SHOCK WAVE MECHANICAL SEAL

Abstract

A shockwave-inducing mechanical rotating shaft seal includes a seal face gap having at least one section of converging and then diverging gap width that supersonically accelerates compressible fluid escaping through the seal gap, thereby causing a shockwave that reduces the fluid pressure and provides a high pressure fluid seal with significantly reduced viscous heating and gap width. A plurality of the converging-diverging sections can be provided, having a combined width between 0.004 and 0.008 inches. The converging-diverging sections can be configured to accelerate the fluid to a Mach number less than 4. The gap can further include a section of flat, parallel seal faces that induce viscous stresses in the fluid, thereby further reducing the fluid pressure. The seal can be configured with axially directed seal faces or radially directed seal faces, and/or used as a pre-conditioner in combination with a conventional downstream mechanical fluid seal.

Claims

1. A mechanical seal configured for sealing a pressurized, compressible fluid, the seal comprising: a rotating sealing ring surrounding a rotating shaft, the rotating sealing ring being rotationally cooperative with and sealed to the rotating shaft; a stationary sealing ring cooperative with and sealed to a housing that is penetrated by the rotating shaft, a stationary seal face of the stationary sealing ring being substantially parallel to a rotating seal face of the rotating sealing ring, the rotating and stationary seal faces being separated by an annular seal gap; and at least one annular shock inducing section included in the seal gap, the shock-inducing section including: an annular converging segment within which a radial cross section of the seal gap narrows with increasing radius; and an annular diverging segment within which the radial cross section of the seal gap widens with increasing radius, the diverging segment being adjacent to and radially outward from the converging segment, so that a local minimum in seal gap width, referred to herein as a choke point, is formed between the converging segment and the diverging segment; the converging and diverging segments being configured to cause the compressible fluid when flowing radially outward through the seal gap to be accelerated within the shock-inducing section into a supersonic state, so that a shockwave is formed by the fluid within the diverging segment, thereby reducing a stagnation pressure of the fluid.

2. The seal of claim 1, wherein the seal gap includes a plurality of adjacent shock-inducing sections.

3. The seal of claim 1, wherein at least one of the narrowing and widening of each segment of each shock-inducing section is due to shaping of at least one of the rotating seal face and the stationary seal face.

4. The seal of claim 1, wherein a combined width of the shock-inducing sections is between 0.004 inches and 0.008 inches.

5. The seal of claim 1, wherein the shock-inducing sections are located proximal to a boundary of the seal gap where the pressurized fluid enters the seal gap.

6. The seal of claim 1, wherein the mechanical seal is axially configured, such that the seal faces are parallel to the rotating shaft, the rotating seal face being radially inward of the stationary seal face.

7. The seal of claim 1, wherein the mechanical seal is radially configured, such that the seal faces are perpendicular to the rotating shaft, the rotating and stationary faces being axially offset from each other.

8. The seal of claim 1, wherein the shock-inducing sections are configured to cause fluid flowing outward through the seal gap to be accelerated into a supersonic state having a Mach number of less than 4.

9. The seal of claim 1, further comprising a concentric, viscosity-inducing section included in the seal gap outward from the at least one shock-inducing section, the seal faces in the viscosity-inducing section being flat and parallel to each other, and being configured to induce viscous stresses on the fluid within the seal gap, thereby further reducing the stagnation pressure of the fluid.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0027] FIG. 1 is a cross-sectional side view of a shock wave mechanical seal in an axial configuration according to an embodiment of the present invention;

[0028] FIG. 2 is a cross-sectional side view illustrating air flow through a single converging-diverging section in an embodiment of the present invention;

[0029] FIG. 3 is a cross-sectional side view of a shock wave mechanical seal in a radial configuration according to an embodiment of the present invention;

[0030] FIG. 4 is a cross-sectional side view illustrating series of three converging-diverging sections in an axial embodiment that is suitable for CO2 at 1300 degrees Fahrenheit and 4400 psi pressure;

[0031] FIG. 5 is a series of side views that illustrate dimensions of the seal gap in a radial embodiment;

[0032] FIG. 6A is a graph rendered in color that presents Mach number and pressure results of a flow simulation of an axial configuration similar to FIG. 5;

[0033] FIG. 6B presents the graph of FIG. 6A rendered in half-toned format;

[0034] FIG. 7 is a graph that illustrates the pressure loss across the sealing surface in the simulation of FIGS. 6A and 6B;

[0035] FIG. 8 is a graph that illustrates changes in temperature across the sealing surface of the simulation of FIGS. 6A and 6B; and

[0036] FIG. 9 is an expansion of the graph of FIG. 8 in the contoured region of the converging-diverging sections.

DETAILED DESCRIPTION

[0037] The present invention is a rotating shaft seal that is structurally analogous to a mechanical seal, but which functions according to a fundamentally different physical principle that enables it to be more efficient and effective in sealing high temperature fluids than traditional mechanical seals. With reference to FIG. 1, and in analogy with a conventional mechanical seal, a rotating sealing ring 100 is fixed to a rotating shaft 102 and is located parallel with and closely adjacent to a stationary sealing ring 104 that is fixed to a housing or other surrounding, stationary structure.

[0038] According to the present invention, the seal is configured such that the pressurized compressible fluid can only escape from the sealed volume 106 to the surrounding, lower pressure environment 108 by passing through the gap 110 between the seal faces 112, 114. The high pressure fluid entering the gap 110 between the seal faces 112, 114 passes through one or more annular sections 116, 118, 120. The structure of one of these sections 116 is enlarged in FIG. 2. Each section includes a converging segment 200 within which the gap 110 narrows, followed by a diverging segment 202 within which the gap 110 widens. Within each section 116, 118, 120, the fluid is thereby accelerated to a supersonic condition, such that a shockwave 204 is induced shortly after the fluid enters the diverging segment 202. The stagnation pressure of the fluid is consequently decreased by the action of the shockwave, causing a backpressure that significantly reduces leakage of the fluid through the gap.

[0039] The dimensions and the number of converging/diverging sections included in each embodiment are determined according to the fluid pressure within the sealed volume 106 and the desired relative pressure drop. For example, the embodiment of FIG. 1 includes three sections 116, 118, 120, and the overall length of the converging-diverging sections is between 0.004 and 0.008 inches.

[0040] In the embodiment of FIGS. 1 and 2, the converging-diverging geometry of each section is imposed on the stationary seal face. In various other embodiments, the converging-diverging geometry of each section is imposed on the rotating seal face, or on both of the seal faces. The configuration can be different for each section. For example, some embodiments are configured such that the converging-diverging geometry is imposed only on the stationary seal face in a first section, only on the rotating seal face in a second section, and on both seal faces in a third section. In the embodiment of FIGS. 1 and 2, the converging-diverging sections 116 118, 120, are located near the edges of the seal faces 112, 114, where the fluid enters the seal gap from the sealed fluid volume 106.

[0041] The embodiment of FIG. 1 is configured axially, whereby the stationary seal face 112 is the inner diameter of a stationary component 100 that surrounds a shaft 102, while the rotary seal face 114 is the outer diameter of a rotating component 100 that surrounds and is fixed to the shaft 102. In the embodiment of FIG. 3, the seal faces 112, 114 are configured radially, whereby the seal faces 112, 114 are axially adjacent to each other, with one sealing ring 100 being attached and sealed to the rotating shaft 102, and the other sealing ring 104 being attached and sealed to the stationary assembly.

Principle of Operation

[0042] With reference again to FIG. 2, in each converging-diverging section 116 of the disclosed seal, the compressible fluid is first accelerated within the converging segment 200 as the gap 110 narrows, until it reaches a minimum gap clearance 206. At this location, the fluid reaches a choked condition, where the fluid velocity cannot increase beyond Mach 1. As the fluid enters the diverging segment 202, the gap 110 widens, further accelerating the flow to a supersonic condition, whereupon back-pressure imposed by downstream sections induce a standing normal shockwave 204 in the diverging segment 202. Although the static pressure of the fluid 210 after the shockwave is much higher than the static pressure immediately upstream of the shockwave 208, the stagnation pressure of the fluid 210 is greatly reduced, and is a function of the maximum Mach number that is reached in the diverging segment 202 before the shock wave 204. The amount of pressure drop in each section is therefore limited by the maximum Mach number that is achievable in each section.

[0043] In some embodiments, a Mach number of 4 or higher can tend to result in dissociation of the fluid within the shockwave and along the walls, and may begin to cause significant viscous heating effects on the walls. Accordingly, embodiments are designed such that the maximum Mach number of each section is 3 or less. Under these conditions, each section results in a pressure drop of approximately 50%. Thus, to achieve a desired pressure drop across the seal faces, the number of converging-diverging sections is selected according to the requirements of the embodiment, with higher sealed fluid pressures typically requiring a greater number of converging-diverging sections.

[0044] In embodiments, the amount of fluid leakage through the seal is determined by the first converging-diverging section's minimum gap width and area.

[0045] Referring again to FIG. 1, if it is desirable to combine the disclosed shockwave pressure reduction mechanism with viscous-effect pressure reduction, then the seal faces 112, 114 can be extended downstream 108 of the converging-diverging sections 116, 118, 120 so as to create two sealing regions 122, 124, wherein the first sealing region 122 includes the converging-diverging sections that reduce fluid pressure by inducing shock waves 206, and the second sealing region 124 further reduces the fluid pressure due to viscous dissipation within the seal face gap 110, in the manner of a conventional mechanical seal.

[0046] Similarly, a seal operating according to the principles disclosed herein can be used as a pre-conditioner, much like a throttle bushing, in combination with a conventional downstream fluid seal. In this way, a seal of the present invention can be used to enable existing seal technology that is well proven for sealing fluids at lower pressures to be applied in ultra-high pressure applications.

Advantages

[0047] The present invention provides at least two significant technical advantages as compared to prior art mechanical seals. The first is the significant reduction in viscous heating associated with the action of the shockwaves that reduce the fluid pressure. Although some viscous heating is unavoidable due to the small gap clearances required by the invention, the principle by which the invention operates does not depend upon viscous effects (other than the shockwaves) to reduce the fluid pressure, and so embodiments can be designed to minimize viscous heating. The second advantage is the short length scale of the converging-diverging seal features, which can allow the seal faces to be scaled to very small sizes, reducing material costs and product envelopes.

[0048] In the embodiment of FIG. 4, for example, a radial embodiment is illustrated that is suitable for CO2 at 1300 degrees Fahrenheit and 4400 psi pressure, with a flow rate through the gap 110 of 1 gram per second. The choked opening 206 in this embodiment is 6.975 millionths of an inch wide, and the distance from the first choked opening 206 to the low pressure end of the converging-diverging architecture is 3.81 thousandths of an inch.

[0049] FIG. 5 illustrates dimensions of the gap 110 in a radial embodiment, where the fluid flow is from top to bottom in the figure. FIGS. 6A and 6B present results of a flow simulation of an axial configuration similar to FIG. 5.

[0050] FIG. 7 is a graph that illustrates the pressure loss across the sealing surface in the simulation of FIGS. 6A and 6B. The flow is from top to bottom. Note that nearly all of the pressure loss occurs almost immediately (at the top), coinciding with the contoured region of the converging-diverging sections.

[0051] FIG. 8 is a graph that illustrates changes in temperature across the sealing surface of the simulation of FIGS. 6A and 6B. The walls are considered to be adiabatic in this simulation, such that the result represents the highest possible temperatures. Close clearances at the top lead to high viscous heating and rapid temperature increases. These temperature increases can be controlled by increasing the clearance at the inlet and outlet, since the performance of the seal is not strongly dependent upon the clearance at the inlet and outlet of the contoured region of the gap. Other approaches to controlling the temperature included in various embodiments include selecting thermally conductive materials and/or active thermal management, e.g. by utilizing a cooling liquid.

[0052] FIG. 9 is an expansion of the graph of FIG. 8 in the contoured region of the converging-diverging sections. Note that the temperature increase is only about 40 degrees Fahrenheit in this region, as compared to 250 degrees Fahrenheit overall. Much of this temperature increase is due to viscous heating, while the action of the shockwaves does comparatively little to increase the temperature.

[0053] The foregoing description of the embodiments of the invention has been presented for the purposes of illustration and description. Each and every page of this submission, and all contents thereon, however characterized, identified, or numbered, is considered a substantive part of this application for all purposes, irrespective of form or placement within the application.

[0054] The invention illustratively disclosed herein suitably may be practiced in the absence of any element which is not specifically disclosed herein and is not inherently necessary. However, this specification is not intended to be exhaustive. Although the present application is shown in a limited number of forms, the scope of the invention is not limited to just these forms, but is amenable to various changes and modifications without departing from the spirit thereof. One of ordinary skill in the art should appreciate after learning the teachings related to the claimed subject matter contained in the foregoing description that many modifications and variations are possible in light of this disclosure. Accordingly, the claimed subject matter includes any combination of the above-described elements in all possible variations thereof, unless otherwise indicated herein or otherwise clearly contradicted by context. In particular, the limitations presented in dependent claims below can be combined with their corresponding independent claims in any number and in any order without departing from the scope of this disclosure, unless the dependent claims are logically incompatible with each other.