US4043147A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Intershaft balance weight
Assignee: United States Department of the Air Force
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Filing: 1976-06-15
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Granted: 1977-08-23
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Expires: 1996-06-15
Abstract
Abstract A balance weight supported by a spring clip is inserted inside the low turbine shaft of a jet engine at the proper position and frictionally engages an inner bulkhead in the form of an "anti-oval plug". The clip is provided with a threaded opening to receive the threaded end of an elongated rod whereby the clip is inserted within the shaft and installed at the desired location after which the rod is unscrewed from the clip and withdrawn, leaving the weight in place on the anti-oval plug.
Inventors
- 👤 David J. Wiebe
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 08:14
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/02; F01D5/027; F16; F16F; F16F15/00; F16F15/32; F16F15/322; F16F15/34; F16C; F16C2360/00; F16C2360/23; F16C3/00; F16C3/02; F16C3/023
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
115 words
An intershaft balance weight for use on the low turbine shaft of a jet engine and the like, comprising, a hollow shaft having an open forward end, an anti-oval plug of annular configuration fixedly attached near the longitudinal center of the shaft and in contact with the inner surface thereof, said anti-oval plug including a right angled portion extending upwardly from one edge thereof, said inwardly extending right angled portion forming a wall inside said hollow turbine shaft, and means for attaching the balance weight to a predetermined position on said anti-oval plug through the open forward end of said hollow shaft without substantial disassembly of the jet engine thereby trim balancing the turbine shaft.
Claim 2
Dependent Claim
115 words
An intershaft balance weight for use on the low turbine shaft of a jet engine and the like, comprising, a hollow shaft having an open forward end, an anti-oval plug of annular configuration fixedly attached near the longitudinal center of the shaft and in contact with the inner surface thereof, said anti-oval plug including a right angled portion extending upwardly from one edge thereof, said inwardly extending right angled portion forming a wall inside said hollow turbine shaft, and means for attaching the balance weight to a predetermined position on said anti-oval plug through the open forward end of said hollow shaft without substantial disassembly of the jet engine thereby trim balancing the turbine shaft.
Claim 3
Dependent Claim
81 words
The intershaft balance weight defined in claim 1 wherein the means for attaching the balance weight to the anti-oval plug includes a clip having an elongated U-shaped portion for engaging the right angled portion of said anti-oval plug and a plurality of bent ears for holding a variable weight therein, and an elongated rod threadably attached to said clip during the installation of said balance weight, said elongated rod being removed after said balance weight is positioned on said anti-oval plug.
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) | 1980-08-22 | 1981-02-21 | 1981-08-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-08-22 | 1985-02-21 | 1985-08-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-08-22 | 1989-02-21 | 1989-08-23 | $7700.00 | Window Closed / Lapsed |