This disclosure relates generally to a method and apparatus for controlling fluid flow and, more particularly, to a method and apparatus for controlling the injection of fluid.
Various fuel injection devices have been designed to transmit pressurized fuel through an injection nozzle into a combustion chamber of an engine. Typically, an injection nozzle will have one or more orifices formed in an end thereof, and a selectively movable check member will be arranged inside the nozzle to selectively permit or prevent pressurized fuel from exiting the nozzle through the injection orifices. The geometric configuration of a nozzle-check assembly may significantly impact various injection device characteristics, such as (i) injection device longevity, (ii) injection device cost, (iii) fuel injection repeatability, and (iv) engine exhaust emission levels, for example.
U.S. Patent Application Publication No. US 2003/0057299 A1 discloses a fuel injection nozzle having a nozzle body with at least one injection port therein, and having a nozzle needle that is displaceable within the nozzle body. The nozzle needle has a radial shoulder and, downstream of the shoulder, a circumferential groove that extends to the injection port. The radial shoulder is embodied with very sharp edges, presumably to reduce the effect of production variations. The recited object of the invention disclosed in the '299 publication is to provide reliable fuel metering.
Prior fuel injection devices may be improved by providing novel configurations and methods that effectively balance injection device longevity and cost, injection repeatability, and engine exhaust emissions effects.
The present invention is directed to overcome or improve one or more disadvantages associated with prior devices and methods for controlling the injection of fluid.
In one aspect of the present invention, a fluid injector is disclosed having a nozzle body with first and second body portions and at least one fluid injection orifice within the second body portion. The nozzle body may be configured for transmitting fluid from the first body portion toward the orifice.
The fluid injector may also include a check member movably arranged inside the nozzle body for affecting fluid flow through the orifice and having a contoured outer surface defining (i) a recessed region and (ii) a generally convex region forming at least a portion of the recessed region.
In another aspect of the present invention, a method of supplying fluid to a machine through a fluid injector is disclosed. The method may include transmitting fluid from a first portion of a nozzle body toward at least one fluid injection orifice defined in a second portion of the nozzle body. The method may further include moving a check member arranged within the nozzle body to transmit the fluid past (i) a recessed region about the outer surface of the check member and (ii) a generally convex outer surface of the check member forming at least a portion of the recessed region.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate exemplary embodiments or features of the invention and, together with the description, serve to explain the principles of the invention. In the drawings,
Although the drawings depict exemplary embodiments or features of the present invention, the drawings are not necessarily to scale, and certain features may be exaggerated in order to better illustrate and explain the present invention. The exemplifications set out herein illustrate exemplary embodiments or features of the invention and such exemplifications are not to be construed as limiting the scope of the invention in any manner.
Reference will now be made in detail to embodiments or features of the invention, examples of which are illustrated in the accompanying drawings. Wherever possible, the same or corresponding reference numbers will be used throughout the drawings to refer to the same or corresponding parts.
Referring now to
In one embodiment, the nozzle tip 26 has a generally curved internal wall 34 at an end portion 36 of the nozzle body 14. For example, the generally curved internal wall 34 shown in
The check member 18 may be movably arranged within the nozzle body 14. For example, the check member 18 may be biased via a spring (not shown) toward the internal wall 34 of the nozzle body 14 and held in a first position (as shown in
With reference to
The recessed region 46 may define a circumferential groove 48 about the check member 18. The recessed region 46 includes a bottom portion 50, which is the deepest part of the recessed region 46 (for example, the part of the recessed region 46 of
In one embodiment, the recessed region 46 (such as in the form of the groove 48) may be configured with a volume equal to or less than about 0.2 mm3. For example, in an exemplary embodiment, the recessed region 46 may be configured with a volume within a range of about 0.2 mm3 to about 0.07 mm3, such as a volume of about 0.15 mm3 or a volume of about 0.075 mm3.
The outer surface 42 of the check member 18 may define a generally convex region, the center of which is generally indicated at R1 of
The outer surface 42 of the check member 18 may further define another generally convex region R2 disposed upstream of the generally convex region R1 and having a different curvature than the generally convex region R1. For example, the generally convex region R2 may have a lesser degree of curvature than the generally convex region R1. In the embodiment of
The outer surface 42 of the check member 18 may define yet another generally convex region R3 disposed upstream of the generally convex region R2, between the generally cylindrical outer surface 54 of the check member 18 and the generally convex region R2. The generally convex region R3 has a different curvature than the generally convex region R2. For example, the generally convex region R3 may have a greater degree of curvature than the generally convex region R2.
The outer surface 42 of the check member 18 may define another generally convex region R4 disposed downstream of the bottom portion 50 of the recessed region 46, between the bottom portion 50 of the recessed region 46 and an end portion 58 of the check member 18. The generally convex region R4 may be interconnected with and adjacent the recessed region 46. In one embodiment, the generally convex region R4 forms a downstream beginning of the recessed region 46 and extends into the recessed region 46.
The outer surface 42 of the check member 18 may define yet another generally convex region R5 disposed downstream of the generally convex region R4, between the generally convex region R4 and the end portion 58 of the check member 18. The generally convex region R5 has a different curvature than the generally convex region R4. For example, the generally convex region R5 may have a lesser degree of curvature than the generally convex region R4.
The outer surface 42 of the check member 18 may also define a generally concave region RA disposed downstream of the generally convex region R1, for example between the generally convex regions R1 and R4. The generally concave region RA may be adjacent and interconnected with the generally convex region R1 and may define a portion of the recessed region 46. In the embodiment of
The outer surface 42 of the check member 18 may define another generally concave region RB disposed downstream of the generally concave region RA, between the generally concave region RA and the end portion 58 of the check member 18. More specifically, the generally concave region RB may be disposed downstream of the generally convex region R5 between the generally convex region R5 and the end portion 58 of the check member 18.
The check member 18 may also include a generally curved region 62 at the end portion 58 of the check member 18. Moreover, the generally curved region 62 may have a contour that substantially matches the contour of the generally curved internal wall 34 of the tip 26. For example, the embodiment of
This disclosure provides an apparatus and method for controlling the injection of fuel into an engine. The apparatus described herein is predicted to facilitate repeatable, reliable injection performance with enhanced longevity while balancing engine emissions and cost effects. It should be appreciated that the components and arrangements described herein may be applied by one skilled in the art to various injector designs, including but not limited to an electronically controlled unit injector, a hydraulically-actuated electronically controlled unit injector, a mechanically-actuated injector, or an injector coupled with a pump and line fuel system, for example.
One skilled in the art would appreciate that the check member 18 may be moved to a flow blocking position (
In a flow blocking position (
In the flow blocking position, a chamber volume 66, or sac volume, exists between the end portion 58 of the check member 18 and the end portion 36 of the nozzle body 14. The generally curved region 62 of the check member 18 may be arranged within the chamber volume 66 such that the chamber volume 66 is bounded, at least in part, by the generally curved region 62 of the check member 18 and the generally curved wall 34 of the nozzle body 14.
In one embodiment, the chamber volume 66 may be configured with a volume equal to or less than about 0.7 mm3 when the check member 18 is in a flow blocking position. For example, in an exemplary embodiment, the chamber volume 66 may be configured with a volume within a range of about 0.7 mm3 to about 0.3 mm3, such as a volume of about 0.67 mm3 or a volume of about 0.35 mm3.
When the check member 18 is moved to a flow passing position (
In a flow passing position, the generally convex regions R1, R2 may be disposed adjacent the injection orifices 30. Moreover, at least a portion of the generally convex regions R1, R2 may be arranged at least slightly upstream of the injection orifices 30 so that the fluid communicates with the generally convex regions R1, R2 prior to entering the orifices 30. Moreover, the bottom portion 50 of the recessed region 46 may also be arranged at least partially upstream of the injection orifices 30 so that the fluid communicates with the bottom portion 50 prior to entering the orifices 30. Thus, as fluid flows downstream from the first body portion 22 of the nozzle body 14 toward the injection orifices 30 past the generally convex region R3, the fluid may approach and flow through a gradually widening channel defined by the wall of the nozzle body 14 and the recessed region 46 of the check member 18 so that the velocity of the fluid is reduced prior to the fluid entering the orifices 30. More specifically, the velocity of the fluid may be reduced as it flows past and fluidly communicates with the generally convex regions R1, R2 of the check member 18 and the recessed region 46 of the check member 18 prior to entering the orifices 30. With a configuration as disclosed herein, pressurized fluid transmitted through the injector is estimated to experience a decrease in fluid separation phenomena proximate or within the orifices 30, thereby decreasing fluid cavitation effects within the tip 26 to ultimately decrease potential damage to the injector and increase the life of the injector. Moreover, increased injection spray uniformity, for example via improved check lift characteristics, is also estimated to result.
The geometrical and structural elements (e.g., one or more of the generally convex regions) described herein are further estimated to facilitate one or more desirable characteristics for fuel injectors, such as providing smooth velocity transition regions and/or uniform pressure distributions within the fuel injector when the injector is in a flow passing state, beneficial management of stresses and pressures generated within the check member 18 during operation of the check member (e.g., resulting from repeated engagement with the nozzle body 14), and improved manufacturability.
From the foregoing it will be appreciated that, although specific embodiments of the invention have been described herein for purposes of illustration, various modifications may be made without deviating from the spirit or scope of the invention. Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and figures and practice of the invention disclosed herein. It is intended that the specification and disclosed examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims and their equivalents. Accordingly, the invention is not limited except as by the appended claims.
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