A shaft holding system for cryogenic pumps or expanders comprising a set of hydraulic brakes surrounding the shaft of a turbomachine. Fluid or gas is introduced into the bellows chamber of a brake assembly. The bellows chamber expands due to the increase in pressure, thus exerting a force on the piston of the brake assembly. The piston in turn exerts a force on a brake rod, which pushes a brake pad attached to the end of the brake rod against the shaft. A feed line supplies fluid or gas to the hydraulics of the brake assembly. Two or more brakes can be used to secure the shaft of the turbomachine. A turbomachine including more than one shaft can use a set of brakes for each shaft of the turbomachine.
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Cryogenic liquids are refrigerated liquefied gases with boiling points below −90° C. at atmospheric pressure. Different cryogens become liquids under different conditions of temperature and pressure. Industrial facilities that produce, store, transport and utilize such gases make use of a variety of valves, pumps and expanders to move, control and process the liquids and gases.
There are problems which can damage a shaft of an expander or a pump during standstill conditions. For example, reverse flow can force the shaft to rotate in reverse, potentially damaging the shaft and introducing stress to the shaft bearings. An unstable foundation can also make the shaft of an expander or a pump rotate. Movement in floating platforms can cause the pump or expander to move around, which can cause the shaft of the pump or expander to get damaged. In floating storage and regasification units that are permanently moored offshore, weather conditions can result in significant movement due to ocean conditions. For example, if a ship motion constantly changes by pitching and rolling, this can make an expander or pump installed in a vessel, or on a floating storage tank, receive continuous side forces that can damage the shaft.
A shaft holding system consisting of two or more brake assemblies surrounding the shaft of turbomachinery. Turbomachinery generally refers to machines that transfer energy from the processing of a fluid or gas using some type of turbine. From herein, the terms “turbomachinery” and “turbomachines” will be used to refer to turbines, expanders, compressors, fans, or pumps.
Each brake assembly consists of one or more hydraulic brakes. In operation, pressure is introduced into a bellows chamber of the brake, which exerts force on a piston. The piston applies force to a brake pad, which forces the brake pads to be pushed against the shaft of the expander, the pump, or other structure. Face seals are used to prevent pressure from escaping around the piston.
Turbomachines with two or more shafts can use a set of brakes for each of the two or more shafts. For example, in a turbine with a first shaft and a second shaft, where torque from the first shaft is transferred to the second shaft via a magnetically coupled membrane, a first set of brakes can be used for the first shaft and a second set of brakes can be used for the second shaft. Alternative embodiments can also include more than one set of brakes for each shaft. For example, a first set of brakes can be used on the top portion of a turbine shaft, and a second set of brakes can be used for the bottom portion of the turbine shaft.
The brake piston 106 can similarly be made from stainless steel or other metals. The brake piston 106 exerts a force on a brake rod 206 via a central spring 208. A brake stop 210 prevents the brake rod 206 from fully extending under the expansion pressure of the central spring 208, thus restricting the piston travel. The brake rod 206, with the central spring 208, allow for pressure to be applied on the various face seals (further described below) of the brake assembly 100 and on the shaft (not shown) of the turbomachine. As previously noted, the bias spring 116 exerts pressure against the piston 106 in a direction opposite the shaft such that when pressure is removed from the bellows 104, the piston is retracted from contact with the shaft.
The brake pad 118 is attached via a support disk 212 to the brake rod 206. A screw cap 214 is used to attach the brake pad 118 to the piston 106. The brake pad 118 can be made out of Polytetrafluoroethylene (PTFE). The support disk 212 and the screw cap 214 can be made out of metal, such as stainless steel.
A pressure seal 216 seals the pressure inside of the piston 106. The pressure seal 216 can be made out of Tetrafluoroethylene (TFE) with a stainless steel spring. A first face seal 218 on the piston 106 creates a seal between the piston 106 and the upper portion of the brake body 102 when the piston 106 is disengaged. The piston 106 is disengaged when the piston 106 is not exerting a force against the shaft of the system. A second face seal 220 creates a seal between the piston and the brake plate 202 when the piston 106 is engaged. The piston 106 is engaged when the piston 106 is exerting a force on the shaft of the system. The face seals 218 and 220 can be o-rings made from PTFE. A third face seal 222 can also be used between the brake plate 202 and the upper portion of the brake body 102 to seal the pressure within the brake assembly 100.
Embodiments are not limited to using only two brakes to support the shaft 306. For example, depending on the size of the shaft and the size of the brakes, more than two brakes may be necessary. It may also be determined that when the vessel is subject to constant and heavy forces, more than two brakes may be necessary to reduce the stress on the bearings. Brakes need not be arranged opposite of each other across the shaft, at angles of approximately 180 degrees from each other. However, it is important for the overall forces applied by the brakes to the shaft be balanced; otherwise additional stress could be introduced to the bearings. For example, if three brakes are used, they should be positioned at angles of approximately 120 degrees from each other so as to balance the forces between the three brakes and steps should be taken to make sure that all three brakes employ and deploy at the same time, such as by using a single feed line with split lines of approximately equal length to each brake so gas or fluid being supplied to one brake does not arrive before gas or fluid supplying other brakes.
If the pump/expander or other structure includes more than one shaft, a set of brakes can be used for each shaft of the pump/expander. For example, an expander may consist of a turbine shaft and an electric motor shaft, with the torque from the turbine shaft transmitted to the electric motor shaft through a magnetic coupling membrane. In such an expander, a first set of brakes can be used to secure the turbine shaft and a second set of brakes can be used to secure the electric motor shaft. The fluid or gas used to feed the hydraulics of the first set of brakes and the second set of brakes can be supplied via a single feed line, with the single feed line first splitting into a first feed line for the first set of brakes and a second feed line for the second set of brakes. The first feed line and the second feed line may subsequently split into two or more feed lines as necessary for each brake within each set of brakes. Alternatively, each set of brakes can have its own independent feed line, which is subsequently split as necessary to feed each brake within each set of brakes. Alternative embodiments may also use the fluid or gas being pumped or expanded to feed the hydraulics of the brake assembly. Since the shaft holding system described herein is used during standstill conditions, the supply line can also extract fluid or gas from the vessel housing the pump/expander.
While a number of embodiments have been illustrated and described herein, along with several alternatives and combinations of various elements, for use in pumps, expanders, or some other form of turbomachine structure, it is to be understood that the embodiments described herein are not limited to only be used with turbomachines and can have a multitude of additional uses and applications. Accordingly, the embodiments should not be limited to just the particular descriptions, variations and drawing figures contained in this specification, which merely illustrate a preferred embodiment and several alternative embodiments.
This application claims priority from provisional patent application Ser. No. 61/217,201, filed May 26, 2009, which is hereby incorporated herein by reference in its entirety to be considered part of this specification.
Number | Date | Country | |
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61217201 | May 2009 | US |