High-speed generator for a gas turbine engine

• US 4,669,263 A
• Filed: 11/18/1985
• Issued: 06/02/1987
• Est. Priority Date: 11/19/1984
• Status: Expired due to Term

• Current Assignee: Toyota Jidosha Kabushiki Kaisha (Toyota Motor Corporation)
• Original Assignee: Toyota Jidosha Kabushiki Kaisha (Toyota Motor Corporation)
• Inventors: Sugiyama, Matsuyoshi
• Primary Examiner(s): Casaregola, Louis J.
• Assistant Examiner(s): Thorpe, Timothy S.
• Application Number:
  US06/799,167
• Time in Patent Office: 561 Days
• Field of Search: 60/39.08, 184/6.11, 290/52, 415/168, 415/169, 415/110, 415/112, 417/366, 417/372
• US Class Current: 60/39.08
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M

Abstract

In the arrangement of a high-speed generator having its rotor shaft direct-coupled to the main shaft of a gas turbine engine, the upper space of a oil tank fixed to the generator communicates to a cavity formed between the high-speed generator and the air intake of the gas turbine engine, aside from the normal oil return path; and the cavity is open to the atmosphere through the upper space of the oil tank, thereby eliminating any difference in pressure between the cavity and the inside of the high-speed generator. With elimination of any pressure differences, the development of air flow at a tiny gap between the rotor and the stator of the high-speed generator can be avoided, resulting in successful prevention of oil leakage from the rotor bearing into the tiny gap and no drop in the efficiency of the high-speed generator.

Claims

1. A high-speed generator for a gas turbine engine, said high-speed generator comprising:

a generator having a rotor shaft direct-coupled to a main shaft of said gas turbine engine, said generator defining a tiny gap between a rotor and a stator thereof;

an oil tank storing oil for lubricating various parts of said generator and said gas turbine engine;

oil return path means for returning oil from said various parts of said generator and said gas turbine engine to said oil tank; and

communicating path means for communicating from a cavity formed between said generator and an air intake of said gas turbine engine to an upper space in said oil tank, said communicating path means being separate and distinct from said oil return path means, communication due to said communicating path being capable of eliminating any difference in pressure between said cavity and said tiny gap.

2. The high-speed generator of claim 1, wherein said communicating means communicates to said cavity at a higher position than the axis of said main shaft of said gas turbine engine.

3. The high-speed generator of claim 1, wherein said communicating means comprises a pipe located externally of said high-speed generator.

4. The high-speed generator of claim 1, wherein said communicating means comprises an internal path formed with the device.

5. The high-speed generator of claim 1, wherein said oil return means comprises at least one return path communicating from bearings at both ends of the rotor shaft to said oil tank.

6. The high-speed generator of claim 1, wherein said oil tank communicates to said oil return means for returning oil from bearings supporting said main shaft of said gas turbine engine.

7. The high-speed generator of claim 1, wherein said upper space of said oil tank is open to the atmosphere through a breather.