The present disclosure relates to engine fuel systems, and more specifically to fuel injectors.
This section provides background information related to the present disclosure which is not necessarily prior art.
A fuel injector may include a pressurized fuel supply used to open and close an injection nozzle opening. The injector may include an actuation member and a valve mechanism to selective open and close a leakage path between low pressure and high pressure regions of the injector. Opening the leakage path may reduce a closing biasing force applied to an injection valve to open the injection nozzle opening. When the leakage path is closed, the injection valve may be displaced to close the injection nozzle opening. Thus, the injection nozzle opening is typically in one of two positions, i.e., a closed position or an open position, depending on whether pressurized fuel is being provided to the injection nozzle opening.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
A fuel injector may include a housing, a pintle nozzle assembly and an actuation assembly. The housing may define a longitudinal bore, a high pressure fuel duct in communication with the longitudinal bore and a valve seat including a valve seat surface and an aperture. The valve seat surface may be in communication with the high pressure fuel duct. The aperture may extend through the valve seat surface and be in communication with the longitudinal bore. The pintle nozzle assembly may include a stem and a pintle. The pintle nozzle assembly may be at least partially disposed within the longitudinal bore and be variably displaceable between a first position and a second position. In the first position, the pintle nozzle assembly may abut the valve seat to seal the aperture. In the second position, the pintle nozzle assembly may be displaced from the valve seat to open the aperture. The actuation assembly may be coupled with the pintle nozzle assembly. The actuation assembly may operate to move the pintle nozzle assembly to a plurality of positions between the first position and the second position.
An engine assembly may include an engine structure defining a cylinder and a fuel injector supported by the engine structure and in communication with the cylinder. The fuel injector may include a housing, a pintle nozzle assembly and an actuation assembly. The housing may define a longitudinal bore, a high pressure fuel duct in communication with the longitudinal bore and a valve seat including a valve seat surface and an aperture. The valve seat surface may be in communication with the high pressure fuel duct. The aperture may extend through the valve seat surface and be in communication with the longitudinal bore. The pintle nozzle assembly may include a stem and a pintle. The pintle nozzle assembly may be at least partially disposed within the longitudinal bore and be variably displaceable between a first position and a second position. In the first position, the pintle nozzle assembly may abut the valve seat to seal the aperture. In the second position, the pintle nozzle assembly may be displaced from the valve seat to open the aperture. The actuation assembly may be coupled with the pintle nozzle assembly. The actuation assembly may operate to move the pintle nozzle assembly to a plurality of positions between the first position and the second position.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only and are not intended to limit the scope of the present disclosure in any way.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Examples of the present disclosure will now be described more fully with reference to the accompanying drawings. The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses.
Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.
When an element or layer is referred to as being “on,” “engaged to,” “connected to” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.
Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
Referring to
The fuel system 14 may include a fuel pump 22, a fuel tank 24, a fuel rail 26, fuel injectors 28, a main fuel supply line 30, secondary fuel supply lines 32 and fuel return lines 34. The fuel pump 22 may be in communication with the fuel tank 24 and may provide a pressurized fuel supply to the fuel rail 26 via the main fuel supply line 30. The fuel rail 26 may provide the pressurized fuel to injectors 28 via the secondary fuel supply lines 32. The fuel rail 26 may include a pressure regulating valve 36 that regulates fuel pressure within the fuel rail 26 by returning excess fuel to the fuel tank 24 via a return line 38.
The fuel injectors 28 may each include an actuation assembly 40 in communication with the control module 16. In the present non-limiting example, the fuel injectors 28 may form direct injection fuel injectors where fuel is injected directly into the cylinders 20. The fuel injectors 28 may return excess fuel to the fuel tank 24 via the fuel return lines 34.
Referring to
The housing 50 may further define a valve seat 56 and a nozzle 51. The valve seat 56 may include an aperture 56A and a valve seat surface 56B. The valve seat surface 56B may be in communication with the longitudinal bore 52 and high pressure fuel duct 54. The aperture 56A may extend through the valve seat surface 56B and be in communication with the longitudinal bore 52. The nozzle 51 may extend from the valve seat 56 to a nozzle outlet 57 and be in communication with the valve seat 56 and the longitudinal bore 52.
Fuel injector 28 may include a pintle nozzle assembly 60 disposed within the longitudinal bore 52. The pintle nozzle assembly 60 may include a stem 62 and a pintle 64. The stem 64 may be disposed within the longitudinal bore 52 and the pintle 64 may be disposed within the nozzle 51. In a first position of the pintle nozzle assembly 60, i.e., the closed position, the pintle nozzle assembly 60 may abut the valve seat 56 to seal the aperture 56A. In a second position of the pintle nozzle assembly 60, i.e., the fully opened position, the pintle nozzle assembly 60 may open the aperture 56A to the maximum extent allowed to spray pressurized fuel into the cylinder 20 in which the fuel injector 28 is inserted. The pintle nozzle assembly 60 may be variably displaceable such that the pintle nozzle assembly 60 may be moved to a plurality of positions between the first (closed) position and the second (fully opened) position. In this manner, the pintle nozzle assembly 60 may vary the size of the nozzle opening 55, which provides a variable amount of fuel and/or fuel flow rate to the cylinder 20.
The pintle nozzle assembly 60 may further include a biasing member 68. The biasing member 68 may interact with the pintle nozzle assembly 60, e.g., stem 62, to bias the pintle nozzle assembly 60 to be in the first (closed) position. The biasing member 68 may thus assist the pintle nozzle assembly 60 to seal the aperture 56A. The biasing member 68 may be a compression spring or similar device.
The pintle nozzle assembly 60 may be moved between the first (closed) position and the second (fully opened) position by an actuation assembly 40 coupled thereto. The actuation assembly 40 may be any variable position actuator, for example, a piezoelectric actuator, an electromagnetic actuator, a magnetostrictive actuator, a servo actuator or a solenoid actuator. In a non-limiting example, the actuation assembly 40 is coupled to the stem 62 and operates to move the pintle nozzle assembly 60 between the first (closed) position and second (fully opened) position. As discussed above, the actuation assembly 40 may operate to move the pintle nozzle assembly 60 to a plurality of positions between the first (closed) position and the second (fully opened) position such that the size of the nozzle opening 55 will vary, thus providing a variable amount of fuel and/or fuel flow rate to the cylinder 20.
The housing 50 may further define a low pressure fuel duct 58. The low pressure fuel duct 58 may be in communication within the longitudinal bore 52. During operation of the fuel injector 28, pressurized fuel may travel around the stem 62 from the high pressure fuel duct 54 to the low pressure fuel duct 58. The low pressure fuel duct 58 may be in communication with the fuel return lines 34 such that excess fuel may be returned to the fuel tank 24, as discussed above. The clearance between the stem 62 and the walls of the longitudinal bore 52 may be set as small as practicable to minimize fuel flow between the high pressure fuel duct 54 to the low pressure fuel duct 58. In a non-limiting example, the clearance between the stem 62 and the walls of the longitudinal bore 52 may be set between 0.1 and 4.0 microns, however this clearance may be adjusted for the application and execution of a specific design.
In a non-limiting example, the stem 62 may include a guide member 61 that assists in maintaining the pintle nozzle assembly 60 centered within the longitudinal bore 52 of the housing 50. For example only, referring to
Referring to
In the non-limiting example illustrated in
The valve seat 56 may have a seat angle Θ between ninety degrees and one hundred and eighty degrees to provide a large valve opening 65 with a relatively small amount of lift S. Smaller seat angles Θ (such as, forty degrees to ninety degrees) may also be used if, for example, it is desirable to have a lower injection pressure associated with a relatively small amount of lift S.
Referring to
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3035780 | Peras | May 1962 | A |
4046322 | Knape et al. | Sep 1977 | A |
4213568 | Hofmann | Jul 1980 | A |
4528951 | Yamada | Jul 1985 | A |
4693424 | Sczomak | Sep 1987 | A |
5033679 | Golev et al. | Jul 1991 | A |
5671890 | Cooper et al. | Sep 1997 | A |
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7308169 | Chandrasekhar et al. | Dec 2007 | B2 |
Number | Date | Country |
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1712697 | Dec 2005 | CN |
Number | Date | Country | |
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20110240770 A1 | Oct 2011 | US |