Gaseous fuel mixer assembly for engine and engine system operating method

US11236705B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11236705-B2
Application numberUS-202016912300-A
CountryUS
Kind codeB2
Filing dateJun 25, 2020
Priority dateJun 25, 2020
Publication dateFeb 1, 2022
Grant dateFeb 1, 2022

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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 gaseous fuel mixer assembly for an engine includes a mixer housing forming gas delivery openings, and positioned to extend across a flow path formed by an intake conduit for the engine. A spool valve is within a central bore in the mixer housing and includes gas distribution openings selectively connectable to the gas delivery openings by moving the spool valve within the mixer housing using a piezoelectric actuator coupled with the spool valve by way of a pivot arm. Sealing lands of the spool valve are in an alternating arrangement with the gas distribution openings, such that at the closed position the sealing lands block the gas distribution openings from the gas delivery openings, and at the open position the respective openings are fluidly connected.

First claim

Opening claim text (preview).

What is claimed is: 1. A gaseous fuel mixer assembly for an engine comprising: a mixer housing defining a longitudinal axis and including an inner housing surface forming a central bore, an outer housing surface, and gas delivery openings fluidly connected to the central bore and extending to the outer housing surface; the gas delivery openings form gas outlet locations having a circumferential distribution and an axial distribution in the outer housing surface, and gas inlet locations having an axial distribution in the inner housing surface; a spool valve within the central bore and including an inner valve surface forming a gas supply passage, an outer valve surface, gas distribution openings fluidly connected to the gas supply passage and extending to the outer valve surface, and sealing lands extending circumferentially around the longitudinal axis; a spool valve electrical actuator coupled with the spool valve to move the spool valve in axial directions between an open position and a closed position relative to the gas inlet locations; and the sealing lands are in an alternating arrangement with the gas distribution openings, relative to the longitudinal axis, and have an axial distribution matched to the axial distribution of the gas inlet locations, such that at the closed position the sealing lands block the gas distribution openings from the gas delivery openings, and at the open position the gas distribution openings are fluidly connected to the gas delivery openings; an intake structured to fluidly connect to a cylinder in an engine, and forming a flow path for intake gases extending between an air inlet and an intake port for feeding the intake gases into the cylinder, the mixer housing supported in the intake conduit and extending across the flow path. 2. The mixer assembly of claim 1 wherein the spool valve electrical actuator includes a piezoelectric actuator stack. 3. The mixer assembly of claim 2 wherein the spool valve electrical actuator further includes a pivot arm, a first pusher coupled between the pivot arm and the piezoelectric actuator stack, and a second pusher coupled between the pivot arm and the spool valve. 4. The mixer assembly of claim 3 wherein the pivot arm is a lever arm pivotable about a pivot point closer to the first pusher than to the second pusher, such that a displacement of the spool valve is amplified relative to a displacement of the piezoelectric actuator stack responsive to energizing of the piezoelectric actuator stack. 5. The mixer assembly of claim 1 wherein the mixer housing has a major diameter (x) and a minor diameter (y), in an axial section plane, such that an aspect ratio of the mixer housing is x:y, where x=1 and y<1. 6. The mixer assembly of claim 5 wherein the aspect ratio of the mixer housing is x:y, where x=1 and y≤0.25. 7. The mixer assembly of claim 5 wherein the outer housing surface is profiled to form an oval shape, in an axial section plane. 8. The mixer assembly of claim 7 wherein the oval shape forms opposite end curves, in an axial section plane, and the major diameter intersects each of the opposite end curves at the gas outlet locations. 9. The mixer assembly of claim 1 wherein at least one of the gas distribution openings or the gas delivery openings include grooves in the respective inner housing surface and outer valve surface. 10. The mixer assembly of claim 9 wherein each of the gas distribution openings and the gas delivery openings include grooves in the respective inner housing surface and outer valve surface that are fully circumferential of the longitudinal axis. 11. The mixer assembly of claim 1 wherein: the spool valve includes a first axial end surface and a second axial end surface; the spool valve electrical actuator is coupled with the first axial end surface; and the mixer assembly further includes a biaser held captive between the second axial end surface and the mixer housing. 12. An engine system comprising: an intake conduit structured to fluidly connect to a cylinder in an engine, and forming a flow path for intake gases extending between an air inlet, and an intake port for feeding the intake gases into the cylinder; a gaseous fuel mixer assembly including a mixer housing supported in the intake conduit and extending across the flow path, the mixer housing forming a central bore and gas delivery openings opening to the flow path and fluidly connected to the central bore; the mixer housing defining a longitudinal axis, and the gas delivery openings having a circumferential distribution and an axial distribution in the mixer housing; the gaseous fuel mixer assembly further including a spool valve within the central bore, the spool valve forming a gas supply passage and gas distribution openings fluidly connected to the gas supply passage; and the gaseous fuel mixer assembly further including a spool valve electrical actuator coupled with the spool valve to move the spool valve in axial directions between an open position where the gas distribution openings are fluidly connected to the gas delivery openings, and a closed position where the spool valve blocks the gas distribution openings from the gas delivery openings; sealing lands extending circumferentially around the longitudinal axis of the mixer housing; the sealing lands are in an alternating arrangement with the gas distribution openings, relative to the longitudinal axis, and have an axial distribution matched to the axial distribution of the as inlet locations, such that at the closed position the sealing lands block the gas distribution openings from the gas delivery openings, and at the open position the gas distribution openings are fluidly connected to the gas delivery openings. 13. The engine system of claim 12 wherein the mixer housing extends fully across the flow path and is supported at opposite mixer housing ends in contact with the intake conduit. 14. The engine system of claim 12 wherein the spool valve electrical actuator includes a pivot arm coupled with the spool valve. 15. The engine system of claim 14 wherein the spool valve electrical actuator further includes a piezoelectric actuator stack, and the pivot arm is coupled with the piezoelectric actuator stack and pivots about a pivot point between the piezoelectric actuator stack and the spool valve. 16. The engine system of claim 12 wherein: the mixer housing includes an outer housing surface profiled to form an oval shape, in an axial section plane, having a major diameter oriented parallel to a flow direction of the flow path; and the oval shape forms opposite end curves, and the gas delivery openings are intersected by the opposite end curves. 17. The engine system of claim 12 wherein the gas distribution openings include grooves that are circumferential of the longitudinal axis. 18. A method of operating an engine system comprising: conveying intake air through a flow path in an intake conduit to an intake port fluidly connected to a cylinder in an engine; energizing a spool valve electrical actuator coupled with a spool valve in a gaseous fuel mixer assembly extending across the flow path in the intake conduit; moving the spool valve from a closed position to an open position in a mixer housing of the gaseous fuel mixer assembly, such that a gas supply passage in the spool valve is fluidly connected to gas delivery openings in the mixer housing having a circumferential distribution and an axial distribution relative to a longitudinal axis of the mixer housing, sealing lands extending circumferentially around the longitudinal axis of the m

Assignees

Inventors

Classifications

  • Use of alternative fuels, e.g. biofuels · CPC title

  • Mixing gases with gases · CPC title

  • being adjustable · CPC title

  • Perforated, multi-opening, with a plurality of holes · CPC title

  • Hydrocarbon fuels, e.g. methane or acetylene · CPC title

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What does patent US11236705B2 cover?
A gaseous fuel mixer assembly for an engine includes a mixer housing forming gas delivery openings, and positioned to extend across a flow path formed by an intake conduit for the engine. A spool valve is within a central bore in the mixer housing and includes gas distribution openings selectively connectable to the gas delivery openings by moving the spool valve within the mixer housing using …
Who is the assignee on this patent?
Caterpillar Inc
What technology area does this patent fall under?
Primary CPC classification F02M21/0254. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 01 2022 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).