Abstract: A system for selecting components for an engine includes an electronic control unit comprising a processor and a memory component and a machine-readable instruction set. The machine-readable instruction set is stored in the memory component of the electronic control unit and causes the system to perform at least the following when executed by the processor: receive a catalog of a plurality of components, where the plurality of components include a measured manufacturing characteristic, receive at least one operating environment characteristic of a plurality of operating environment characteristics, and select one or more components from the catalog of the plurality of components for a bill of materials based on the measured manufacturing characteristic and the at least one operating environment characteristic.

Abstract: A gas turbine engine includes a combustion section space between a compressor section in a turbine section. The combustion section defines a combustion chamber and includes a combustor member defining an opening to the combustion chamber. A mounting assembly extends around or is positioned adjacent to the opening defined by the combustor member. In igniter extends through a ferrule of the mounting assembly and includes a distal end positioned proximate the opening in the combustor member. The igniter defines a plurality of channels each channel extending between a first end and a second end. The first end is positioned away from the distal end of the igniter relative to the second end, and the second end is a terminal end spaced from the distal end of the igniter.

Abstract: An analytics core and/or an analytics core associated with aggregation are presented. For example, a system includes a monitoring component, a catalog component, a model suite component, and a model processing/learning component. The monitoring component monitor and analyzed data associated with one or more assets. The catalog component manages analytics associated with the one or more assets, where the catalog component manages a set of models for the one or more assets. The model suite component selects a subset of models from the set of models. The model processing/learning component process the subset of models and performs learning associated with the subset of models to predict a health state for the one or more assets.

Abstract: A windage shield system is provided. The system includes an annular cavity having an inlet end and an outlet end. The annular cavity is configured to direct a flow of cooling fluid from the inlet end to the outlet end. The system also includes a source of a flow of cooling fluid coupled in flow communication with the annular cavity. The annular cavity is bounded by a stationary component and a rotating component, and the rotating component introduces heat into the annular cavity by windage effects. The system also includes a cooling channel coupled in flow communication with the outlet end, and a first windage shield extending from the outlet end towards the inlet end within the annular cavity.

Abstract: A compressor for a gas turbine engine includes a stator and a rotor. The stator includes first and second stator vanes attached to first and second vane platforms, respectively. The rotor includes a plurality of rotor blades that rotate with respect to the stator. An inner stator casing supports the first and second vane platforms and encloses the stator and the rotor. An outer stator casing encloses the inner stator casing, and a bleed cavity is disposed therebetween. At least one diffuser is disposed between the first vane platform and the second vane platform, and is configured to allow air communication between the inner stator casing and the bleed cavity. An exit opening of the diffuser is disposed within the bleed cavity at a location separate from the inner stator casing and the outer stator casing.

Abstract: A clearance control apparatus for a gas turbine engine including an annular turbine case having opposed inner and outer surfaces; an annular manifold surrounding a portion of the turbine case, the manifold including: an inlet port in fluid communication with the manifold and the outer surface of the turbine case, and an exit port; and a bypass pipe having an upstream end coupled to the exit port, a downstream end coupled to a low-pressure sink, and a valve disposed between upstream and downstream ends, the valve selectively moveable between a first position which blocks flow between the upstream and downstream ends, and a second position which permits flow between the upstream and downstream ends.

Abstract: A compressor for a gas turbine engine includes a stator and a rotor. The stator includes first and second stator vanes attached to first and second vane platforms, respectively. The rotor includes a plurality of rotor blades that rotate with respect to the stator. An inner stator casing supports the first and second vane platforms and encloses the stator and the rotor. An outer stator casing encloses the inner stator casing, and a bleed cavity is disposed therebetween. At least one diffuser is disposed between the first vane platform and the second vane platform, and is configured to allow air communication between the inner stator casing and the bleed cavity. An exit opening of the diffuser is disposed within the bleed cavity at a location separate from the inner stator casing and the outer stator casing.

Abstract: A gas turbine engine includes a combustion section space between a compressor section in a turbine section. The combustion section defines a combustion chamber and includes a combustor member defining an opening to the combustion chamber. A mounting assembly extends around or is positioned adjacent to the opening defined by the combustor member. In igniter extends through a ferrule of the mounting assembly and includes a distal end positioned proximate the opening in the combustor member. The igniter defines a plurality of channels each channel extending between a first end and a second end. The first end is positioned away from the distal end of the igniter relative to the second end, and the second end is a terminal end spaced from the distal end of the igniter.

Abstract: A windage shield system is provided. The system includes an annular cavity having an inlet end and an outlet end. The annular cavity is configured to direct a flow of cooling fluid from the inlet end to the outlet end. The system also includes a source of a flow of cooling fluid coupled in flow communication with the annular cavity. The annular cavity is bounded by a stationary component and a rotating component, and the rotating component introduces heat into the annular cavity by windage effects. The system also includes a cooling channel coupled in flow communication with the outlet end, and a first windage shield extending from the outlet end towards the inlet end within the annular cavity.

Abstract: Embodiments for generating programming code by a processor are described. A plurality of shapes are displayed on a display device. Each of the plurality of shapes is associated with a respective functionality of programming code. User input is received. Based on the user input, the plurality of shapes are arranged on the display device. Based on said arrangement of the plurality of shapes, programming code is generated. A total functionality of the generated programming code includes the respective functionality of programming code associated with each of the plurality of shapes.

Abstract: A bottle cap removing cutlery is disclosed herein. The bottle cap removing cutlery comprises a main body, a cutlery member, a bottle cap opener. The cutlery member is preferably a knife, spoon, fork or like utensil. The bottle cap opener comprises a fulcrum portion, a lifting portion and an opener cutout.

Abstract: Louver systems for gas turbine bleed air systems are disclosed. An example louver system may include a bleed system discharge opening arranged to vent bleed air from a bleed flow conduit and a plurality of pivotable louvers disposed proximate the discharge opening, the pivotable louvers being pivotable between a shut position and an open position. In the shut position, individual louvers may at least partially obstruct the discharge opening. In the open position, individual louvers may at least partially control a direction of flow of the bleed air exiting the discharge opening.

Abstract: A spinal decompression machine includes a portable frame, a user support element, a laterally positioned handle extending from the frame, and a drive mechanism operatively coupled to the handle. A force bar operatively coupled to the drive mechanism extends longitudinally beyond a longitudinal end of the frame. A harness is attached to the first force bar. The drive mechanism causes the force bar to move longitudinally upon rotation of the handle. A method of providing traction includes positioning a person in a face up position upon the user support element, attaching a harness to a neck or pelvis of the person, the harness attached to a cervical traction bar or a pelvic traction bar, and moving the cervical fraction bar and pelvic fraction bar simultaneously in a common longitudinal direction by moving a handle.

Abstract: A clearance control apparatus for a gas turbine engine including an annular turbine case having opposed inner and outer surfaces; an annular manifold surrounding a portion of the turbine case, the manifold including: an inlet port in fluid communication with the manifold and the outer surface of the turbine case, and an exit port; and a bypass pipe having an upstream end coupled to the exit port, a downstream end coupled to a low-pressure sink, and a valve disposed between upstream and downstream ends, the valve selectively moveable between a first position which blocks flow between the upstream and downstream ends, and a second position which permits flow between the upstream and downstream ends.

Abstract: A spinal decompression machine includes a portable frame, a user support element, a laterally positioned handle extending from the frame, and a drive mechanism operatively coupled to the handle. A force bar operatively coupled to the drive mechanism extends longitudinally beyond a longitudinal end of the frame. A harness is attached to the first force bar. The drive mechanism causes the force bar to move longitudinally upon rotation of the handle. A method of providing traction includes positioning a person in a face up position upon the user support element, attaching a harness to a neck or pelvis of the person, the harness attached to a cervical traction bar or a pelvic traction bar, and moving the cervical fraction bar and pelvic fraction bar simultaneously in a common longitudinal direction by moving a handle.

Abstract: A crane assembly for lifting marine vessels is provided. The assembly includes a sleeve having first and second clamps extending therefrom that are configured for engaging with a pylon of a dock and a boom pole slideably and rotatably received within the sleeve. A winch assembly is carried by the boom pole and including a winch and a cord. A crossbar is provided that has a main support that receives the cord and that has a pair of adjustable supports being carried along a length thereof that are adjustable to vary the space between the pair of adjustable supports. The adjustable supports are configured for engaging a support strap that is configured for passing beneath the marine vessel.

Abstract: System and methods configured to permit a user such as a health care provider to organize and manage patient information quickly and efficiently from a simplified representation. Such simplified representations may include a patient representation and a context representation. The representations may be updated to represent real-time patient conditions through the input of information directly from treatment or monitoring devices or from user input.