Turbine assembly for an internal combustion engine

US12012888B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12012888-B2
Application numberUS-202318454887-A
CountryUS
Kind codeB2
Filing dateAug 24, 2023
Priority dateAug 25, 2022
Publication dateJun 18, 2024
Grant dateJun 18, 2024

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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

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A turbine assembly for an internal combustion engine having: a first turbine that rotates around a first rotation axis and is configured to rotate due to the thrust exerted by exhaust gases emitted by the internal combustion engine; a second turbine which is independent of and separate from the first turbine, rotates around a second rotation axis parallel to and spaced from the first rotation axis, and is configured to rotate due to the thrust exerted by exhaust gases emitted by the internal combustion engine; an electric generator operated by the first turbine; and a transmission device that connects both the turbines to the same electric generator.

First claim

Opening claim text (preview).

The invention claimed is: 1. A turbine assembly ( 42 ) for an internal combustion engine ( 5 ) and comprising: a first turbine ( 43 ), which rotates around a first rotation axis ( 55 ) and is configured to rotate due to a thrust exerted by exhaust gases emitted by the internal combustion engine ( 5 ); a second turbine ( 43 ) which is independent and separate from the first turbine ( 43 ), rotates around a second rotation axis ( 55 ) and is configured to rotate due to the thrust exerted by exhaust gases emitted by the internal combustion engine ( 5 ); an electric generator ( 54 ), which is operated by the first turbine ( 43 ) and by the second turbine ( 43 ); and a transmission device ( 56 ), which connects the both turbines ( 43 ) to the same electric generator ( 54 ) and is configured to give the two turbines ( 43 ) the same rotation speed; wherein the second rotation axis ( 55 ) of the second turbine ( 43 ) is parallel to and spaced from the first rotation axis ( 55 ) of the first turbine ( 43 ). 2. The turbine assembly ( 42 ) according to claim 1 , wherein the transmission device ( 56 ) comprises: two toothed gears, each integral to a shaft of the corresponding turbine ( 43 ) so as to receive the rotary motion from the turbine ( 43 ); and a connection element, which connects the two toothed gears to one another so as to cause the both toothed gears to rotate together and at the same rotation speed. 3. The turbine assembly ( 42 ) according to claim 2 , wherein the toothed gear of the transmission device ( 56 ) is directly constrained to a shaft of the electric generator ( 54 ) so that the electric generator ( 54 ) rotates at the same rotation speed as the two turbines ( 43 ). 4. The turbine assembly ( 42 ) according to claim 2 , wherein the toothed gear of the transmission device ( 56 ) is connected to a shaft of the electric generator ( 54 ) through the interposition of a speed reducer so that the electric generator ( 54 ) rotates at a lower rotation speed than the rotation speed of the two turbines ( 43 ). 5. The turbine assembly ( 42 ) according to claim 2 , wherein the connection element that connects the two toothed gears to each other is a timing belt, a chain, or a gear cascade. 6. The turbine assembly ( 42 ) according to claim 1 , wherein the electric generator ( 54 ) is coaxial to the turbine ( 43 ). 7. The turbine assembly ( 42 ) according to claim 1 , wherein the two turbines ( 43 ) are identical to one another. 8. The turbine assembly ( 42 ) according to claim 1 , wherein the two turbines ( 43 ) are arranged side by side and the two respective rotation axes ( 55 ) are parallel to and spaced apart from one another. 9. The turbine assembly ( 42 ) according to claim 1 , wherein the two turbines ( 43 ) are centrifugal turbines and each have a radial inlet ( 57 ) connected to a respective exhaust duct ( 41 ) and an axial outlet ( 52 ) arranged on the opposite side of the transmission device ( 56 ). 10. A car ( 1 ) comprising: two front wheels ( 2 ); two rear drive wheels ( 4 ); an internal combustion engine ( 5 ), which is provided with a plurality of cylinders ( 18 ), where respective pistons ( 19 ) slide on the inside, and with a drive shaft ( 20 ) connected to the pistons ( 19 ); and a turbine assembly ( 42 ), which is arranged along at least one exhaust duct ( 41 ) of the internal combustion engine ( 5 ) and is manufactured according to claim 1 . 11. The car ( 1 ) according to claim 10 , wherein the internal combustion engine ( 5 ) comprises two exhaust ducts ( 41 ), which originate from the cylinders ( 18 ), go through the turbines ( 43 ) of the turbine assembly ( 42 ) and end in a silencer ( 44 ), which is arranged on a side of the car ( 1 ). 12. The car ( 1 ) according to claim 10 , wherein the internal combustion engine ( 5 ) is longitudinally arranged in a central or rear position and is vertically oriented with the drive shaft ( 20 ) arranged higher than the cylinders ( 18 ).

Assignees

Inventors

Classifications

  • the internal combustion or jet propulsion unit is arranged behind the rear axle · CPC title

  • the internal combustion or jet propulsion unit is arranged between the front and the rear axle · CPC title

  • concerning exhaust · CPC title

  • Arrangement or mounting of internal-combustion or jet-propulsion units (B60K7/00 takes precedence; arrangement or mounting of plural diverse prime-movers for mutual or common propulsion B60K6/00) · CPC title

  • the devices using kinetic energy · CPC title

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What does patent US12012888B2 cover?
A turbine assembly for an internal combustion engine having: a first turbine that rotates around a first rotation axis and is configured to rotate due to the thrust exerted by exhaust gases emitted by the internal combustion engine; a second turbine which is independent of and separate from the first turbine, rotates around a second rotation axis parallel to and spaced from the first rotation a…
Who is the assignee on this patent?
Ferrari Spa
What technology area does this patent fall under?
Primary CPC classification F02B41/10. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 18 2024 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).