US3749514A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Blade attachment
Assignee: RTX Corp
•
Filing: 1971-09-30
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Granted: 1973-07-31
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Expires: 1991-09-30
Abstract
Abstract A blade attachment means for use in a small gas turbine engine. A disk is provided having at least two annular flanges extending radially therefrom with a plurality of blades having root fingers metallurgically bonded to the flanges. The flanges being approximately the same length as the blades with the space between the fingers providing for the passage of a coolant to cooling passages in the blade. Said fingers having a brazing area sized so that at least a 50 percent braze coverage will provide the necessary bond strength.
Inventors
- 👤 H Welcer
- 👤 G Kelch
- 👤 B Taylor
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 12:58
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/02; F01D5/08; F01D5/085; F01D5/087; F01D5/30; F01D5/3061
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
269 words
A high speed rotor comprising a small rotor disk and a plurality of small blades, said disk having an outer surface with a pair of spaced annular radial flanges extending therefrom, said annular radial flanges being a continuous circumferential extension from each side of the disk, each blade having a blade platform, each blade having a bottom surface below said platform with a pair of spaced root fingers extending therefrom, said root fingers having a flat surface overlapping and being bonded to a flat surface on said radial flanges, said platform extending forwardly and rearwardly over the annular radial flanges, said flanges and said root fingers being of such length that the bottom surface of the blade is spaced from the outer surface of the rotor disk a distance not less than about half the length of the blade, a circumferential passage being formed between the bottom surface of the blade and the outer surface of the rotor disk and the flanges and root fingers, said passage being sized to act as an insulator to restrict heat conduction from the blades to the disk, means for supplying a coolant through said passage, the length of said blades being approximately one inch or less, the root fingers being thin and tapered inwardly from said bottom surface and said radial flanges being thin and tapered inwardly as they extend from said outer surface, said thin flanges and fingers prOviding for axial deflection in response to growth due to the blades operating at a much higher temperature than the main body of the disk and reducing the heat flow into the disk.
Claim 2
Dependent Claim
269 words
A high speed rotor comprising a small rotor disk and a plurality of small blades, said disk having an outer surface with a pair of spaced annular radial flanges extending therefrom, said annular radial flanges being a continuous circumferential extension from each side of the disk, each blade having a blade platform, each blade having a bottom surface below said platform with a pair of spaced root fingers extending therefrom, said root fingers having a flat surface overlapping and being bonded to a flat surface on said radial flanges, said platform extending forwardly and rearwardly over the annular radial flanges, said flanges and said root fingers being of such length that the bottom surface of the blade is spaced from the outer surface of the rotor disk a distance not less than about half the length of the blade, a circumferential passage being formed between the bottom surface of the blade and the outer surface of the rotor disk and the flanges and root fingers, said passage being sized to act as an insulator to restrict heat conduction from the blades to the disk, means for supplying a coolant through said passage, the length of said blades being approximately one inch or less, the root fingers being thin and tapered inwardly from said bottom surface and said radial flanges being thin and tapered inwardly as they extend from said outer surface, said thin flanges and fingers prOviding for axial deflection in response to growth due to the blades operating at a much higher temperature than the main body of the disk and reducing the heat flow into the disk.
Claim 3
Dependent Claim
39 words
A high speed rotor as set forth in claim 1 wherein said root fingers have an area so that at least a 50 percent bond coverage of said area with the radial flanges will provide the necessary bond strength.
References Cited (Backward Citations)
DE675222C
Cited
US2431249A
Cited
US2696364A
Cited
US2675208A
Cited
US2857132A
Cited
DE939782C
Cited
GB868788A
Cited
US3297301A
Cited
US3609841A
Cited
US3550372A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1976-07-30 | 1977-01-29 | 1977-07-31 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1980-07-30 | 1981-01-29 | 1981-07-31 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1984-07-30 | 1985-01-29 | 1985-07-31 | $7700.00 | Window Closed / Lapsed |