, wherein the seal and the seal seat each have a sealing surface which together define a sliding seal, and wherein at least the sealing surface of the seal seat is made of the same carbon material as the sealing surface of the seal.
Abstract: A process of forming a shaped cooling passage in an article comprising positioning the article within a laser drilling apparatus; laser ablating a near net-shaped cooling passage having a meter section and a diffuser section; forming a re-recast on an interior wall of said cooling passage in both the meter section and the diffuser section; positioning the article within an electric discharge machining apparatus; and electric discharge machining said re-cast from said interior wall at both the meter section and diffusor section with the same electric discharge machine electrode to form a finished shaped cooling passage.
Abstract: A filtration system is disclosed. In various embodiments, the filtration system includes a fine mesh filter configured for disposition within a chamber and defining a first volume, the first volume in fluid communication with a main exit conduit; and a coarse mesh filter configured for disposition within the chamber and at least partially surrounding the fine mesh filter, the coarse mesh filter and the fine mesh filter defining a second volume, the second volume in fluid communication with a first bypass valve, the coarse mesh filter and the chamber defining a third volume, the third volume in fluid communication with a second bypass valve.
Abstract: A gas turbine engine is disclosed. In various embodiments, the gas turbine engine includes a low speed spool; a first compressor, a turbine and a generator rotationally coupled via the low speed spool; a high speed spool; and a second compressor and a motor rotationally coupled via the high speed spool.
Type:
Application
Filed:
August 20, 2019
Publication date:
February 25, 2021
Applicant:
UNITED TECHNOLOGIES CORPORATION
Inventors:
Daniel Bernard Kupratis, Paul R. Hanrahan
Abstract: A composite laminate comprising a substrate having a hot side and a cold side opposite said hot side; a thermal barrier coating coupled to said hot side of said substrate; and a reflective coating disposed on said thermal barrier coating.
Type:
Application
Filed:
August 20, 2019
Publication date:
February 25, 2021
Applicant:
United Technologies Corporation
Inventors:
Scott Alan Eastman, Justin B. Alms, Xuemei Wang
Abstract: A component includes a diffusion coating comprising an inter-diffusion zone between the diffusion coating and a substrate and a non-metallic inclusions zone adjacent to an outer surface of the diffusion coating. A method of coating a component includes applying an aluminizing slurry to a localized area of a component and applying a chromizing slurry to the localized area of the component subsequent to heat treating the aluminizing slurry.
Abstract: A method of distributing power within a gas turbine engine is disclosed. In various embodiments, the method includes driving a high pressure turbine having a first stage and a second stage with an exhaust stream from a combustor, the first stage connected to a high pressure turbine first stage spool and the second stage connected to a high pressure turbine second stage spool; driving a high pressure compressor connected to a high pressure compressor spool via a differential system, the differential system having a first stage input gear connected to the high pressure turbine first stage spool, a second stage input gear connected to the high pressure turbine second stage spool and an output gear assembly connected to the high pressure compressor spool; and selectively applying an auxiliary input power into at least one of the high pressure compressor spool and the high pressure turbine.
Type:
Application
Filed:
October 18, 2019
Publication date:
February 25, 2021
Applicant:
UNITED TECHNOLOGIES CORPORATION
Inventors:
Daniel Bernard Kupratis, Paul R. Hanrahan, Arthur M. Salve, JR.
Abstract: A guide plate for a swirler assembly is disclosed. In various embodiments, the guide plate includes a guide plate flange configured for engagement with a swirler body having a swirler inlet; and a guide plate collar, the guide plate collar having an aft protrusion with respect to an axial direction extending through the swirler body, the aft protrusion having an aft protrusion tip position configured to be equal to or extend downstream of a swirler inlet forward position with respect to the axial direction and a radially outer surface that forms a radially outer surface angle greater than ninety degrees with respect to a radial direction.
Abstract: An external turning vane includes a vane body extending radially from the inner cowl and disposed upstream from an inlet of the secondary flow system, the vane body configured to turn an airflow in a bypass flow path towards an axial direction to minimize separation between the airflow and the secondary flow system.
Abstract: A compliant jumper tube fitting assembly may comprise an outer housing comprising a first annular cylindrical structure including a first opening defined by a base wall, and an inner housing comprising a second annular cylindrical structure including a second opening defined by an annular wall, wherein the inner housing is configured to generate a seal between an inner diameter wall of the outer housing and an outer diameter wall of the inner housing in response to inserting the inner housing into a mouth end of the outer housing, wherein the inner housing is configured to receive an end fitting and generate a seal between an inner diameter wall of the inner housing in response to inserting the end fitting into the inner housing.
Abstract: A rotor blade for a rotary wing aircraft and a tip for the rotor blade. The rotor blade includes a blade root, a blade tip and a blade body that extends from the blade root to the blade tip. The blade tip includes: a continuously swept leading edge, a compound trailing edge, and a continuous anhedral.
Type:
Grant
Filed:
March 9, 2018
Date of Patent:
January 26, 2021
Assignees:
SIKORSKY AIRCRAFT CORPORATION, UNITED TECHNOLOGIES CORPORATION
Inventors:
Daniel Caleb Sargent, Timothy James Conti, Brian E. Wake, Byung-Young Min, Blake Almy Moffitt, Joseph Pantalone, III
Abstract: A method of additively-manufacturing a flexible sensor system having a lattice topology includes a number of electrical interconnects, each having one or more electrically-conductive layers alternately sandwiched between two or more dielectric layers, and two or more sensors defining a sensor array, each sensor located at an intersection of and electrically connected to the interconnects on the lattice topology and electrically-connected to the interconnects. Each of the electrically-conductive layers includes a cured material base and silver, copper, aluminum, gold, platinum, ruthenium, carbon, and/or alloys thereof, and each of the dielectric layers includes a cured material base. The additively-manufactured flexible sensor system is configured to be installed on the surface of an asset for the monitoring of that asset.
Type:
Grant
Filed:
February 4, 2019
Date of Patent:
January 26, 2021
Assignee:
United Technologies Corporation
Inventors:
Sameh Dardona, Dustin D. Caldwell, Callum Bailey
Abstract: A method for inspecting a component made using an additive manufacturing process, the component having an internal conduit, is disclosed. In various embodiments, the method includes the steps of: attaching a fluid-blocking header to the component, the fluid-blocking header having an internal conformal surface configured to mate with an external conformal surface of the component; introducing a plugging media into the internal conduit; activating the fluid-blocking header to freeze the plugging media in a vicinity of the fluid-blocking header; pressurizing the internal conduit of the component; and analyzing a fluid flow characteristic at an outlet of the component to assess an occurrence of a blockage within the internal conduit.
Abstract: A rotor has a rotor body having: a flange with a circumferential array of discontiguous apertures; and a surface spaced apart from the flange. One or more rotor balance weight assemblies each have a weight and a fastener. The weight has: a passageway having a first end and a second end; an internal thread along the passageway; and a boss at the first end of the passageway. The boss is in a respective one of the apertures. The fastener has: a shank having a first end and a second end and an external thread engaged to the passageway internal thread; an engagement feature at the shank first end for engagement by a tool to turn the fastener; and a head at the second end contacts the surface.
Abstract: A multi-angle multi-wave array may comprise a first set of sensing elements, a second set of sensing elements, and a third set of sensing elements wherein the first set of sensing elements, the second set of sensing elements, and the third set of sensing elements are collectively configured to detect and discriminate between categories of foreign object debris including solid objects and particulates including silicate sand, water vapor, dust, volcanic ash, and smoke.
Type:
Application
Filed:
July 3, 2019
Publication date:
January 7, 2021
Applicant:
UNITED TECHNOLOGIES CORPORATION
Inventors:
David L Lincoln, Wayde R. Schmidt, Michael J. Birnkrant, Michael T. Gorski, Jonathan Gilson, Xuemei Wang, Coy Bruce Wood
Abstract: A tool system to install an interference fit component within a bore of a component, includes a guide bushing that at least partially fits within a bore of a component. A drive screw is of a length to extend through the guide bushing and the bore. A threaded insert is receivable at least partially within the bore, the threaded insert receivable at least partially within the interference fit component.