Patent US4126012A successfully refreshed from Google Patents.
Patent US3950113A successfully refreshed from Google Patents.
US3950113A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbine blade
Assignee: Daimler Benz AG
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Filing: 1970-10-09
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Granted: 1976-04-13
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Expires: 1990-10-09
Abstract
Abstract An air-cooled turbine blading whose blade consists of a blade core provided with longitudinal ribs and cross ribs and of a blade jacket abutting against the ribs; the jacket is provided with air discharge apertures for the discharge of the cooling air out of the hollow spaces formed by the respective longitudinal and cross ribs; the cross ribs are provided with apertures for the flow of air which are constructed as throttling places.
Inventors
- 👤 Gunther Albrecht
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 16:06
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/187; F01D5/182; F01D5/183; F05; F05B; F05B2240/00; F05B2240/80; F05B2240/801; F05D; F05D2240/00; F05D2240/80; F05D2240/81; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
385 words
An air-cooled type turbine blade structure for mounting on a rotor having an axis of rotation, said structure comprising: root means for attaching said blade structure to the rotor, web plate means disposed radially outwardly of said root means with respect to said axis, solid blade core means disposed radially outwardly of said web plate means, blade jacket means surrounding said core means and including discharge apertures arranged over the surface thereof for discharging cooling air, a plurality of longitudinal radially extending rib means and a plurality of cross rib means interconnecting respective adjacent longitudinal rib means being arranged on the surface of said core means, said jacket means being attached to the outer edges of the respective rib means to form a set of first hollow spaces between said jacket means and the surface of said core means which are bounded by said respective rib means, channel means extending through said web plate means for communicating the radially innermost first hollow spaces between respective adjacent longitudinal rib means with cooling air supply means, and aperture means extending through said cross rib means for communicating said radially innermost first hollow spaces with first hollow spaces arranged radially outwardly thereof, said aperture means being dimensioned as throttling spaces for effecting a predetermined distribution of cooling air throughout the various first hollow spaces arranged on the surface of the blade core means, wherein said Web plate means includes recess means formed in a radially outwardly facing surface, a sheet metal member being provided for covering said recess means to form a plurality of second hollow spaces between said sheet metal member and said web plate means, each of said second hollow spaces extending to a position directly radially inwardly with respect to a respective radially innermost first hollow space such that said second spaces and said radially innermost first spaces communicate respectively with one another, said channel means extending from outside the web plate means to said second spaces, wherein each of said second spaces is connected with a separate channel forming part of said channel means for communicating cooling air from the cooling air supply means to the respective second space, and wherein the cross-sectional area of each of the respective channels is substantially less than the cross-sectional area of the respective second space connected therewith.
Claim 2
Dependent Claim
385 words
An air-cooled type turbine blade structure for mounting on a rotor having an axis of rotation, said structure comprising: root means for attaching said blade structure to the rotor, web plate means disposed radially outwardly of said root means with respect to said axis, solid blade core means disposed radially outwardly of said web plate means, blade jacket means surrounding said core means and including discharge apertures arranged over the surface thereof for discharging cooling air, a plurality of longitudinal radially extending rib means and a plurality of cross rib means interconnecting respective adjacent longitudinal rib means being arranged on the surface of said core means, said jacket means being attached to the outer edges of the respective rib means to form a set of first hollow spaces between said jacket means and the surface of said core means which are bounded by said respective rib means, channel means extending through said web plate means for communicating the radially innermost first hollow spaces between respective adjacent longitudinal rib means with cooling air supply means, and aperture means extending through said cross rib means for communicating said radially innermost first hollow spaces with first hollow spaces arranged radially outwardly thereof, said aperture means being dimensioned as throttling spaces for effecting a predetermined distribution of cooling air throughout the various first hollow spaces arranged on the surface of the blade core means, wherein said Web plate means includes recess means formed in a radially outwardly facing surface, a sheet metal member being provided for covering said recess means to form a plurality of second hollow spaces between said sheet metal member and said web plate means, each of said second hollow spaces extending to a position directly radially inwardly with respect to a respective radially innermost first hollow space such that said second spaces and said radially innermost first spaces communicate respectively with one another, said channel means extending from outside the web plate means to said second spaces, wherein each of said second spaces is connected with a separate channel forming part of said channel means for communicating cooling air from the cooling air supply means to the respective second space, and wherein the cross-sectional area of each of the respective channels is substantially less than the cross-sectional area of the respective second space connected therewith.
Claim 3
Dependent Claim
45 words
A turbine blade structure according to claim 1, characterized in that said second spaces correspond in number to the radially innermost first spaces, and in that each of said second spaces is positioned to communicate with a corresponding one of said radially innermost first spaces.
Claim 4
Dependent Claim
34 words
A turbine blade structure according to claim 2, characterized in that each of said channels is dimensioned as throttling spaces for effectiing a predetermined distribution of cooling air to the various second hollow spaces.
Claim 5
Dependent Claim
28 words
A turbine blade structure according to claim 3, characterized in that the root means, web plate means and blade core means are formed as a single solid member.
Claim 6
Dependent Claim
28 words
A turbine blade structure according to claim 1, characterized in that the radially innermost end of said blade jacket means is attached directly to said sheet metal member.
Claim 7
Dependent Claim
28 words
A turbine blade structure according to claim 3, characterized in that the radially innermost end of said blade jacket means is attached directly to said sheet metal member.
Claim 8
Dependent Claim
32 words
A turbine blade structure according to claim 5, characterized in that said first hollow spaces are in communication with one another only by way of said apertures in the cross rib means.
Claim 9
Dependent Claim
32 words
A turbine blade structure according to claim 3, characterized in that said first hollow spaces are in communication with one another only by way of said apertures in the cross rib means.
Claim 10
Dependent Claim
55 words
A turbine blade structure according to claim 1, characterized in that said web plate means includes a shoulder portion extending parallel to the axis of rotation of the rotor, said shoulder portion exhibiting a larger cross-section than either the blade core means or the root means, said channel means being arranged in said shoulder portion.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-04-13 | 1979-10-13 | 1980-04-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-04-13 | 1983-10-13 | 1984-04-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-04-13 | 1987-10-13 | 1988-04-13 | $7700.00 | Window Closed / Lapsed |