Seal assembly for a pressurized fuel feed system for an internal combustion engine
View Patent ↗The seal assembly comprises providing a fuel conduit having a fluid flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction with a first sealing surface disposed on the fuel conduit. A second sealing surface engages with the first sealing surface, such as to provide a fluid-tight connection preventing pressurized gas from leaving the fluid flow passage. The said first and second sealing surfaces are substantially perpendicular to the general fluid-flow direction. An o-ring is disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection. Preferably the o-ring is subjected to a squeeze of at least 40%, more preferably 50%, when the first and second sealing surfaces are coupled together. The sealing arrangement is most advantageously applied to throttle assemblies and the like, in particular for use with low-speed, gaseous fueled engines.
1. A fuel supply system for supplying a pressurized gaseous fuel to a low speed internal combustion engine comprising:
a fuel conduit having a fluid flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction;
a first sealing surface disposed on the fuel conduit;
a second sealing surface engaged with and parallel to the first sealing surface, to provide a fluid-tight connection preventing pressurized gas from leaving the fluid flow passage;
said first and second sealing surfaces are substantially perpendicular to the general fluid-flow direction;
an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection;
wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 30% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
2. The fuel supply system as claimed in claim 1 , wherein the o-ring extends around the fuel conduit.
3. The fuel supply system as claimed in claim 1 , wherein the fuel conduit is a throttle body.
4. The fuel supply system as claimed in claim 3 , wherein the second sealing surface is formed on a cover plate mounted over an opening in the throttle body.
5. The fuel supply system as claimed in claim 3 , further comprising an actuator for the throttle, wherein the second sealing surface is formed on the actuator.
6. The fuel supply system as claimed in claim 1 , wherein the first sealing surface is formed on a flange extending from the fuel conduit.
7. The fuel supply system as claimed in claim 1 , wherein the o-ring is located in a groove.
8. The fuel supply system as claimed in claim 7 , wherein the groove is formed in the first sealing surface.
9. The fuel supply system as claimed in claim 1 , wherein the o-ring between the first sealing surface and second sealing surface has a thickness that is at least 40% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
10. The fuel supply system as claimed in claim 9 , wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 50% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
11. A throttle for a fuel supply system of a low speed internal combustion engine, the fuel supply system supplying a pressurized normally gaseous fuel to the engine, the throttle comprising:
a throttle body having a pressurized fuel gas flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction;
a first sealing surface disposed on the throttle body;
a second sealing surface engaged with and parallel to the first sealing surface, to provide a fluid-tight connection preventing pressurized gas from leaving the pressurized fuel gas flow passage;
an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection, wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 30% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
12. The throttle as claimed in claim 11 , wherein the first and second sealing surfaces extend substantially perpendicular to the general fluid-flow direction.
13. The throttle as claimed in claim 12 , wherein the o-ring extends around the pressurized fuel gas flow passage.
14. The throttle as claimed in claim 11 , wherein the second sealing surface is formed on a cover plate mounted over an opening in the throttle body.
15. The throttle as claimed in claim 11 , further comprising an actuator for the throttle, wherein the second sealing surface is formed on the actuator.
16. The throttle as claimed in claim 11 , wherein the first sealing surface is formed on a flange extending from the throttle body.
17. The throttle as claimed in claim 11 , wherein the o-ring is located in a groove.
18. The throttle as claimed in claim 17 , wherein the groove is formed in the first sealing surface.
19. The throttle as claimed in claim 11 , wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 40% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
20. The throttle as claimed in claim 19 , wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 50% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
21. A low speed, pressurized gaseous fuel internal combustion engine comprising:
a pressurized fuel gas feed system for supplying pressurized gaseous fuel to an inlet of the internal combustion engine;
the pressurized fuel gas feed system comprising a throttle for regulating the flow of pressurized gaseous fuel to the internal combustion engine;
the throttle comprising a throttle body having a pressurized fuel gas flow passage therethrough for conveyance of the pressurized gaseous fuel in a general fluid-flow direction;
a first sealing surface disposed on the throttle body;
a second sealing surface engaged with the first sealing surface, to provide a fluid-tight connection preventing pressurized gaseous fuel from leaving the fluid flow passage;
an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection, wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 30% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
22. The internal combustion engine as claimed in claim 21 , wherein the first and second sealing surfaces extend substantially perpendicular to the general fluid-flow direction.
23. The internal combustion engine as claimed in claim 22 , wherein the o-ring extends around the fluid flow passage.
24. The internal combustion engine as claimed in claim 21 , wherein the second sealing surface is formed on a cover plate mounted over an opening in the throttle body.
25. The internal combustion engine as claimed in claim 21 , further comprising an actuator for the throttle, wherein the second sealing surface is formed on the actuator.
26. The internal combustion engine as claimed in claim 21 , wherein the first sealing surface is formed on a flange extending from the throttle body.
27. The internal combustion engine as claimed in claim 21 , wherein the o-ring is located in a groove.
28. The internal combustion engine as claimed in claim 27 , wherein the groove is formed in the first sealing surface.
29. The internal combustion engine as claimed in claim 21 , wherein the o-ring when acted upon by the first and second sealing surfaces has a thickness that is at least 40% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.
30. The internal combustion engine as claimed in claim 21 , wherein the o-ring provides a seal under an operating pressure for the pressurized gaseous fuel of up to 100 psi.
31. A system, comprising:
an internal combustion engine having a pressurized gaseous fuel source;
a fuel conduit having a fluid flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction;
a first sealing surface disposed on the fuel conduit;
a second sealing surface engaged with the first sealing surface, to provide a fluid-tight connection preventing pressurized gas from leaving the fluid flow passage;
said first and second sealing surfaces being substantially perpendicular to the general fluid-flow direction; and
an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection, wherein the o-ring is at least partially disposed in a groove located on the first sealing surface and a further groove located on the second sealing surface, the o-ring when acted upon by the first and second sealing surfaces having a thickness that is at least 30% less than the thickness of the o-ring when not acted upon by the first and second sealing surfaces.