Double layered, bent exhaust pipe
10174663 ยท 2019-01-08
Assignee
Inventors
Cpc classification
F01N13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/141
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2470/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2470/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2510/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
An exhaust pathway for an internal combustion engine passes from a larger pipe to a smaller pipe, and then back to a larger pipe. The smaller pipe has a bend of at least approximately 80, and each of the smaller and downstream larger pipes is disposed within, and spaced apart from, portions of a shell, such that cooling air passes in an air gap between the pipes and the shell.
Claims
1. An exhaust system for an internal combustion engine comprising: an exhaust path that includes an upstream exhaust segment, an intermediate exhaust segment, and a downstream exhaust segment; the upstream, intermediate, and downstream exhaust segments having lumens with maximal normal cross-sections, wherein a maximal inside diameter of the upstream exhaust segment and the downstream exhaust segment are each greater than a maximal inside diameter of the intermediate exhaust segment; a reducer that gaseously couples the upstream exhaust segment to the intermediate exhaust segment; an expander that gaseously couples the intermediate exhaust segment to the downstream exhaust segment; a first shell segment disposed about the reducer, and spaced apart from the intermediate exhaust segment, thereby forming a first portion of a continuous air gap, wherein a first baffle positioned internal to the first shell allows ambient air to flow into the first portion of the continuous air gap through a first passageway; a second shell segment disposed about the expander, and spaced apart from and the downstream exhaust segment, thereby forming a second portion of the continuous air gap, wherein a second baffle positioned internal to the second shell allows ambient air to flow into the second portion of the continuous air gap through a second passageway and out to the atmosphere through a third baffle; wherein the intermediate exhaust segment has a curve that subtends an angle between 80 and 100.
2. The exhaust system of claim 1, wherein the second shell is at least 3 meters long.
3. The exhaust system of claim 1, wherein the intermediate exhaust segment is at least 20% less than the upstream exhaust segment.
4. The exhaust system of claim 1, wherein the upstream exhaust segment has a maximal inside diameter of at least 5, the intermediate exhaust segment has a maximal inside diameter of no more than 4, and the downstream segment has a maximal inside diameter of at least 4.75.
5. The exhaust system of claim 1, wherein at least one of the upstream, intermediate and downstream exhaust segments comprise a stainless steel.
6. The exhaust system of claim 1, wherein each of the first and second shells has a chrome coating.
7. The exhaust system of claim 1, wherein a downstream end of the first shell is positioned to abut an upstream end of the second shell.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
DETAILED DESCRIPTION
(5)
(6) A first segment 120A of the shell 120 is disposed about the intermediate exhaust segment 110B, and second segment 120B of the shell is disposed about the downstream exhaust segment 110C. This arrangement provides a continuous air gap 150 between the intermediate and downstream exhaust segments 110B, 110C and the shell 120. Air enters the air gap 150 through a baffle 130A disposed within the lumen of the first segment 120A of the shell, passes though baffle 130B disposed within the lumen of the lower end of the second segment 120B of the shell, and then out to the atmosphere through baffle 130C, disposed within the lumen of the upper end of second segment 120B of the shell.
(7) When installed in a typical semi truck 300, the upstream exhaust segment often has an inside diameter of at least 5. This is problematic because if the intermediate exhaust segment 110B were to have the same 5 inside diameter, the bent region of the pipe and its shell are so large that they are very difficult to bend without producing significant distortions.
(8) The class of solutions contemplated herein provides an intermediate exhaust segment 110B having a smaller inside diameter than both upstream and downstream exhaust segments, 110A, 110C. A reducer 170 is used to couple the upstream and intermediate exhaust segments 110A, 110B, and an expander 172 is used to couple the intermediate and downstream exhaust segments 110B, 110C.
(9) In a particularly preferred embodiment the upstream, intermediate and downstream exhaust segments 110A, 110B and 110C have inside diameters of 5, 4 and 4.75, respectively, and the upstream and second shells 120A, 120B have substantially the same outer diameters of 7.845.
(10) More generally, it is preferred that a maximal normal cross-section area of the intermediate exhaust segment 110B is at least 10% smaller than that of the upstream exhaust segment 110A. It is even more preferred that a maximal normal cross-section area of the intermediate exhaust segment 110B is smaller by at least 15% than that of the upstream exhaust segment 110A, and still more preferred smaller by at least 20%.
(11) It is also preferred that the maximal normal cross-section of area of the downstream exhaust segment 110C has at least 10% larger than that of the intermediate exhaust segment 110B. It is even more preferred that a maximal normal cross-section area of the downstream exhaust segment 110C is larger by at least 15% than that of the intermediate exhaust segment 110B, and still more preferred larger by at least 20%.
(12)
(13) The various exhaust segments 110A, 110B and 110C can be of any suitable lengths, which would depend on the size of the truck to which they are installed, and in some cases on person preference. In
(14) Each of upstream, intermediate and downstream exhaust segments 110A, 110B and 110C, and shell segments 120A and 120B are made of a stainless steel to avoid corrosion, preferably 304 or 409 steels. Shell segments 120A and 120B are to be interpreted as being either powder coated or layered with chrome. The inside diameters of shell segments 120A and 120B are preferably selected relative to the outside diameters of intermediate and downstream exhaust segments 110B, 110C such that there is sufficient airflow through air gap 150 to keep the shell segments 120A, 120B below temperatures that would disrupt the integrity of the coating.
(15) Since exhaust gas within the upstream exhaust segment 110A could be at least 450 F., the size of the air gap is particularly important in the case of chrome coatings. If the chrome becomes too hot, chemical interaction with bugs that hit the chrome can cause significant erosion of the chrome. It is preferred that the air gap 150 be at least 1 in.
(16)
(17) Baffle 200 has air passageways 240A, 240B, 240C, 240D, 240E and 240F. There can be more or fewer gaps in different embodiments, and they can have any suitable shapes. The passageways are meant to be a large as realistically possible to provide minimal resistance to flow of air, given the need to maintain structural integrity. Baffles 200 can be manufactured in any suitable manner, including for example water cast aluminum.
(18) In
(19) Baffle 130B is shown as being disposed about downstream exhaust segment 110C, and internal to the lumen of shell segment 120B. Alternatively baffle 130B could be disposed about downstream exhaust segment 110C, internal to the lumen of shell segment 120A.
(20) Baffle 130C is preferably disposed near the top of downstream exhaust segment 110C, internal to the lumen of shell segment 120B.
(21) An optional venturi 250 component positioned near the exhaust gas exit from downstream exhaust segment 110C can be used to assist in drawing exhaust gas up through the upstream, intermediate and downstream exhaust segments 110A, 110B, 110C.
(22)
(23) One of ordinary skill in the art would not have thought to pass exhaust gas successively through larger, smaller and then larger segments of an exhaust pipe. Among other things, passaging of the gas from the larger upstream segment to the smaller segment would be expected to add considerable back pressure to the engine, and significantly increase heat in the transition from the larger upstream segment to the smaller segment. The strain on the smaller segment is exacerbated if, as in various embodiments of the present subject matter, the smaller segment has a significant bend.
(24) The discussion herein provides example embodiments of the inventive subject matter. Although each embodiment represents a single combination of inventive elements, the inventive subject matter is considered to include all possible combinations of the disclosed elements. Thus if one embodiment comprises elements A, B, and C, and an intermediate embodiment comprises elements B and D, then the inventive subject matter is also considered to include other remaining combinations of A, B, C, or D, even if not explicitly disclosed.
(25) As used herein, and unless the context dictates otherwise, the term coupled to is intended to include both direct coupling (in which two elements that are coupled to each other contact each other) and indirect coupling (in which at least one additional element is located between the two elements). Therefore, the terms coupled to and coupled with are used synonymously.
(26) In some embodiments, the numbers expressing quantities of ingredients, properties such as concentration, reaction conditions, and so forth, used to describe and claim certain embodiments of the invention are to be understood as being modified in some instances by the term about. Accordingly, in some embodiments, the numerical parameters set forth in the written description and attached claims are approximations that can vary depending upon the desired properties sought to be obtained by a particular embodiment. In some embodiments, the numerical parameters should be construed in light of the number of reported significant digits and by applying ordinary rounding techniques. Notwithstanding that the numerical ranges and parameters setting forth the broad scope of some embodiments of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as practicable. The numerical values presented in some embodiments of the invention may contain certain errors necessarily resulting from the standard deviation found in their respective testing measurements.
(27) As used in the description herein and throughout the claims that follow, the meaning of a, an, and the includes plural reference unless the context clearly dictates otherwise. Also, as used in the description herein, the meaning of in includes in and on unless the context clearly dictates otherwise.
(28) The recitation of ranges of values herein is merely intended to serve as a shorthand method of referring individually to each separate value falling within the range. Unless otherwise indicated herein, each individual value is incorporated into the specification as if it were individually recited herein. All methods described herein can be performed in any suitable order unless otherwise indicated herein or otherwise clearly contradicted by context. The use of any and all examples, or exemplary language (e.g. such as) provided with respect to certain embodiments herein is intended merely to better illuminate the invention and does not pose a limitation on the scope of the invention otherwise claimed. No language in the specification should be construed as indicating any non-claimed element essential to the practice of the invention.
(29) Groupings of alternative elements or embodiments of the invention disclosed herein are not to be construed as limitations. Each group member can be referred to and claimed individually or in any combination with other members of the group or other elements found herein. One or more members of a group can be included in, or deleted from, a group for reasons of convenience and/or patentability. When any such inclusion or deletion occurs, the specification is herein deemed to contain the group as modified thus fulfilling the written description of all Markush groups used in the appended claims.
(30) It should therefore be apparent to those skilled in the art that many more modifications besides those already described are possible without departing from the inventive concepts herein. The inventive subject matter, therefore, is not to be restricted except in the spirit of the appended claims. Moreover, in interpreting both the specification and the claims, all terms should be interpreted in the broadest possible manner consistent with the context. In particular, the terms comprises and comprising should be interpreted as referring to elements, components, or steps in a non-exclusive manner, indicating that the referenced elements, components, or steps may be present, or utilized, or combined with other elements, components, or steps that are not expressly referenced. Where the specification claims refers to at least one of something selected from the group consisting of A, B, C . . . and N, the text should be interpreted as requiring only one element from the group, not A plus N, or B plus N, etc.