Seal, assembly, and retention method
10584796 ยท 2020-03-10
Assignee
Inventors
- Jerry Hielkema (Loves Park, IL, US)
- Matthew Lindsay (Loves Park, IL, US)
- Scott Johnson (Loves Park, IL, US)
- Roy Ott (Loves Park, IL, US)
- Joseph Popham (Loves Park, IL, US)
Cpc classification
F16K1/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/205
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16K1/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/226
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present invention relates to a valve assembly that includes a retaining ring disposed within a cavity formed by adjoining a retainer and a disk member. The retaining ring can be disposed at a slant with respect to an inner surface of the cavity.
Claims
1. A valve assembly, comprising: a disk member; a retainer a seal having two parts, one part being secured between an outer surface of the disk member and a bottom surface of the retainer, and a second part protruding outwardly, away from the disk member and the retainer; and a retaining ring having a sloped configuration and being disposed within a cavity formed by adjoining an outer groove of the disk member and an inner groove of the retainer; wherein, the sloped configuration of the retaining ring results in the retaining ring having a slanted orientation with respect to an inner surface of the cavity; and wherein, the slanted orientation is characterized by (i) an upper portion of the retaining ring being secured against a side of the inner groove of the retainer, and (ii) a lower portion of the retaining ring being secured against an opposite side of the outer groove of the disk member, both (i) and (ii) providing a lateral force that presses the retainer against the seal.
2. The valve assembly of claim 1, wherein the retaining ring has a rectangular cross-section.
3. The valve assembly of claim 1, further comprising a metal support disposed at a bottom end of the seal.
4. The valve assembly of claim 1, wherein the seal includes carbon.
5. The valve assembly of claim 1, wherein at least one of the retainer and the disk member is made of steel.
6. The valve assembly of claim 5, wherein at least one of the retainer and the disk member is made of a corrosion-resistant material.
7. The valve assembly of claim 1, wherein the retaining ring is made of an iron-based alloy.
8. The valve assembly of claim 1, wherein the retaining ring is made of an age hardened iron superalloy.
Description
IV. BRIEF DESCRIPTION OF THE DRAWINGS
(1) Illustrative embodiments may take form in various components and arrangements of components. Illustrative embodiments are shown in the accompanying drawings, throughout which like reference numerals may indicate corresponding or similar parts in the various drawings. The drawings are for purposes of illustrating the embodiments and are not to be construed as limiting the disclosure. Given the following enabling description of the drawings, the novel aspects of the present disclosure should become evident to a person of ordinary skill in the relevant art(s).
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V. DETAILED DESCRIPTION OF THE EMBODIMENTS
(9) While the illustrative embodiments are described herein for particular applications, it should be understood that the present disclosure is not limited thereto. Those skilled in the art and with access to the teachings provided herein will recognize additional applications, modifications, and embodiments within the scope thereof and additional fields in which the present disclosure would be of significant utility.
(10)
(11) More specifically, excessive bending forces exerted on seal 106 during operation can lead to premature failure, especially when seal 106 is made of carbon. These forces also cause the retainer 104 to fail by causing the retainer 104 to extend into the valve's bore (not shown). This extending causes the conventional valve assembly 100 to jam in the open position. The exemplary embodiments described herein resolve these issues.
(12)
(13) The seal 204 can be secured partly between a first surface 218 of the disk member 202 and a second surface 220 of the retainer 206. A part of the seal 204 can protrude outwardly, away from the disk member 202 and the retainer 206. The part of seal 204 protruding outwardly performs the sealing operation of the valve when the valve assembly 200 is actuated. The seal 204 can be an L-shaped seal. That is, its cross-section can have a form shaped substantially like an L. The seal 204 can also have other cross-section shapes, known to one of skill in the relevant art(s). For example, a T-shaped seal could also be used.
(14) A cavity 210 is formed by adjoining the disk member 202 and the retainer 206. Specifically, the retainer 206 includes a first groove 212 and the disk member 202 includes a second groove 214, which, when the two parts are joined, form the cavity 210.
(15) A retaining ring 208 is disposed at a slant 216 with respect to a bottom surface of cavity 210. Generally speaking, the retaining ring 208 is angled (i.e., slanted) with respect to an inner surface of cavity 210. The retaining ring 208 can have a rectangular cross-section. Furthermore, the retaining ring 208 can be made of an age-hardened iron super alloy, or generally speaking, from an iron-based alloy.
(16) When disposed (i.e., with the slanted orientation with respect to the bottom surface of the cavity 210), the retaining ring 208 provides a lateral force. That is, the retaining ring 208 provides a force from right to left in
(17) The retaining ring 208 provides an additional retaining force that helps keep the seal 204 in place during typical operation where an air stream is incident on the valve assembly 200. The retaining force is, in addition to the forces being generated by the retainer 206, pressing or biasing the seal 204 on the disk member 202. As such, the seal 204 is securely held in place and does not excessively protrude into the air stream. Thus, the stresses exerted on the seal 204 by the air stream are prevented (or reduced to a minimum) because the retaining ring 208 provides the additional retaining for securing the seal 204 during operation. In this manner, the embodiments provide highly durable seals. For valve assemblies that utilize carbon seals, increased durability can be obtained as carbon seals are more susceptible to failure, than other types of seals, from being overly stressed.
(18)
(19) The support 302 confers several advantages to the valve assembly 300. For example, the support 302 acts as a substrate for the seal 204, thus providing increased physical support when the valve assembly 300 is operated. In addition, the support 302 biases the seal 204 against the valve body wall (not shown). This additional biasing reduces leakage when the valve assembly is operated.
(20)
(21) In aerospace applications, the valve assembly 200 can be a butterfly valve. More precisely, the valve assembly 200 can be a pressure-regulating butterfly valve assembly. Such a valve could be the lead pressure regulating valve in a jet engine. As such, the valve assembly 200 can provide a robust pressure regulating system in which the carbon seal used (i.e., the seal 204) has an increased lifespan because stresses resulting from the air stream it is subjected to are reduced. These reduced stresses result from the seal 204 being tightly secured between disk member 202 and retainer 206.
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(23) Having set forth various embodiments and their structure, specific details regarding the assembly of various constitutive elements of valve assembly 200 are now described with respect to
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(26) Upon assembly, the retaining ring 208 will expand into the groove of the retainer 206, indicated by the position 704. During expansion, the retaining ring 208 will develop an axial pre-load resulting from being compressed axially as it expands radially.
(27) With the retaining ring 208 still expanded inside the retainer 206, the two are slipped over the butterfly (i.e. over the disk member 202). Once the retainer 206 and the retaining ring 208 are mated with the disk member 202, as shown in
(28) Generally, the embodiments provide a retention method for a seal in a valve assembly. The seal is retained in the valve using a retainer. The retainer includes a retaining ring that expands therein and retracts radially when placed in a proper position. A weld can be provided at interface between the retainer and the disk member of the valve, thereby providing a strong retention force and an adequate supporting substrate for the seal. This configuration extends the lifetime of the seal by reducing the amount of stresses exerted on the seal during valve operation.
(29) While the embodiments have been described in the context of valves, butterfly valves, and valve assemblies, one of ordinary skill in the art will readily recognize that the techniques and configurations disclosed herein can be used in applications where any part is to be secured. For example, the techniques disclosed herein can be used to secure a bearing by using a retainer fitted with the retaining ring, as disclosed above.
(30) Moreover, the embodiments provide a method for creating tamper-proof assemblies. Specifically, because once the seal (or a bearing) is secured, the seal cannot be remove be removed from the assembly without releasing the retaining ring, which can only happen by breaking open the cavity in which the retaining ring is located. As such, for some applications, the embodiments provides advantages where means for providing passive tamper-proof mechanisms for securing parts and components are needed.
(31) Those skilled in the relevant art(s) will appreciate that various adaptations and modifications of the embodiments described above can be configured without departing from the scope and spirit of the disclosure. Therefore, it is to be understood that, within the scope of the appended claims, the disclosure may be practiced other than as specifically described herein.