US4192137A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turboshaft engine
Assignee: National Research Council Canada
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Filing: 1978-08-21
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Granted: 1980-03-11
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Expires: 1998-08-21
Abstract
Abstract An improvement in torque characteristics is provided for a turboshaft engine of the type having a compressor rotor driven by a gas generator turbine that is mechanically independent of the power turbine. The improvement comprises a rotatable compressor stator casing which is interconnected with the power turbine rotor to allow rotation of the compressor casing in the same direction as the compressor rotor at a lower speed. At reduced output shaft speed, the relative speed between the compressor rotor blades and stator blades is increased for increased gas generator output and hence torque, for a predetermined compressor rotor speed.
Inventors
- 👤 Marcus S. Chappell
- 👤 Douglas A. J. Millar
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 09:04
CPC Classifications
F; F02; F02C; F02C3/00; F02C3/04; F02C3/06; F02C3/067; F01; F01D; F01D5/00; F01D5/02; F01D5/03; F02C3/107; F02C3/113; F02C9/00; F02C9/16
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
105 words
A turboshaft engine comprising a compressor having a rotor and stator casing, a gas generator turbine having a rotor and a fixed stator, a power turbine having a rotor and a fixed stator, and an output shaft connected with the power turbine; said compressor rotor being connected with the gas generator turbine rotor; and said compressor stator casing being rotatably mounted and coaxial with the compressor rotor and interconnected with the output shaft for allowing rotation of the compressor casing in the direction of the compressor rotor at a speed less than that of the compressor rotor and in proportion to the output shaft speed.
Claim 2
Dependent Claim
105 words
A turboshaft engine comprising a compressor having a rotor and stator casing, a gas generator turbine having a rotor and a fixed stator, a power turbine having a rotor and a fixed stator, and an output shaft connected with the power turbine; said compressor rotor being connected with the gas generator turbine rotor; and said compressor stator casing being rotatably mounted and coaxial with the compressor rotor and interconnected with the output shaft for allowing rotation of the compressor casing in the direction of the compressor rotor at a speed less than that of the compressor rotor and in proportion to the output shaft speed.
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) | 1983-03-11 | 1983-09-10 | 1984-03-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-03-11 | 1987-09-10 | 1988-03-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-03-11 | 1991-09-10 | 1992-03-11 | $7700.00 | Window Closed / Lapsed |