Patent US4897994A successfully refreshed from Google Patents.
US4897994A
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US
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Method of starting turbine engines
Assignee: Sundstrand Corp
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Filing: 1988-10-03
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Granted: 1990-02-06
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Expires: 2008-10-03
Abstract
Abstract The turbine engine may be started without the use of start injectors by a method including the steps of initiating rotation of a compressor and turbine wheel by applying an external angular accelerating force thereto, introducing fuel through a minority of the fuel injectors employed at about 5-10% of rated engine speed while continuing the application of the accelerating force, introducing fuel through the remainder of the injectors after ignition of the fuel introduced by the prior step and when the engine reaches 15-25% of rated speed while maintaining injection through the minority of injectors, and thereafter modulating fuel flow through all of the injectors to operate the engine in a desired fashion. Also disclosed is a turbine engine practicing the foregoing method.
Inventors
- 👤 Jack R. Shekleton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 20:15
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/26; F23; F23R; F23R3/00; F23R3/28
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
144 words
A method of starting a small turbine engine having a rotary turbine wheel, a rotary compressor coupled to the turbine wheel, an annular combustor provided with a plurality of angularly spaced fuel injectors and characterized by the absence of start injectors comprising the steps of: (a) initiating rotation of said compressor and said turbine wheel by applying an external angular accelerating force thereto; (b) at about 5-10% of rated engine speed, providing fuel to a minority of said injectors while continuing the application of said accelerating force; (c) after ignition of the fuel introduced during step (b), and when the engine reaches 15-25% of rated speed, introducing fuel into said combustor through the remainder of said injectors while maintaining injection through said minority of injectors; and (d) thereafter modulating fuel flow through all of said injectors to operate said engine in a desired fashion.
Claim 2
Independent Claim
144 words
A method of starting a small turbine engine having a rotary turbine wheel, a rotary compressor coupled to the turbine wheel, an annular combustor provided with a plurality of angularly spaced fuel injectors and characterized by the absence of start injectors comprising the steps of: (a) initiating rotation of said compressor and said turbine wheel by applying an external angular accelerating force thereto; (b) at about 5-10% of rated engine speed, providing fuel to a minority of said injectors while continuing the application of said accelerating force; (c) after ignition of the fuel introduced during step (b), and when the engine reaches 15-25% of rated speed, introducing fuel into said combustor through the remainder of said injectors while maintaining injection through said minority of injectors; and (d) thereafter modulating fuel flow through all of said injectors to operate said engine in a desired fashion.
Claim 3
Dependent Claim
34 words
The method of claim 1 where step (b) is performed at approximately 7-8% of rated engine speed and step (c) is initiated at an engine speed on the order of 20% rated engine speed.
Claim 4
Independent Claim
154 words
A method of starting a small turbine engine having a rotary turbine wheel, a rotary compressor coupled to the turbine wheel, an annular combustor provided with a plurality of equally angularly spaced fuel injectors and characterized by the absence of start injectors comprising the steps of: (a) initiating rotation of said compressor and said turbine wheel by applying an external angular accelerating force thereto; (b) at about 5-10% of rated engine speed, introducing fuel tangentially into said combustor through a minority of substantially diametrically opposite said injectors while continuing the application of said accelerating force; (c) after ignition of the fuel introduced during step (b) and when the engine reaches 15-25% of rated speed, introducing additional fuel tangentially into said combustor through the remainder of said injectors while maintaining injection through said minority of injectors; and (d) thereafter modulating fuel flow through all of said injectors to operate said engine in a desired fashion.
Claim 5
Independent Claim
154 words
A method of starting a small turbine engine having a rotary turbine wheel, a rotary compressor coupled to the turbine wheel, an annular combustor provided with a plurality of equally angularly spaced fuel injectors and characterized by the absence of start injectors comprising the steps of: (a) initiating rotation of said compressor and said turbine wheel by applying an external angular accelerating force thereto; (b) at about 5-10% of rated engine speed, introducing fuel tangentially into said combustor through a minority of substantially diametrically opposite said injectors while continuing the application of said accelerating force; (c) after ignition of the fuel introduced during step (b) and when the engine reaches 15-25% of rated speed, introducing additional fuel tangentially into said combustor through the remainder of said injectors while maintaining injection through said minority of injectors; and (d) thereafter modulating fuel flow through all of said injectors to operate said engine in a desired fashion.
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) | 1993-02-05 | 1993-08-07 | 1994-02-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-02-05 | 1997-08-07 | 1998-02-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-02-05 | 2001-08-07 | 2002-02-06 | $7700.00 | Window Closed / Lapsed |