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US 8,894,365 B2Granted
Flowpath insert and assembly
AssigneeUnited Technologies Corporation
InventorDarren M. Smith
Life of this patent
Estimating the term…
Abstract
A flowpath assembly for a gas turbine engine includes a plurality of flowpath insert ducts arranged in a cascade configuration. Each flowpath duct includes a radially inward wall, a radially outward wall, a first side wall, and a second side wall. A flowpath volume is defined between the inward, outward, first side and second side walls. The first side wall of a given one of the plurality of flowpath insert ducts is positioned adjacent to the second sidewall of an adjacent one of the plurality of flowpath insert ducts in the cascade configuration.
Claims12
A flowpath assembly for a gas turbine engine, the assembly comprising:
- a plurality of flowpath insert ducts arranged in a cascade configuration, each flowpath duct including:
- a radially inward wall;
- a radially outward wall;
- a first side wall;
- a second side wall, wherein a flowpath volume is defined between the inward, outward, first side and second side walls;
- and
- a plurality of outward-facing retention hooks located on each of the first and second side walls of each of the flowpath ducts,
- wherein the first side wall of a given one of the plurality of flowpath insert ducts is positioned adjacent to the second sidewall of an adjacent one of the plurality of flowpath insert ducts in the cascade configuration;
- and
- a plurality of housing cartridges configured to engage the opposed retention hooks of adjacent flowpath ducts to provide engagement therebetween, wherein each housing cartridge comprises:
- a body;
- a plurality of cutout notches defined in the body configured to accept the retention hooks of flowpath ducts;
- a threaded member;
- a movable member threadably engaged with the threaded member;
- a retention plate engaged with the movable member and positioned proximate a row of the plurality of cutout notches, wherein rotation of the threaded member produces translational movement of the movable member and the retention plate such that retention hooks of at least one of the flowpath ducts can be removably retained in the cutout notches by the retention plate.
12 more elements
A flowpath insert assembly for a gas turbine engine, the assembly comprising:
- a first part that includes a first side wall, a first portion of an inward wall, a first portion of an outward wall, and at least one substantially axially-extending first connection flange;
- a second part including a second side wall, a second portion of the inward wall, a second portion of the outward wall, and at least one substantially axially-extending second connection flange;
- a plurality of outward-facing retention hooks located on each of the first and second side walls;
- and
- a housing cartridge configured to engage the retention hooks of the first and second side walls, wherein the housing cartridge includes a threaded member and a retention plate, wherein rotation of the threaded member produces translational movement of the retention plate such that retention hooks of at least one of the first and second side walls can be removably retained relative to the housing cartridge by the retention plate,
- wherein the first part and the second part at attached together with fasteners secured to the first and second connection flanges such that the first and second portions of the inward wall adjoin each other and the first and second portions of the outward wall adjoin each other, and wherein a flowpath volume is defined between the inward, outward, first side and second side walls.
3 more elements
A flowpath insert assembly for a gas turbine engine, the assembly comprising:
- a side wall;
- an inward wall segment extending from the side wall;
- an outward wall segment extending from the side wall, wherein the side wall, the inward wall segment and the outward wall segment define a substantially U-shaped configuration;
- a substantially axially-extending connection flange having openings for fastener attachment, the connection flange located on one of the inward wall segment and the outward wall segment;
- a plurality of outward-facing retention hooks located on the side wall;
- and
- a housing cartridge configured to engage the retention hooks of the side wall, wherein the housing cartridge includes a threaded member and a retention plate, wherein rotation of the threaded member produces translational movement of the retention plate such that the retention hooks can be removably retained by the retention plate.
4 more elements
A flowpath assembly for a gas turbine engine, the assembly comprising:
- a plurality of flowpath insert ducts arranged in a cascade configuration, each flowpath duct including:
- a radially inward wall;
- a radially outward wall;
- a first side wall;
- a second side wall, wherein a flowpath volume is defined between the inward, outward, first side and second side walls;
- and
- a retention hook located on each of the flowpath ducts,
- wherein the first side wall of a given one of the plurality of flowpath insert ducts is positioned adjacent to the second sidewall of an adjacent one of the plurality of flowpath insert ducts in the cascade configuration;
- and
- a plurality of housing cartridges configured to engage the retention hooks of adjacent flowpath ducts to provide engagement therebetween, wherein each housing cartridge comprises:
- a body;
- a plurality of cutout notches defined in the body configured to accept the retention hooks of flowpath ducts;
- a threaded member;
- a retention plate positioned proximate at least one of the plurality of cutout notches, wherein rotation of the threaded member produces translational movement of the retention plate such that the retention hook of one of the flowpath ducts can be removably retained in a corresponding one of the cutout notches by the retention plate.
11 more elements
Dependencies are inferred from the claim text.