Engine system and method of operating the same

Patent metadata

Field	Value
Publication number	US-2023258135-A1
Application number	US-202318162949-A
Country	US
Kind code	A1
Filing date	Feb 1, 2023
Priority date	Feb 15, 2022
Publication date	Aug 17, 2023
Grant date	—

Abstract

A system has first and second fuel stores for first and second fuels, an engine, a fuel distribution system, first and second flow rates of the fuel contributing to a total flow rate of fuel; and a controller for controlling the relative fractions of the total flow rate of fuel to the engine according to the required power output of the engine such that the relative fraction of the total flow rate of fuel to the engine represented by the second flow rate increases with increasing required power output of the engine. The fuels are selected such that using only the second fuel results in a lower engine temperature than using only the first fuel, for the same mechanical power and/or the second fuel has a lower specific energy than the first and/or the second fuel produces more water during combustion than the first fuel per unit of fuel energy.

First claim

1 . An engine system comprising:
a first fuel store of a first fuel; a second fuel store of a second fuel; an engine arranged to produce mechanical power by combustion or oxidation of fuel in the engine; a fuel distribution system arranged to deliver fuel from the first and second fuel stores to the engine, the first fuel delivered at a first flow rate, the second fuel delivered at a second flow rate, the first and second flow rates contributing to a total flow rate of fuel to the engine; and a control system arranged to control the relative fractions of the total flow rate of fuel to the engine represented by the first and second flow rates according to the required power output of the engine such that the relative fraction of the total flow rate of fuel to the engine represented by the second flow rate increases with increasing required power output of the engine for at least part of a period of operation of the engine,
wherein the first and second fuels are selected such that operation of the engine using only the second fuel results in a lower engine temperature than operation of the engine using only the first fuel, when producing the same amount of mechanical power and/or wherein the second fuel has a lower specific energy than the first fuel and/or wherein the second fuel produces more water during combustion than the first fuel per unit of fuel energy released during combustion.

2 . The engine system of claim 1 , wherein the control system is arranged to, during a period of acceleration, control the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate based on a surge margin.

3 . The engine system of claim 2 , wherein a one of the first fuel or second fuel has a higher specific energy than the other of the first fuel and second fuel and releases a greater mass of water per unit mass of fuel than the other of the first fuel and second fuel, wherein the control system may be arranged to increase the relative fraction of the one of the first fuel or second fuel during an initial portion of the period of acceleration, and wherein the control system may be arranged to reduce the relative fraction of the total mass flow rate of fuel represented by the one of the first fuel and second fuel during a final portion of the period of acceleration.

4 . The engine system of claim 3 , wherein the control system is arranged to control the relative fractions of the total mass flow rate of fuel provided by the first mass flow rate and second mass flow rate such that:
the surge margin is increased compared to operating on the other of the first fuel or second fuel only and the rate of acceleration is the same as operating on the other of the first fuel or second fuel only; or the surge margin is the same as operating on the other of the first fuel or second fuel only and the rate of acceleration is increased compared to operation using the other of the first fuel or second fuel only.

5 . The engine system of claim 1 , wherein the control system is arranged to, during a period of operation of the engine, control the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate, based on an engine temperature, and may be arranged to control the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate to change the engine temperature at a first rate of change, whilst maintaining constant mechanical power.

6 . The engine system of claim 5 , wherein the control system is arranged to vary the engine temperature at constant mechanical power prior to a period of increased or decreased mechanical power demand to pe-warm or pre-cool the engine, wherein the first rate of change is slower than the rate of change of engine temperature resulting from the change in mechanical power demand without pre-warming or pre-cooling.

7 . The engine system of claim 5 , wherein the control system is arranged to control the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate to keep the engine temperature below a threshold temperature for at least a section of a period of operation, wherein the threshold temperature may be variable in different sections of the period of operation.

8 . The engine system of claim 7 , wherein control system is arranged to increase the threshold temperature in sections of the period of operation with higher mechanical power demand and reduce the threshold temperature in sections of the period of operation with lower mechanical power demand.

9 . The engine system of claim 8 , wherein the engine comprises an air flow that is compressed and mixed with the fuel for combustion or oxidation, and a portion of the air flow is removed prior to combustion or oxidation, to provide cooling air for cooling parts of the engine, wherein the control system is further arranged to:
vary a proportion of the air flow removed for cooling air over the period of operation.

10 . The engine system of claim 7 , wherein the control system is arranged to:
when the engine temperature is below a second threshold temperature, lower than the threshold temperature, keeping the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate constant; and when the engine temperature is above the second threshold temperature, varying the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate to keep the engine temperature below the threshold temperature.

11 . The engine system of claim 5 , wherein the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate are controlled to keep the engine temperature substantially constant for at least a section of a period of operation.

12 . The engine system of claim 11 , wherein the mechanical power demand of the engine varies over the section of the period of operation in which the engine temperature is kept substantially constant by control of the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate.

13 . The engine system of claim 5 , wherein the engine comprises an electrical generator powered by operation of the engine, wherein an electrical power drawn by the generator varies over a section of the period of operation, and wherein the control system is further arranged to:
control the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate, based on the engine temperature and the electrical demand.

14 . The engine system of claim 13 , wherein the mechanical power is maintained as constant for the section of the period of operation over which the relative fractions of the total mass flow rate of fuel represented by the first mass flow rate and the second mass flow rate are controlled based on the engine temperature and the electrical demand.

15 . The engine system of claim 5 , wherein the engine temperature is determined for a hottest part in the engine, for example wherein the engine temperature is determined at an exit of a chamber in which combustion or oxidation of the fuel occurs.

16 . The engine system of claim 1 , wherein the control system is further arranged to start the engine using the second fuel based on an ambient temperature.

17 . The engine

Assignees

• Rolls Royce Plc

Inventors

• Swann Peter

Classifications

• F02C9/40 Primary

  specially adapted to the use of a special fuel or a plurality of fuels · CPC title

• F02C7/22

  Fuel supply systems · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2270/053

  Explicitly mentioned power · CPC title

• F05D2270/08

  to produce clean exhaust gases · CPC title