초록 ▼

A nozzle and shroud for use in an air cycle machine has a plate and a shroud curving in a first axial direction about a center axis of the shroud relative to the plate. A plurality of vanes extends in a second axial direction away from the plate. The plurality of vanes extends for a height away from

A nozzle and shroud for use in an air cycle machine has a plate and a shroud curving in a first axial direction about a center axis of the shroud relative to the plate. A plurality of vanes extends in a second axial direction away from the plate. The plurality of vanes extends for a height away from the plate and a width defined as the closest distance between two adjacent vanes, with a ratio of the height to the width being between 1.7377 and 2.1612. An air cycle machine and a method of repair are also disclosed.

대표청구항 ▼

1. A nozzle and shroud for use in an air cycle machine comprising: a plate and a shroud curving in a first axial direction about a center axis of said shroud relative to said plate;a plurality of vanes extending in a second axial direction away from said plate, with said plurality of vanes extending

1. A nozzle and shroud for use in an air cycle machine comprising: a plate and a shroud curving in a first axial direction about a center axis of said shroud relative to said plate;a plurality of vanes extending in a second axial direction away from said plate, with said plurality of vanes extending for a height away from said plate and a width being defined as the closest distance between two adjacent vanes, with a ratio of said height to said width being between 1.7377 and 2.1612;wherein there are 19 circumferentially spaced ones of said vanes; andwherein a total flow area is defined between all 19 of said vanes and said total flow area being between 2.7491 and 3.4191 square inches (17.736-22.058 square centmeters). 2. The nozzle and shroud as set forth in claim 1, wherein said plate and said shroud are formed of a base aluminum material provided with a tungsten carbide erosion coating. 3. An air cycle machine comprising: a first stage turbine rotor and a second stage turbine rotor, said first and second stage turbine rotors being configured to drive a shaft, and a compressor rotor driven by said shaft, and a fan rotor driven by said shaft;a shroud and nozzle combination provided adjacent said first stage turbine rotor with said nozzle being at a location upstream of said first stage turbine rotor, and said shroud curving to a location downstream of said first stage turbine rotor and said shroud and nozzle including a plate and said shroud curving in a first axial direction about a center axis of said shroud relative to said plate;a plurality of vanes extending in a second axial direction away from said plate, with said plurality of vanes extending for a height away from said plate and a width being defined as the closest distance between two adjacent vanes, with a ratio of said height to said width being between 1.7377 and 2.1612;wherein there are 19 circumferentially spaced ones of said vanes; andwherein a total flow area is defined between all 19 of said vanes and said total flow area being between 2.7491 and 3.4191 square inches (17.736-22.058 square centmeters). 4. The air cycle machine as set forth in claim 3, wherein said plate and said shroud are formed of a base aluminum material provided with a tungsten carbide erosion coating. 5. A method of repairing an air cycle machine comprising the steps of: (a) removing a nozzle and shroud combination from a location adjacent a first stage turbine rotor in an air cycle machine, and replacing said removed shroud and nozzle combination with a replacement shroud and nozzle combination;(b) the replacement nozzle and shroud combination including a plate and a shroud curving in a first axial direction about a center axis of said shroud relative to said plate, and a plurality of vanes extending in a second axial direction away from said plate, with said plurality of vanes extending for a height away from said plate and a width being defined as the closest distance between two adjacent vanes, with a ratio of said height to said width being between 1.7377 and 2.1612;wherein there are 19 circumferentially spaced ones of said vanes; andwherein a total flow area is defined between all 19 of said vanes and said total flow area being between 2.7491 and 3.4191 square inches (17.736-22.058 square centmeters). 6. The method as set forth in claim 5, wherein said plate and said shroud are formed of a base aluminum material provided with a tungsten carbide erosion coating.