Turbine rotor disk with dirt particle separator

• US 7,665,965 B1
• Filed: 01/17/2007
• Issued: 02/23/2010
• Est. Priority Date: 01/17/2007
• Status: Expired due to Fees

• Current Assignee: Florida Turbine Technologies, Inc. (Kratos Defense & Security Solutions Incorporated)
• Original Assignee: Florida Turbine Technologies, Inc. (Kratos Defense & Security Solutions Incorporated)
• Inventors: Liang, George
• Primary Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US11/654,157
• Time in Patent Office: 1,133 Days
• Field of Search: 415/1, 415/115, 416/1, 416/90.R, 416/92, 416/95, 416/96.R, 416/96.A, 416/97.R
• US Class Current: 416/1
• CPC Class Codes: F01D 25/00 Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
• CPC Class Codes: F01D 5/18 Hollow blades, i.e. blades with cooling or heating channels or cavities structure of hollow blades in general F01D5/147; Heating, heat-insulating or cooling means on blades
• CPC Class Codes: F05D 2260/607 Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles

Abstract

A turbine rotor disk with a turbine blade, the rotor disk having a cooling air feed channel to force cooling air into an internal cooling air passage within the turbine blade, the feed channel including a swirl generator at the inlet end to promote a swirling motion within the cooling air, and the feed channel including a helical rib extending from the swirl generator to the outlet of the feed channel to maintain the swirling motion of the cooling air within the feed channel such that dirt particles in the cooling air are collected within the center of the swirling air flow. The feed channel directs the swirling cooling air into a first passage of the internal serpentine flow cooling circuit of the blade. A cooling air exit hole is located at the blade tip and is aligned with the cooling air flow in the first passage. The swirling air flow with the collected dirt particles ejects the dirt particles out through the exit hole while the clean cooling air continues through the serpentine flow circuit to provide cooling for the blade.

Claims

1. A turbine rotor disk with a blade having an internal cooling air passage to provide cooling for the blade, the rotor disk including a cooling air feed channel to force cooling air into the internal cooling air passage due to rotation of the rotor disk, the improvement comprising:

a swirl generator located within the cooling air feed channel, the swirl generator forcing the cooling air to flow through the feed channel in a swirling flow.

2. The turbine rotor disk of claim 1, and further comprising:

the swirl generator is located at the entrance to the feed channel.

3. The turbine rotor disk of claim 2, and further comprising:

at least one helical rib located in the feed channel and downstream from the swirl generator, the helical rib forcing the swirling air flowing through the feed channel to continue in the swirling flow.

4. The turbine rotor disk of claim 3, and further comprising:

the at least one helical rib extends substantially from the swirl generator to the outlet of the feed channel and into a live rim box.

5. The turbine rotor disk of claim 1, and further comprising:

the cooling air feed channel is aligned with a first passage in the blade such that the swirling cooling air flows through the first passage in alignment with a blade tip particulate purge hole.

6. The turbine rotor disk of claim 1, and further comprising:

the swirl generator and at least one helical rib forces dirt particles to flow along substantially the center of the swirling air flow.

7. The turbine rotor disk of claim 5, and further comprising:

the first passage is a first leg of a serpentine flow cooling circuit passing through the blade such that dirt particles trapped within the swirling flow pass out through the particulate purge hole while clean cooling air continues around and through the serpentine flow circuit to cool the blade.

8. The turbine rotor disk of claim 1, and further comprising:

a live rim cavity formed in a blade root;

the feed channel opens into the live rim cavity;

a first channel of a serpentine flow cooling circuit extends along a leading edge of the blade and in alignment with the feed channel such that swirling cooling air continues flowing into the first channel; and

,

a blade tip purge hole located at the end of the first channel and in alignment with the swirling cooling air such that dirt particles trapped within the swirling flow of cooling air will be discharged out through the purge hole while the clean cooling air continues through the serpentine flow cooling circuit.

9. In a turbine rotor disk having a feed channel in the rotor disk and an internal cooling passage in a rotor blade, a process for separating dirt particles from cooling air passing through the blade comprising the steps of:

promoting a vortex swirling motion in the cooling air that is passed into a first channel of the blade cooling passage;

providing an initial swirl to the cooling air flowing into the feed channel;

collecting dirt particles within the swirling cooling air passing through the feed channel;

directing the swirling air in the first channel toward a particulate purge hole in the blade tip; and

,

turning the cooling air through the blade cooling passage at the blade tip such that the dirt particles are ejected out through the particulate purge hole while clean cooling air continues along the blade cooling air passage to provide cooling for the blade.

10. The process for separating dirt particles from the cooling air passing through the blade of claim 9, and further comprising the step of:

after the step of providing an initial swirl to the cooling air flowing into the feed channel, maintaining the swirl flow in the cooling air for the remainder of the flow along the feed channel.

11. The process for separating dirt particles from the cooling air passing through the blade of claim 9, and further comprising the step of:

passing the cooling air in the first channel along a leading edge of the blade.

12. The process for separating dirt particles from the cooling air passing through the blade of claim 9, and further comprising the step of:

passing the swirling cooling air from the feed channel into a live rim cavity before passing the swirling cooling air into the first channel.