Assembly comprising a heat engine and an electric compressor

US9657688B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9657688-B2
Application numberUS-201314406756-A
CountryUS
Kind codeB2
Filing dateJun 6, 2013
Priority dateJun 11, 2012
Publication dateMay 23, 2017
Grant dateMay 23, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to an assembly ( 1 ) comprising: an admission circuit ( 4 ) extending between an air inlet ( 11 ) and an outlet connected to the inlet of a heat engine ( 2 ); an exhaust circuit ( 6 ) extending between an inlet connected to the outlet of the heat engine ( 2 ) and an exhaust gas outlet ( 13 ); said heat engine ( 2 ); a return loop ( 22 ) enabling all or some of the exhaust gases in the exhaust circuit ( 6 ) to be reinjected upstream of the heat engine ( 2 ); and an electric compressor ( 30 ) arranged in the assembly ( 1 ) in such a way as to be able to receive gases recirculating in the return loop ( 22 ).

First claim

Opening claim text (preview).

The invention claimed is: 1. An assembly comprising: an intake circuit extending between an air inlet and an outlet connected to the inlet of a heat engine, wherein the intake circuit comprises a mechanical compressor; an exhaust circuit extending between an inlet connected to the outlet of the heat engine and an exhaust gas outlet, wherein the exhaust circuit comprises a turbine; said heat engine; a return loop allowing all or some of the exhaust gases in the exhaust circuit to be reinjected upstream of the heat engine, and an electric compressor, the electric compressor being located in the assembly so as to be able to receive gases recirculating through the return loop, the electric compressor being located in the intake circuit, the return loop having: a first outlet opening into the intake circuit upstream of the electric compressor, a second outlet opening into the intake circuit downstream of the electric compressor and upstream of the manifold admitting gases into the combustion chamber of the heat engine, and an inlet downstream of the turbine and corresponding outlets upstream of the mechanical compressor. 2. The assembly as claimed in claim 1 , the first and second outlets of the return loop being the only outlets of this return loop. 3. The assembly as claimed in claim 1 , the intake circuit comprising a bypass branch starting upstream of the electric compressor and opening downstream of the electric compressor. 4. The assembly as claimed in claim 3 , the system of valves also being configured to direct gases originating from the inlet of the intake circuit into the bypass branch or into the electric compressor. 5. The assembly as claimed in claim 1 , comprising a system of valves which is configured to direct gases recirculating in the return loop toward the first or the second outlet of said loop. 6. A method for controlling an assembly, the assembly comprising: an intake circuit extending between an air inlet and an outlet connected to the inlet of a heat engine; an exhaust circuit extending between an inlet connected to the outlet of the heat engine and an exhaust gas outlet; said heat engine; a return loop allowing at least a portion of the exhaust gases in the exhaust circuit to be reinjected upstream of the heat engine, and an electric compressor, the electric compressor being located in the assembly so as to be able to receive gases recirculating through the return loop, the electric compressor being located in the intake circuit, the return loop having: a first outlet opening into the intake circuit upstream of the electric compressor, and a second outlet opening into the intake circuit downstream of the electric compressor and upstream of the manifold admitting gases into the combustion chamber of the heat engine, wherein the method comprises: during a transient phase, activating the electric compressor and using the electric compressor to compress at least a portion of the gases recirculating in the return loop. 7. The method as claimed in claim 6 , wherein the electric compressor also receives gases originating from the inlet of the intake circuit, and wherein the electric compressor compresses said gases also. 8. The method as claimed in claim 6 , wherein the transient phase is followed by a steady-state phase in which the assembly is controlled in such a way that the electric compressor is not supplied with gases recirculating in the return loop or with gases originating from the inlet of the air intake circuit. 9. The method as claimed in claim 8 , wherein the electric compressor is deactivated during the steady-state phase. 10. The method as claimed in claim 6 , wherein the electric compressor is driven by a variable-reluctance motor. 11. An assembly comprising: an intake circuit extending between an air inlet and an outlet connected to the inlet of a heat engine, wherein the intake circuit further comprises a mechanical compressor; an exhaust circuit extending between an inlet connected to the outlet of the heat engine and an exhaust gas outlet, wherein the exhaust circuit further comprises a turbine; said heat engine; a return loop allowing all or some of the exhaust gases in the exhaust circuit to be reinjected upstream of the heat engine, and an electric compressor, the electric compressor being located in the assembly so as to be able to receive gases recirculating through the return loop, the electric compressor being located in the intake circuit, wherein the electric compressor is configured to activate during a transient phase and compress at least a portion of the gases recirculating in the return loop, the return loop having: a first outlet opening into the intake circuit upstream of the electric compressor, a second outlet opening into the intake circuit downstream of the electric compressor and upstream of the manifold admitting gases into the combustion chamber of the heat engine, and an inlet downstream of the turbine and its outlets upstream of the mechanical compressor.

Assignees

Inventors

Classifications

  • Improving ICE efficiencies · CPC title

  • the substances including exhaust gas · CPC title

  • F02M26/06Primary

    Low pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust downstream of the turbocharger turbine and reintroduced into the intake system upstream of the compressor · CPC title

  • Cross-Sectional Technologies · mapped topic

  • electric · CPC title

Patent family

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Frequently asked questions

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What does patent US9657688B2 cover?
The invention relates to an assembly ( 1 ) comprising: an admission circuit ( 4 ) extending between an air inlet ( 11 ) and an outlet connected to the inlet of a heat engine ( 2 ); an exhaust circuit ( 6 ) extending between an inlet connected to the outlet of the heat engine ( 2 ) and an exhaust gas outlet ( 13 ); said heat engine ( 2 ); a return loop ( 22 ) enabling all or some of the exhaust …
Who is the assignee on this patent?
Valeo Systemes De Controle Moteur, Valeo Systemes De Controle Moteur
What technology area does this patent fall under?
Primary CPC classification F02M26/06. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 23 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).