This invention relates to flexible couplings used in gas flow conduits and in particular to flexible couplings used in conduits for hot exhaust gases, for example, from internal combustion engines.
Flexible couplings used in coupling hot gas exhausting conduits typically include an extended bellows or seal of multiple convolutions oriented between exhaust gas conduits or related components. The couplings may include internal liners and surrounding mesh sleeves or braided outer wire sleeves all of which have the undesirable effect of producing noise, vibration and harshness (NVH) to some degree. The harsh NVH environment in which these couplings are used also places the bellow component (seal) at risk for high frequency displacement fatigue if it is not dampened effectively.
Where a surrounding mesh or outer braid overwrap sleeve is used about the bellows convolutions, it typically and constantly contacts outer surfaces of the convolutions serving as a damper for the bellows component. While thus serving as a dampening component such contacting overwrap engages and abrades on the bellows convolutions and NVH from the coupling is produced.
Prior coupling disclosures are cited herewith for background as follows and these are incorporated herein by reference as if fully set out herein for background: U.S. Pat. Nos. 6,240,969 and 8,453,680; EP Patents 1967783 A1 and 0458011; and German Patent DE 10 2011 110147.
Accordingly, it is one objective of the invention to provide enhanced dampening for couplings having convoluted bellows, whether or not with surrounding mesh sleeves.
A further objective of the invention has been to provide improved flexible couplings for extremely harsh NVH applications where durability of a conventional mesh sleeve as a damper is otherwise compromised.
A further objective of the invention has been to provide improved damping in flexible exhaust gas couplings with or without a mesh or outer braid covering.
In one embodiment of the invention, one or more damping rings, are disposed exteriorly about the coupling bellows and in between at least two of the radially extending convolutions of the bellows. Preferably, the coupling does not include any surrounding outer braid or sleeve over the bellows or ring. The ring or rings serve as a damper in place of any such sleeve, and including during any differential thermal response of the bellows. In other alternate embodiments of the invention, an outer braid sleeve is wrapped around the bellows and one or more damping ring or rings reside outside the bellows but between respective convolutions thereof, under the braid, and inwardly of the radially outermost convolutions of the bellows adjacent the ring or rings.
Use of the dampening ring or rings according to the invention eliminates the need to use exterior mesh to dampen natural frequencies of the bellows. When made of the materials noted herein, the damping rings exceed the durability of a mesh damper in harsh NVH applications.
When a convoluted, sleeve-covered bellows coupling is provided according to the invention, with expansion of the convolutions, the damping rings described herein are disposed between bellows convolutions and inwardly of any sleeve and provide additional damping.
The use of damping rings described herein does not restrict the motion capabilities of the bellows, nor disables the movement of the convolutions resulting from any thermal response or other stress.
The location of the damping ring or rings axially along the bellows is adjustable based on the critical frequency of the components of the particular application. Therefore the damping rings can be placed between two convolutions along the bellows component, at one, two or more axial locations such as at first, second or more frequency nodes along the bellows.
While
4, coupling bellows as in these Figs. may in use be combined with such components.
Turning now to the drawings, components of two embodiments are shown in the Figs. A “one-ring” embodiment is illustrated in
Note the larger (wide-axially) circumferential spaces 17, 18 (
Alternately, a ring 25 may be made of other suitable materials such as heat resistant polymers including thermosets, thermoplastics, or elastomers.
Moreover, it will be appreciated that the cross-section of ring 25 (
As used herein, the term “outer braid” refers to a braided sleeve or any suitable mesh-like sleeve or cover.
With the significant exception of ring 25, its parameters, and the spacing between selected convolutions 12, 13 and 14, 15, one prior structure of a coupling is as seen in European Patent No. EP1467072/EP1238226B incorporated herein by reference.
Being resilient, ring or rings 25 lie between adjacent convolutions such as 12, 13 and 14, 15, or others as desired and dampens NVH generated in the system, when used in couplings 10, 30 as disclosed herein.
In the embodiment of
In each coupling embodiment 10, 30, ring or rings 25 serve to dampen the couplings without use of optional outer braid 26, the rings serving as the damper for the system.
Preferably the ring or rings 25 are located at axial positions along the respective bellows corresponding to or closely corresponding to expected vibrational nodes in the bellows when the couplings are used in an exhaust gas environment. As illustrated, ring location might be at about ½ the bellows length (coupling 30 in
As a result, the invention provides damped bellows for a flexible coupling which is tunable in both density and dampening at critical bellows node positions and on the exterior of the bellows component without restriction of motion capability. The invention eliminates necessary use of an optional mesh outer sleeve component used in the past to dampen bellow natural frequencies, although such a sleeve can be used in conjunction with the invention. Increased ring density provides a damped bellows which exceeds the durability of prior bellows with mesh damper sleeves in harsh NVH applications.
These and other modifications and a advantages will become readily apparent to those of ordinary skill in the art without departing from the scope of the invention and applicant intends to be bound only by the claims appended hereto.
Applicant claims the benefit of the filing date of Jan. 9, 2015 of U.S. Provisional Patent Application Ser. No. 62/101,417, which application is incorporated herein in its entirety as if fully set out here in.
Number | Date | Country | |
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62101417 | Jan 2015 | US |