Method and systems for an energy recovery and energy converting unit for an engine
Various methods and systems are provided for generating exhaust energy and converting exhaust energy to electrical energy while an engine is not running. In one example, a system for an engine comprises: a first turbocharger including a first compressor driven by a first turbine, the first turbine disposed in an exhaust of the engine; a fuel burner fluidly coupled to the exhaust upstream of the first turbine; a generator coupled to one of the first turbine or an auxiliary, second turbine fluidly coupled to the exhaust downstream of the fuel burner; and one or more bypass valves configured to adjust a flow of air that bypasses the engine and is delivered to the fuel burner.
1. A method, comprising:
burning fuel with a fuel burner within an exhaust system to generate burner exhaust when an engine is not operating, the exhaust system receiving bypass air flow from an engine bypass passage, and the engine bypass passage extending between an intake passage and an exhaust passage and bypassing the engine when the engine is not operating;
rotating a turbine of a turbocharger with at least the burner exhaust, wherein the turbocharger is coupled to a generator or an alternator;
generating electricity with the generator or the alternator in response to the turbine being rotated by the burner exhaust; and
supplying generated electricity from the generator or the alternator to an electrical load.
2. The method of claim 1 , further comprising determining to shut down the engine in response to a demanded power level of the engine being below a threshold and based on one or more of an electrical demand from one or more electrical components and an amount of electrical energy stored at the generator.
3. The method of claim 1 , further comprising, after shutting down the engine, starting either the turbine or an auxiliary turbine coupled with the generator via energy stored at the generator.
4. The method of claim 1 , further comprising, before shutting down the engine, starting either the turbine or an auxiliary turbine coupled with the generator using exhaust energy produced at the engine.
5. The method of claim 1 , further comprising, while the engine is not operating but hot, adjusting a flow of air through the engine bypass passage fluidly coupled between the intake passage and the exhaust passage of the engine to flow air to burn in the fuel burner; and
determining an amount of air flow adjustment and an amount of fuel injected to a burner based on an electrical demand of one or more electrical components.
6. The method of claim 1 , further comprising, when the engine is operating, flowing exhaust gas to the turbine and, in response to a speed of the turbine being greater than desired for a torque demand, recovering exhaust energy via the generator.
7. The method of claim 6 , further comprising, in response to the speed of the turbine being less than desired for the torque demand, supplying energy from the generator to the turbine to increase the speed of the turbine.
8. A method, comprising:
flowing bypass air flow through a bypass passage when an engine is off, and the bypass passage bypasses the engine,
burning fuel with a fuel burner to generate burner exhaust when the engine is not operating, and the fuel burner receiving the bypass air flow;
rotating a turbine of a turbocharger with at least the burner exhaust, wherein the turbocharger is coupled to a generator or an alternator;
generating electricity with the generator or the alternator in response to the turbine being rotated by the burner exhaust.
9. The method of claim 8 , wherein the fuel is burned within the bypass passage.
10. The method of claim 8 , wherein the fuel is burned within a second bypass passage.
11. The method of claim 8 , further comprising flowing the bypass air into an exhaust passage of the engine, and
wherein the fuel is burned within the exhaust passage when the engine is off.
12. The method of claim 8 , further comprising closing a bypass valve to prevent flow through the bypass passage when the engine is operating.
13. The method of claim 8 , further comprising supplying electrical energy to one or more electrical components, and
wherein the electrical energy is produced by rotating the turbine of the turbocharger with the burner exhaust when the engine is not operating.