Ejector Integrally Formed with an Intake Air Component and a Method to Manufacture
20180112634 ยท 2018-04-26
Assignee
Inventors
- Steven James Hoffman (Ann Arbor, MI, US)
- John Emley (Canton, MI, US)
- Douglas Scott Sparks (West Bloomfield, MI, US)
- David S. Moyer (Sterling Heights, MI, US)
- Christopher Alan Myers (Holly, MI, US)
- Brandon William Bailey (Milford, MI, US)
- Roger Joseph Khami (Troy, MI, US)
Cpc classification
B29C65/20
PERFORMING OPERATIONS; TRANSPORTING
B29C66/55
PERFORMING OPERATIONS; TRANSPORTING
B29C65/72
PERFORMING OPERATIONS; TRANSPORTING
F02M35/10229
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10321
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C66/534
PERFORMING OPERATIONS; TRANSPORTING
B29C65/48
PERFORMING OPERATIONS; TRANSPORTING
F02M35/10144
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29C45/006
PERFORMING OPERATIONS; TRANSPORTING
F02M35/1036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C66/547
PERFORMING OPERATIONS; TRANSPORTING
B29C66/532
PERFORMING OPERATIONS; TRANSPORTING
F02M35/10157
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10347
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C66/54
PERFORMING OPERATIONS; TRANSPORTING
F02M25/089
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C65/06
PERFORMING OPERATIONS; TRANSPORTING
F02M35/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10118
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M35/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C45/00
PERFORMING OPERATIONS; TRANSPORTING
F02M25/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Vapors in the fuel tank of a vehicle are collected in a carbon canister. An ejector or aspirator is used to purge the carbon canister in a pressure-charged engine in which a positive pressure exists in the intake. A compact ejector includes a substantially planar flange and a venturi tube coupled to the flange with a central axis of the venturi tube substantially parallel to the flange. By manufacturing the ejector in two pieces, dimensions within the ejector: throat, converging section, and diverging section, is more accurate than prior art manufacturing techniques thereby providing better flow characteristics throughout the boost range. By forming one of the two pieces of the ejector integrally with the air intake component in which it is coupled, decreases part count and the number of manufacturing processes.
Claims
1. An ejector system for a boosted internal combustion engine, comprising: a first section of an intake air component having a first ejector portion unitarily formed; and a second ejector portion affixed to the first ejector portion wherein: the first and second ejector portions comprise a venturi tube having a converging section, a throat, and a diverging section; the ejector further comprises a first tube and a second tube; and the second tube fluidly couples to the venturi tube proximate the throat.
2. The ejector system of claim 2, further comprising: a second section of the intake air component affixed to the first section of the intake air component.
3. The ejector system of claim 1 wherein the first and second ejector portions each comprise about one-half of the venturi tube.
4. The ejector system of claim 1 wherein: the first and second tubes are integrally formed with the first ejector portion; and the second tube fluidly couples with an upstream end of the converging section.
5. The ejector system of claim 1 wherein the intake air component an air filter box.
6. The ejector system of claim 1 wherein the intake air component is an intake air duct.
7. The ejector system of claim 1 wherein the center of the venturi tube is substantially parallel to a wall of the intake air component to which it is coupled.
8. An ejector system for a boosted internal combustion engine, comprising: a first section of an intake air component comprising a first ejector portion unitarily formed therewith; a second section of the intake air component affixed to the first section of the intake air component; and a second ejector portion affixed to the first ejector portion wherein: the first and second ejector portions comprise a venturi tube having a diverging section, a throat section, and a converging section; the first and second ejector portions each comprise portions of the diverging, throat, and converging sections.
9. The ejector system of claim 8 wherein the second section of the intake air component is affixed after the second ejector portion is affixed to the first ejector portion.
10. The ejector system of claim 8 wherein first and second intake air components are affixed by one of: sonic welding, vibration welding, induction welding, laser welding, snap fitting, ultrasonic welding, a hot plate, and infrared welding, and thermal welding.
11. The ejector system of claim 8, further comprising: a first tube fluidly coupled to the converging section of the venturi tube; and a second tube fluidly coupled proximate the throat section of the venturi tube wherein the first and second tubes are integrally formed with the first section of the air intake component.
12. The ejector system of claim 8 wherein: the air intake component is an intake air duct; and the first section of the intake air duct and the second section of the intake air duct couple axially.
13. The ejector system of claim 8, wherein first and second ejector portions are affixed by one of: sonic welding, vibration welding, induction welding, laser welding, snap fitting, ultrasonic welding, a hot plate, and infrared welding, and thermal welding.
14. The ejector system of claim 11, wherein a centerline of the first tube forms an acute angle with a surface of the air intake component proximate the first tube.
15. A method to fabricate an air intake component with an ejector, comprising: injection molding a first portion of the air intake component, the air intake component comprising a first venturi tube portion; injection molding a second venturi tube portion; and affixing the first venturi tube portion to the second venturi tube portion.
16. The method of claim 15 wherein: the first and second venturi tube portions are part of the ejector; from upstream to downstream, the venturi tube comprises a converging section, a throat section, and a diverging section; the ejector further comprises first and second tubes that are integrally formed with the first venturi tube portion; the first tube fluidly couples to an upstream end of the converging section; and the second tube fluidly couples proximate the throat section.
17. The method of claim 15 wherein: the first and second venturi tube portions are part of the ejector; from upstream to downstream, the venturi tube comprises a converging section, a throat section, and a diverging section; the ejector further comprises first and second tubes that are integrally formed with the second venturi tube portion; the first tube fluidly couples to an upstream end of the converging section; and the second tube fluidly couples proximate the throat section.
18. The method of claim 15, further comprising: injection molding a second portion of the air intake component; and affixing the second portion of the air intake component to the first portion of the air intake component wherein the affixing of the second portion of the air intake component to the first portion of the air intake component occurs after the first venturi tube portion is affixed to the second venturi tube portion.
19. The method of claim 15 wherein the affixment of the first venturi tube portion to the second venturi tube portion is by one of: sonic welding, vibration welding, induction welding, laser welding, ultrasonic welding, hot plate, and infrared welding, thermal welding, and snap fitting.
20. The method of claim 15 wherein the air intake component is one of an intake air component and an air filter box.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
[0051] As those of ordinary skill in the art will understand, various features of the embodiments illustrated and described with reference to any one of the Figures may be combined with features illustrated in one or more other Figures to produce alternative embodiments that are not explicitly illustrated or described. The combinations of features illustrated provide representative embodiments for typical applications. However, various combinations and modifications of the features consistent with the teachings of the present disclosure may be desired for particular applications or implementations. Those of ordinary skill in the art may recognize similar applications or implementations whether or not explicitly described or illustrated.
[0052] An ejector 150 disclosed in commonly assigned application U.S. Ser. No. 15/225,920 is shown in cross section in
[0053] Ejector 150 of
[0054] In
[0055] Referring back to
[0056] In
[0057] After the ejector is made whole by coupling 412 to the ejector portion in portion 400, a second section 422 of the air duct is coupled to section 400 of the air duct, as shown assembled in
[0058] In an alternative embodiment shown in
[0059] In
[0060] In
[0061] The two pieces of the ejector, one of which is integral with the air intake component, may be coupled by welding. According to an alternative embodiment, the ejector is coupled via a snap fit. In a cross-sectional view in
[0062] In another embodiment in
[0063] According to embodiments of the disclosure, an intake component with an ejector affixed is simplified over prior-art ejectors. Referring to
[0064] Referring now to
[0065] While the best mode has been described in detail with respect to particular embodiments, those familiar with the art will recognize various alternative designs and embodiments within the scope of the following claims. While various embodiments may have been described as providing advantages or being preferred over other embodiments with respect to one or more desired characteristics, as one skilled in the art is aware, one or more characteristics may be compromised to achieve desired system attributes, which depend on the specific application and implementation. These attributes include, but are not limited to: cost, efficiency, strength, durability, life cycle cost, marketability, appearance, packaging, size, serviceability, weight, manufacturability, ease of assembly, etc. The embodiments described herein that are characterized as less desirable than other embodiments or prior art implementations with respect to one or more characteristics are not outside the scope of the disclosure and may be desirable for particular applications.