US4118145A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Water-cooled turbine blade
Assignee: Westinghouse Electric Corp
•
Filing: 1977-03-02
•
Granted: 1978-10-03
•
Expires: 1997-03-02
Abstract
Abstract A gas turbine blade is shown having channels subjacent the surface for a coolant to flow therethrough from a radially inner inlet to a discharge port adjacent the blade tip. The channels include intermediate enlarged chambers wherein a portion of the coolant is permitted to vaporize, so that the smaller diameter coolant distributing channels remain substantially liquid full. The vapor from the chambers is exhausted at a position radially inwardly of the blade tip and preferably below the blade platform.
Inventors
- 👤 William F. Stahl
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 15:07
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/185
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
171 words
An improved fluid cooled gas turbine blade having a coolant delivery passage through the blade root in flow communication with coolant flow channels traversing the airfoil portion of the blade subjacent the surface thereof wherein the improvement comprises: a plurality of enlarged chambers in the blade serially connected by coolant flow channels with each such chamber having at least one coolant channel discharging coolant thereinto and at least another coolant channel removing coolant therefrom, said chamber providing a coolant reservoir for separation of the coolant according to its density to permit vaporization therein of at least a portion of the coolant; vapor exhaust path means extending from each chamber to a downstream facing blade surface for discharging the vapor generated in each chamber whereby said another coolant channel receives liquid coolant from said chamber substantially free of vapor to optimize heat transfer from the blade to the coolant therein; and, final coolant passage connecting the last of said chambers in said series to an exhaust port generally adjacent the blade tip.
Claim 2
Dependent Claim
171 words
An improved fluid cooled gas turbine blade having a coolant delivery passage through the blade root in flow communication with coolant flow channels traversing the airfoil portion of the blade subjacent the surface thereof wherein the improvement comprises: a plurality of enlarged chambers in the blade serially connected by coolant flow channels with each such chamber having at least one coolant channel discharging coolant thereinto and at least another coolant channel removing coolant therefrom, said chamber providing a coolant reservoir for separation of the coolant according to its density to permit vaporization therein of at least a portion of the coolant; vapor exhaust path means extending from each chamber to a downstream facing blade surface for discharging the vapor generated in each chamber whereby said another coolant channel receives liquid coolant from said chamber substantially free of vapor to optimize heat transfer from the blade to the coolant therein; and, final coolant passage connecting the last of said chambers in said series to an exhaust port generally adjacent the blade tip.
Claim 3
Dependent Claim
32 words
Structure according to claim 1 wherein said vapor exhaust path means extending from each chamber have a common outlet generally adjacent the radially innermost portion of the airfoil portion of the blade.
Claim 4
Dependent Claim
41 words
Structure according to claim 1 wherein each of said chambers has walls extending generally radially inwardly and angled in the downstream direction to provide walls slanted from the coolant inlet channel to promote thermal currents in the coolant within the chamber.
Claim 5
Dependent Claim
37 words
Structure according to claim 3 wherein the coolant channels provide flow communication with the chambers at the radially outermost end thereof and the exhaust path provides flow communication with said chambers at the radially innermost end thereof.
Claim 6
Dependent Claim
61 words
Structure according to claim 4 wherein the coolant flow channel connecting said chambers in serial flow communication is in communication with the downstream chamber at a point radially outwardly from its point of communication with the upstream chamber to establish a pressure head under centrifugal force for coolant flow in a direction to ultimately exhaust the coolant through said final passage.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-10-02 | 1982-04-03 | 1982-10-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-10-02 | 1986-04-03 | 1986-10-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-10-02 | 1990-04-03 | 1990-10-03 | $7700.00 | Window Closed / Lapsed |