Thrust bearing loading arrangement for gas turbine engines

• US 4,730,977 A
• Filed: 12/31/1986
• Issued: 03/15/1988
• Est. Priority Date: 12/31/1986
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Haaser, Frederic G.
• Primary Examiner(s): Makay, Albert J.
• Assistant Examiner(s): NOT, DEFINED
• Application Number:
  US06/948,370
• Time in Patent Office: 440 Days
• Field of Search: 415/104, 415/105, 415/106, 415/107, 415/131, 415/132, 416/170 R, 60/39.31, 60/39.091, 60/39.25, 60/39.83
• US Class Current: 415/104
• CPC Class Codes: F01D 3/00 Machines or engines with axial-thrust balancing effected by working-fluid

Abstract

A plurality of openings are provided in a stationary wall of a gas turbine engine aft of the compressor discharge to admit compressor discharge air into a sealed cavity formed between the stationary wall and the rotor of the gas turbine engine. A valve, biased to an open position, is associated with each of the openings so that under low speed conditions some of the compressor discharge air is admitted to the cavity to provide supplementary axial force on the rotor in one direction to prevent crossover under such conditions. Under higher speed conditions the increase in compressor discharge pressure overcomes the force biasing the valve to its open position, thereby causing the valve to close and terminate flow of compressor discharge air to the cavity, terminating the aforementioned supplementary axial force on the rotor. Each of the valves includes a housing surrounding the corresponding opening in the stationary wall and a valve piston within the housing is biased to an open position by open or more belleville springs positioned within the housing.

Claims

1. In a gas turbine engine including a stationary wall and a rotor comprising a compressor and a turbine, a thrust bearing loading arrangement comprising:

(a) means for mounting said rotor for rotating movement, said means including a thrust ball bearing;

(b) said engine including at least one sealed cavity between a portion of said rotor and said stationary wall;

(c) said cavity including an aft wall and a forward wall, one of said walls having a greater surface area than the other of said walls;

(d) said stationary wall having an opening aft of said compressor for providing a path for flow of compressor discharge air into said cavity to increase the load on said thrust bearing;

(e) means responsive to compressor discharge pressure for controlling flow of compressor discharge air into said cavity to insure unidirectional loading on said thrust bearing throughout the normal operating range of said engine.

2. The thrust bearing loading arrangement as recited in claim 1 including a plurality of openings in said stationary wall for providing a plurality of paths for flow of compressor discharge air into said cavity and a plurality of said means for controlling flow of compressor discharge air through said openings into said cavity.

3. The thrust bearing loading arrangement as recited in claim 2 wherein each of said means for controlling flow of discharge air through said openings comprises:

(a) a housing;

(b) means for securing each of said housings to said stationary wall surrounding a corresponding one of said openings;

(c) means providing a valve seat at each of said openings;

(d) a valve piston positioned for engaging each of said seats and movable within its corresponding housing between an open and a closed position;

(e) all of said housings having the same predetermined height;

(f) a plurality of flat nonresilient washers and a plurality of belleville springs arranged in a stack in each of said housings for biasing the corresponding valve piston toward its open position;

(g) the number of said flat washers and the number of said belleville springs in each of said housings being varied to vary the biasing force on the corresponding valve element while maintaining substantially the same height for each of said stacks of springs and washers;

(h) whereby said valves controlling said plurality of openings are arranged to open and close at different times so as to vary said thrust bearing loading in stepped fashion while employing the same standard parts.

4. The thrust bearing loading arrangement as recited in claim 1 wherein said means for controlling flow of compressor discharge air through said opening comprises a valve, said valve including means for biasing said valve to an open position, said valve being moved to its closed position when said compressor discharge pressure exceeds the force exerted by said biasing means.

5. The thrust bearing loading arrangement as recited in claim 4 wherein said biasing means comprises a spring.

6. The thrust bearing loading arrangement as recited in claim 5 wherein said spring is a belleville spring.

7. The thrust bearing loading arrangement as recited in claim 4 wherein said valve comprises:

(a) a housing;

(b) means for securing said housing to said stationary wall surrounding said opening;

(c) means providing a valve seat at said opening;

(d) a valve piston positioned for engaging said seat and movable within said housing between an open and a closed position; and

(e) a spring disposed in said housing and engaging said valve piston for biasing said valve piston to its open position.

8. The thrust bearing loading arrangement as recited in claim 7 wherein said housing is made in two complementary halves to facilitate assembly of said valve element and said spring therein.

9. The thrust bearing loading arrangement as recited in claim 8 wherein said securing means for each of said housing halves comprises at least two fasteners engaging said stationary wall whereby said housing cannot become disassembled unless at least two or more fasteners fail.

10. The thrust bearing loading arrangement as recited in claim 7 wherein said spring is a belleville spring.

11. The thrust bearing loading arrangement as recited in claim 10 wherein said housing has a predetermined height, a plurality of belleville springs are employed, and said biasing force is varied by substituting flat nonresilient washers for one or more of said belleville springs.

12. The thrust bearing loading arrangement as recited in claim 7 wherein the face of said housing engaging said stationary wall is formed to include a recess therein, and a sealing gasket is disposed within said recess.