Internal combustion engine
US-2024003313-A1 · Jan 4, 2024 · US
US10344705B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10344705-B2 |
| Application number | US-201615296425-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 18, 2016 |
| Priority date | Oct 18, 2016 |
| Publication date | Jul 9, 2019 |
| Grant date | Jul 9, 2019 |
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An engine has a cylinder head defining an intake port with a roof defining first and second valve guide bores upstream of first and second siamesed intake valve seats for a cylinder. The head has first and second asymmetric fairings extending outwardly from the roof and positioned directly upstream of respective bores. Each fairing has an inner wall intersecting an outer wall along an upstream edge and an inclined planar roof wall extending between the inner and outer walls. A method of forming the cylinder head and engine is also provided by milling the fairings from a roof preform formed with the intake port of the head.
Opening claim text (preview).
What is claimed is: 1. An engine comprising: a head defining an intake port with a roof defining first and second valve guide bores upstream of first and second siamesed intake valve seats for a cylinder; and first and second fairings extending outwardly from the roof and positioned directly upstream of respective bores, each fairing with: an inner wall intersecting an outer wall along an upstream edge, a downstream guide wall intersecting the inner and outer walls and positioned upstream of the associated bore, and an inclined planar roof wall extending between the inner and outer walls and the guide wall, wherein the roof wall is inclined towards the associated inner wall of each respective fairing. 2. The engine of claim 1 wherein a length of the inner wall is less than a length of the outer wall for each fairing; and wherein each fairing is asymmetric. 3. The engine of claim 1 wherein the inner walls of the first and second fairings face one another. 4. The engine of claim 1 wherein, for each fairing, the inner wall is oriented at a first angle relative to the surrounding roof and the outer wall is oriented at a second angle relative to the surrounding roof, the first angle less than the second angle such that the inner wall is steeper than the outer wall. 5. The engine of claim 1 wherein the inner and outer walls of each fairing are planar, and an angle formed between the inner and outer walls of each fairing is an acute angle. 6. The engine of claim 1 wherein the roof wall is inclined towards the associated upstream edge of each respective fairing. 7. The engine of claim 1 wherein the roof wall is spaced apart from and nonintersecting with the surrounding roof of the intake port. 8. The engine of claim 1 wherein the guide wall is concave. 9. The engine of claim 1 wherein the roof wall is substantially triangular. 10. The engine of claim 1 wherein the guide wall of the fairing is concentric with a respective guide bore. 11. The engine of claim 1 wherein a distance between the inner and outer walls of each fairing at a downstream end of the fairing is less than a diameter of an associated guide bore. 12. The engine of claim 1 further comprising first and second valve guides positioned within the first and second valve guide bores, respectively; wherein each valve guide extends into the intake port to a plane containing the associated roof wall. 13. The engine of claim 1 wherein the first and second fairings are mirror symmetric to one another with respect to a plane extending through a bridge between the siamesed ports and a mounting flange for an intake manifold. 14. The engine of claim 1 wherein each of the first and second fairings is integrally formed with the cylinder head. 15. The engine of claim 1 wherein the roof wall of each fairing is contained within a plane extending between the associated inner and outer walls. 16. A cylinder head comprising: a member defining an intake port extending from an intake manifold mounting flange to first and second intake siamesed intake valve ports separated by a valve bridge, a roof of the intake port defining first and second v-shaped fairings upstream of and directly adjacent to first and second valve guide bores; wherein each fairing has a planar inner wall and a planar outer wall extending outwardly from an adjacent surface of the roof, the inner and outer walls intersecting along an upstream edge of each fairing, a length of the outer wall being greater than a length of the inner wall for each fairing, the inner walls of the first and second fairings facing one another; wherein each fairing has a downstream guide wall positioned upstream of the associated bore, extending outwardly from the adjacent roofsurface, and extending between and intersecting the inner and outer side walls, the guide wall shaped to be concentric with the associated bore; wherein each fairing has a planar roof wall extending between the inner and outer side walls and the guide wall, each roof wall inclined towards the upstream edge of the associated fairing, and each roof wall inclined towards the inner wall of the associated fairing; and wherein each fairing is asymmetric. 17. The head of claim 16 wherein the first and second fairings are mirror symmetric with respect to one another about a plane extending through the bridge and the mounting flange. 18. An engine comprising: a head defining first and second fairings extending outwardly from a roof of an intake port for a cylinder, the first and second fairings positioned entirely upstream of first and second valve guide bores associated with first and second siamesed intake valve seats, each fairing having a roof wall contained within an inclined plane and extending between inner and outer walls, the inner and outer walls intersecting along an upstream edge; wherein the roof wall of each respective fairing is inclined towards the associated upstream edge and towards the associated inner wall.
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