Pulse modulation technique for gas turbine engines
Various implementations described herein are related to an aircraft having a multi-engine configuration with multiple engines. The aircraft may have a flight control system coupled to the multiple engines with a multi-engine interface. The flight control system may be configured to reduce fuel consumption of at least one engine of the multiple engines during reduced-engine operation by pulse modulating fuel delivery to the at least one engine of the multiple engines.
1. An aircraft comprising:
a multi-engine configuration with multiple engines; and
a flight control system coupled to the multiple engines with a multi-engine interface, wherein the flight control system is configured to:
reduce fuel consumption of at least one engine of the multiple engines during reduced-engine operation by pulse modulating fuel delivery to the at least one engine of the multiple engines;
calculate a minimum altitude of the aircraft for reduced-engine operation; and
restart the at least one engine if a current altitude of the aircraft drops below the minimum altitude.
2. The aircraft of claim 1 , wherein:
during the reduced-engine operation, the flight control system is configured to adjust operation of the at least one engine of the multiple engines by throttling the at least one engine to IDLE or sub-IDLE.
3. The aircraft of claim 2 , wherein:
the flight control system is configured to maintain IDLE or sub-IDLE via oscillating fuel flow to the at least one engine during the reduced-engine operation.
4. The aircraft of claim 3 , wherein:
by maintaining an IDLE or sub-IDLE operation condition, the at least one engine has a reduced time required to produce and contribute additional engine power available.
5. The aircraft of claim 1 , wherein:
the flight control system is configured to selectively reduce engine power to at least one other engine of the multiple engines based on input from a pilot, and
the flight control system is configured to provide visual indication of the at least one other engine selectively operating with reduced engine power by the pilot.
6. The aircraft of claim 5 , wherein:
upon selective reduction in engine power to at least one other engine by the pilot or by automated means, the flight control system is configured to adjust operation of the at least one other engine of the multiple engines by throttling the at least one other engine to IDLE, sub-IDLE, or completely OFF.
7. The aircraft of claim 5 , wherein the flight control system is configured to selectively reduce engine power of the at least one other engine of the multiple engines by continuously calculating altitude for the reduced-engine operation based on an aircraft descent rate of the at least one other engine.
8. The aircraft of claim 7 , wherein:
the aircraft descent rate is based on current ambient conditions related to the altitude including outside ambient temperature during autorotation of the aircraft with the at least one engine of the multiple engines operating with reduced engine power.
9. The aircraft of claim 1 , wherein:
the aircraft comprises a rotorcraft, and
the multiple engines comprise multiple turbo-shaft engines.
10. A method comprising:
interfacing with multiple engines in an aircraft, the aircraft having a multiple engine configuration;
continuously calculating a minimum altitude of the aircraft for reduced-engine operation;
reducing fuel consumption of at least one engine of the multiple engines by pulse modulating fuel delivery to the at least one engine of the multiple engines during the reduced-engine operation; and
restarting the at least one engine if a current altitude of the aircraft drops below the minimum altitude.
11. The method of claim 10 , further comprising:
during reduced-engine operation, adjusting operation of the at least one engine of the multiple engines by throttling the at least one engine to IDLE or sub-IDLE.
12. The method of claim 11 , further comprising:
maintaining IDLE or sub-IDLE via oscillating fuel flow to the at least one engine during the reduced-engine operation,
wherein, by maintaining an IDLE or sub-IDLE operation condition, the at least one engine has a faster engine restart time.
13. The method of claim 10 , further comprising:
increasing fuel delivery to the at least one engine and providing corresponding advisory messages to a pilot if altitude drops significantly while in reduced-engine operation during flight.
14. The aircraft of claim 1 , wherein the flight control system is configured to calculate the minimum altitude for reduced-engine operation based on a descent rate of the aircraft and an engine restart time of the at least one engine.
15. The method of claim 10 , wherein calculating the minimum altitude for reduced-engine operation is based on a descent rate of the aircraft and an engine restart time of the at least one engine.