Powerplant and related control system and method

Patent metadata

Field	Value
Publication number	US-9719411-B2
Application number	US-201615009776-A
Country	US
Kind code	B2
Filing date	Jan 28, 2016
Priority date	Sep 23, 2008
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A hydrogen fueled powerplant including an internal combustion engine that drives a motor-generator, and has a two-stage turbocharger, for an aircraft. A control system controls the operation of the motor-generator to maintain the engine at a speed selected based on controlling the engine equivalence ratio. The control system controls an afterburner, an intercooler and an aftercooler to maximize powerplant efficiency. The afterburner also adds power to the turbochargers during high-altitude restarts. The turbochargers also include motor-generators that extract excess power from the exhaust.

First claim

What is claimed is:

1. A powerplant, comprising:
an engine configured to react a first reactant with a gaseous stream of second reactant to produce energy and an exhaust stream, wherein the gaseous stream of second reactant is provided to the engine at a flow rate;
a compressor configured to pressurize the gaseous stream of second reactant supplied to the engine;
a turbine, wherein the compressor is driven in rotation by a driving force from the turbine, and wherein the turbine is propelled by the exhaust stream; and
an electrical generator configured to be driven by energy extracted from the exhaust stream.

2. The powerplant of claim 1 , and further comprising:
an afterburner in the exhaust stream upstream of the turbine, and upstream of where energy is extracted from the exhaust stream for the generator, the afterburner being configured to react additional reactants in the exhaust stream; and
a control system configured to control the amount of additional reactants reacted in the exhaust such that adequate energy is present in the exhaust stream to drive both the generator and the compressor at optimized levels.

3. The powerplant of claim 1 , wherein the turbine is further configured to drive the generator using energy extracted from the exhaust stream.

4. The powerplant of claim 3 , and further comprising a control system, wherein the generator is configured to apply variable levels of motive force on the turbine, and wherein the control system configured to control the variable motive force applied to the turbine by the generator.

5. The powerplant of claim 4 , wherein the control system is configured to control the variable motive force applied to the turbine by the generator to control the flow rate of the gaseous stream of second reactant based on an operating condition of the engine such that an exhaust stream temperature is maintained below a temperature limit.

6. The powerplant of claim 4 , wherein the generator is configured to operate as an electric motor, and wherein the control system is configured to restart the engine in at least some ambient conditions by controlling the variable motive force applied to the turbine by the generator such that the compressor is driven at a speed that provides for the gaseous stream of second reactant to be provided to the engine at a flow rate at or above a threshold level.

7. The powerplant of claim 6 , wherein the control system is configured to control the variable motive force applied to the turbine by the generator to control the flow rate of the gaseous stream of second reactant based on an operating condition of the engine such that an exhaust stream temperature is maintained below a temperature limit.

8. A powerplant, comprising:
a fuel cell configured to react a first reactant with a gaseous stream of second reactant to produce energy and an exhaust stream;
a compressor configured to pressurize the gaseous stream of second reactant supplied to the power generation system;
a turbine, wherein the compressor is driven in rotation by a driving force from the turbine, and wherein the turbine is propelled by the exhaust stream;
a catalytic afterburner in the exhaust stream intermediate the power generation system and the turbine, the afterburner being configured to react reactants in the exhaust stream; and
a control system configured to control the operation of the afterburner to power the turbine at a rate such that the compressor is driven at a speed that provides for the gaseous stream of second reactant to be provided to the power generation system at a flow rate appropriate to a rate at which the second reactant is being provided to the power generation system.

9. A powerplant, comprising:
an engine configured to react a first reactant with a gaseous stream of second reactant to produce energy and an exhaust stream;
a compressor configured to pressurize the gaseous stream of second reactant supplied to the power generation system;
a turbine, wherein the compressor is driven in rotation by a driving force from the turbine, and wherein the turbine is propelled by the exhaust stream;
an afterburner in the exhaust stream intermediate the power generation system and the turbine, the afterburner being configured to react reactants in the exhaust stream; and
a control system configured to control the operation of the afterburner to power the turbine during a system cold start based on the temperature of the turbine.

Assignees

• Aerovironment Inc

Inventors

• Brooks Alexander Nelson
• Daley James Gallagher

Classifications

• F02D41/0025

  Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures · CPC title

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

• F02D41/1446

  the characteristics being exhaust temperatures · CPC title

• B60W2710/0644

  Engine speed · CPC title

• Y02T10/32

  Cross-Sectional Technologies · mapped topic