Patent US4337616A successfully refreshed from Google Patents.
US4337616A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel air ratio controlled fuel splitter
Assignee: Rolls Royce Corp
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Filing: 1980-04-14
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Granted: 1982-07-06
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Expires: 2000-04-14
Abstract
Abstract A fuel distribution system for regulating split of fuel flow between a pilot nozzle system and a main nozzle system for a combustor includes a flow network for directing fuel from a main fuel metering valve into an unrestricted line to a small pilot nozzle orifice producing a fine fuel spray pattern at low fuel flow rates and further including a fuel splitter valve interposed between the outlet from the fuel metering valve and a fuel conduit connected to a main fuel nozzle of increased orifice size to atomize higher rates of fuel flow thereto and wherein the fuel splitter valve includes an electrically energizable component that receives a control signal of desired pilot fuel/air ratio generated by a controller in part utilizing a signal of total actual fuel flow and total actual air flow to produce the control signal to control operation of the splitter valve so as to regulate the amount of fuel flow to the main nozzle system in accordance with the control signal thereby to produce a residual flow of fuel to the pilot valve to maintain a prescheduled fuel/air ratio for the pilot nozzle system to improve combustor efficiency.
Inventors
- 👤 Noel L. Downing
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 22:31
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/22; F02C7/228; F02C9/00; F02C9/26; F02C9/32; F02C9/34
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
261 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising; a pilot fuel nozzle and a main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to said pilot nozzle and said main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozzle, fuel splitter valve means for regulating fuel flow from said fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including means responsive to said control signal to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency.
Claim 2
Dependent Claim
261 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising; a pilot fuel nozzle and a main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to said pilot nozzle and said main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozzle, fuel splitter valve means for regulating fuel flow from said fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including means responsive to said control signal to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency.
Claim 3
Dependent Claim
305 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising; a pilot fuel nozzle and main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to said pilot nozzle and said main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozzle, fuel splitter valve means for requiring fuel flow from said nozzle fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including controlled means responsive to said control signal to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency, said fuel splitter controlled means being responsive to a zero control signal to condition said fuel splitter valve means to direct equal amounts of fuel to said pilot fuel nozzle and said main fuel nozzle thereby to equalize fuel distribution into the combustor.
Claim 4
Dependent Claim
305 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising; a pilot fuel nozzle and main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to said pilot nozzle and said main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozzle, fuel splitter valve means for requiring fuel flow from said nozzle fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including controlled means responsive to said control signal to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency, said fuel splitter controlled means being responsive to a zero control signal to condition said fuel splitter valve means to direct equal amounts of fuel to said pilot fuel nozzle and said main fuel nozzle thereby to equalize fuel distribution into the combustor.
Claim 5
Dependent Claim
328 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising: a pilot fuel nozzzle and a main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to a pilot nozzle and a main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozzle, fuel splitter valve means for regulating fuel flow from said fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including solenoid valve means responsive to said control signal, means including a control poppet valve defining a control pressure chamber bled by said solenoid valve means to control said poppet valve to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency, said fuel splitter solenoid valve means being responsive to a zero control signal to condition said poppet valve means to direct equal amounts of fuel to said pilot fuel nozzle and said main fuel nozzle thereby to equalize fuel distribution into the combustor.
Claim 6
Dependent Claim
328 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising: a pilot fuel nozzzle and a main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to a pilot nozzle and a main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozzle, fuel splitter valve means for regulating fuel flow from said fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including solenoid valve means responsive to said control signal, means including a control poppet valve defining a control pressure chamber bled by said solenoid valve means to control said poppet valve to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency, said fuel splitter solenoid valve means being responsive to a zero control signal to condition said poppet valve means to direct equal amounts of fuel to said pilot fuel nozzle and said main fuel nozzle thereby to equalize fuel distribution into the combustor.
Claim 7
Dependent Claim
306 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising: a pilot fuel nozzle and a main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to said pilot nozzle and said main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozle, fuel splitter valve means for regulating fuel flow from said fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including a sleeve valve and motor means responsive to said control signal to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency, said motor means being responsive to a zero control signal to condition said sleeve valve means to direct equal amounts of fuel to said pilot fuel nozzle and said main fuel nozzle thereby to equalize fuel distribution into the combustor.
Claim 8
Dependent Claim
306 words
A fuel control system for establishing a desired scheduled pilot fuel/air ratio at the pilot nozzle supplying fuel to a gas turbine engine combustor comprising: a pilot fuel nozzle and a main fuel nozzle, fuel metering means for supplying total engine fuel requirements, conduit means for directing the total engine fuel requirements to said pilot nozzle and said main nozzle, said conduit means including an unrestricted conduit directly connected between said fuel metering means and said pilot nozzle to maintain fuel metering means outlet pressure on said pilot fuel nozzle, said pilot fuel nozzle having a small orifice outlet therefrom for mixing reduced quantities of fuel with inlet air to maintain a combustible fuel/air mixture, a branch conduit to said main nozle, fuel splitter valve means for regulating fuel flow from said fuel metering means into said unrestricted conduit and said branch conduit, means establishing a control signal schedule corresponding to a desired, predetermined pilot fuel/air ratio required to maintain fuel flow from said pilot fuel nozzle to produce a fuel/air mixture therefrom to maintain combustor efficiency during reduced fuel flow rates from said fuel metering means, said fuel splitter valve means including a sleeve valve and motor means responsive to said control signal to throttle fuel flow from said fuel metering means to said branch conduit so as to maintain a controlled residual fuel flow in said unrestricted conduit to maintain the scheduled pilot fuel/air ratio at low levels of fuel flow from said metering means thereby to prevent either pilot nozzle fuel richness or pilot nozzle fuel leanness that would otherwise reduce combustor efficiency, said motor means being responsive to a zero control signal to condition said sleeve valve means to direct equal amounts of fuel to said pilot fuel nozzle and said main fuel nozzle thereby to equalize fuel distribution into the combustor.
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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) | 1985-07-05 | 1986-01-04 | 1986-07-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-07-05 | 1990-01-04 | 1990-07-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-07-05 | 1994-01-04 | 1994-07-06 | $7700.00 | Window Closed / Lapsed |