Invention Grant
- Patent Title: Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation
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Application No.: US14811122Application Date: 2015-07-28
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Publication No.: US10094229B2Publication Date: 2018-10-09
- Inventor: Brooks E. Snyder , Michael G. McCaffrey , Thomas N. Slavens
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- Main IPC: F01D5/08
- IPC: F01D5/08 ; F01D9/02 ; F02C7/18 ; F01D17/16 ; F01D9/06

Abstract:
A cooling system integrated into a stator assembly of a gas turbine engine has an on-board injector or cooling nozzle located for cooling of a rotor assembly. The nozzle may be generally annular and may contain a plurality of pivoting airfoils circumferentially spaced from one-another for directing cooling air flow from the nozzle and generally toward a plurality of holes in a cover of the rotor assembly. The pivoting airfoils are adapted to move between a spoiled state where the mass flow of cooling air is reduced, and to an optimal state where the mass flow is increased. The system may further include a plurality of fixed airfoils in the nozzle with adjacent fixed airfoils defining a discharge orifice in the nozzle. Each one of the plurality of pivoting airfoils may be located in a respective discharge orifice.
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