This application is based upon and claims the benefit of priority from Japanese Patent Application No. 2017-178355, filed on Sep. 15, 2017; the entire contents of which are incorporated herein by reference.
Embodiments described herein relate generally to a gas circuit breaker.
A conventionally known gas circuit breaker has two contact portions constituting an electrical circuit, and arc discharge generated between the two contact portions is extinguished by spraying an arc-extinguishing gas.
This type of gas circuit breaker is significant, for example, if arc discharge can be extinguished more smoothly or more reliably.
According to an embodiment, a gas circuit breaker includes, for example, a container, a movable portion, an opposing portion, and a nozzle. The container is filled with an arc-extinguishing gas. The movable portion is housed in the container, and includes a movable arc contact. The movable portion is provided with a pressure accumulator that increases pressure of an arc-extinguishing gas. The opposing portion is housed in the container, and includes an opposing arc contact, an exhaust pipe, and a shielding portion provided in the exhaust pipe in a state of allowing flow of an arc-extinguishing gas in the exhaust pipe. The nozzle is housed in the container. The nozzle is provided with a space in which arc discharge is generated between the movable arc contact and the opposing arc contact. The shielding portion includes a first shielding wall intersecting with an axial direction of the exhaust pipe, and a second shielding wall having a cylindrical shape extending from the first shielding wall toward the movable portion along the axial direction of the exhaust pipe. The second shielding wall is provided with a plurality of through-holes with a space therebetween along the axial direction. The length of each of the through-holes along the axial direction is from 18 millimeters to 55 millimeters inclusive. An arc-extinguishing gas whose pressure has been increased in the pressure accumulator flows into the space to extinguish the arc discharge, and flows into the second shielding wall.
Exemplary embodiments of the present invention will be disclosed below. Configurations and control (technical characteristics) of the embodiments described below, and operations and results (effects) due to the configurations and control are only examples.
As illustrated in
As illustrated in
The arc-extinguishing gas is a gas exhibiting excellent arc extinguishing performance and insulation performance, for example, sulfur hexafluoride gas (SF6 gas), air, carbon dioxide, oxygen, nitrogen, and a mixed gas thereof. The arc-extinguishing gas can be a gas, for example, having a global warming potential lower than the SF6 gas and a lower molecular weight than the SF6 gas, and being in a gas phase at at least 1 atmospheric pressure or higher and at a temperature of 20° C. or lower.
In the airtight container 30, the opposing contact portion 10 and the movable contact portion 20 are provided to face each other. The opposing contact portion 10 and the movable contact portion 20 include a plurality of cylindrical or columnar members and are provided concentrically around a central axis Ax. In the following descriptions, “axial direction” is an axial direction of the central axis Ax, “radial direction” is a radial direction of the central axis Ax, and “circumferential direction” is a circumferential direction of the central axis Ax. The opposing contact portion 10 is an example of an opposing portion, and the movable contact portion 20 is an example of a movable portion. In the following descriptions, for convenience sake, the side of the opposing contact portion 10 in the axial direction, that is, the left side in
A support member 31 projects from an inner surface of the airtight container 30 inward in the radial direction. The opposing contact portion 10 is fixed to the airtight container 30 via the support member 31. The support member 31 insulates between the airtight container 30 and the opposing contact portion 10. Accordingly, the support member 31 is also referred to as “insulation support member”.
The movable contact portion 20 is connected to an operating rod 40. The operating rod 40 is formed in a cylindrical shape extending along the axial direction A around the central axis Ax, and is configured to be capable of reciprocating along the central axis Ax. The operating rod 40 is moved along the axial direction A by a drive system (not illustrated). The movable contact portion 20 moves in the axial direction A in association with the operating rod 40. When the operating rod 40 moves in a direction approaching the opposing contact portion 10, that is, moves in the axial direction A, as illustrated in
The opposing contact portion 10 includes an opposing arc contact 11 and an opposing energizing contact 12. The movable contact portion 20 includes a movable arc contact 21 and a movable energizing contact 22. The opposing arc contact 11 and the movable arc contact 21 face each other in the axial direction A, and are electrically connected with each other in a connected state. The opposing energizing contact 12 and the movable energizing contact 22 face each other in the axial direction A, and are electrically connected with each other in a connected state. When the opposing contact portion 10 is fixed to the airtight container 30, the opposing arc contact 11 can be also referred to as “fixed arc contact”, and the opposing energizing contact 12 can be also referred to as “fixed energizing contact”.
The opposing arc contact 11 is a rod-like conductor, and extends along the axial direction A around the central axis Ax. A first shielding wall 14 having a disk shape being orthogonal to the axial direction A is provided in an exhaust pipe 13 of the opposing contact portion 10. A second shielding wall 15 having a cylindrical shape extending along the axial direction A is provided from the first shielding wall 14 toward the other side of the axial direction A.
The movable arc contact 21 is a cylindrical conductor, and extends along the axial direction A around the central axis Ax. According to the present embodiment, the movable arc contact 21 is integrated with the operating rod 40 as an example. A through-hole 21a having a circular shape is provided at the end of the movable arc contact 21 in the axial direction A. The end provided with the through-hole 21a is divided into a plurality of finger-like electrodes extending along the axial direction A by a plurality of slits (not illustrated) extending along the axial direction A. Ends of the finger-like electrodes are aligned along an edge having a diameter narrower than an outer periphery of the opposing arc contact 11. The movable arc contact 21 approaches the opposing arc contact 11 with movement of the operating rod 40, and as illustrated in
Apical ends of the opposing arc contact 11 and the movable arc contact 21 are covered with an insulation nozzle 50 with a gap. The insulation nozzle 50 is formed of a material having heat resistance and insulation properties such as polytetrafluoroethylene. According to the present embodiment, as an example, the insulation nozzle 50 is fixed to the end of the movable contact portion 20 in the axial direction A, and moves integrally with the operating rod 40 and a cylinder 23 in the axial direction A. The insulation nozzle 50 has a cylindrical outer surface, and extends along the axial direction A around the central axis Ax. The insulation nozzle 50 is an example of a nozzle.
An opening 50a penetrating the insulation nozzle 50 in the axial direction A around the central axis Ax is provided in the insulation nozzle 50. As illustrated in
The opposing energizing contact 12 is a cylindrical conductor and extends along the axial direction A around the central axis Ax. The opposing energizing contact 12 is bonded to an outer periphery of the other end of the exhaust pipe 13 in the axial direction A. An opening edge of the opposing energizing contact 12 in a longitudinal direction projects inward in the radial direction.
The movable energizing contact 22 is a cylindrical conductor and extends along the axial direction A around the central axis Ax. The movable contact portion 20 includes the cylindrical cylinder 23 that houses the operating rod 40. The movable energizing contact 22 is bonded to an end of the cylinder 23 in the axial direction A. The movable energizing contact 22 approaches the opposing energizing contact 12 with movement of the operating rod 40, and as illustrated in
In the configurations described above, in an open state subsequent to a connected state, as illustrated in
Gas flow is generated in the cylinder 23. The cylinder 23 is a cylindrical conductor and extends along the axial direction A around the central axis Ax. The cylinder 23 is fixed with the operating rod 40. That is, the cylinder 23 moves with movement of the operating rod 40.
An annular space is provided between the cylinder 23 and the operating rod 40. The annular space is separated in the axial direction A by a partition wall 24 extending in the radial direction to constitute the thermal puffer chamber 25 and a machine puffer chamber 26. Gas flow to be sprayed to the arc discharge Ad is generated in the thermal puffer chamber 25 and the machine puffer chamber 26. A plurality of through-holes 24a are provided in the partition wall 24. An arc-extinguishing gas can move in and out between the thermal puffer chamber 25 and the machine puffer chamber 26 via the through-holes 24a. The thermal puffer chamber 25 and the machine puffer chamber 26 are an example of a pressure accumulator, and can be also referred to as “pressure accumulator space”.
In the thermal puffer chamber 25, pressure of the arc-extinguishing gas is increased by thermal energy generated by the arc discharge Ad between the opposing arc contact 11 and the movable arc contact 21 as illustrated in
A piston 27 fixed to the airtight container 30 is located on an opposite side to the partition wall 24. The piston 27 is housed in the cylinder 23 slidably in the axial direction A relative to the cylinder 23 and the operating rod 40. As is obvious from comparison between
As illustrated in
The exhaust pipe 13 includes a cylindrical portion 13a and a conical portion 13b. The cylindrical portion 13a is located on the side of the axial direction A of the exhaust pipe 13. The conical portion 13b is located on the other side of the axial direction A of the exhaust pipe 13. The conical portion 13b is formed so as to become narrower gradually as approaching from the cylindrical portion 13a toward an end 13c on the side of the movable contact portion 20. The conical portion 13b can be also referred to as “diffuser”.
As illustrated in
The second shielding wall 15 is formed in a cylindrical shape extending along the axial direction A around the central axis Ax. The second shielding wall 15 extends to the other side of the axial direction A from an outside end in the radial direction of the first shielding wall 14 toward the end 13c of the exhaust pipe 13. The second shielding wall 15 comes in contact with the end 13c of the exhaust pipe 13, that is, the opening edge. That is, a space between the second shielding wall 15 and the conical portion 13b is substantially blocked by the end 13c. The second shielding wall 15 can be in a tubular shape other than the cylindrical shape, and can be for example a tubular shape having a polygonal section. The second shielding wall 15 can be also referred to as “shielding tube”.
A through-hole 15a is provided in the second shielding wall 15. Specifically, a plurality of the through-holes 15a are provided in the second shielding wall 15 along the axial direction A with a space therebetween. These through-holes 15a constitute a row along the axial direction A. According to the present embodiment, a plurality of rows including the through-holes 15a are provided with a space therebetween in a circumferential direction of the exhaust pipe 13. According to the present embodiment, as an example, three through-holes 15a (through-holes 15a1, 15a2, 15a3) are provided along the axial direction A in the respective rows. The through-hole 15a1 is provided adjacent to the first shielding wall 14. The through-hole 15a2 is located away from the first shielding wall 14 than the through-hole 15a1 and an opening area thereof is smaller than the through-hole 15a1. The through-hole 15a3 is located away from the first shielding wall 14 than the through-holes 15a1 and 15a2, and an opening area thereof is larger than the through-hole 15a2.
As illustrated in
As is obvious from
The through-holes 15a are provided in the second shielding wall 15. An inside space of the second shielding wall 15 and an outside space of the second shielding wall 15 are connected via the through-holes 15a.
Therefore, as illustrated in
At this time, the arc-extinguishing gas flowing into the second shielding wall 15 passes between the opposing arc contact 11 and the second shielding wall 15 at a supersonic speed. More specifically, according to the present embodiment, the arc-extinguishing gas passes between the structural object 18 and the second shielding wall 15 at a supersonic speed. After having passed between the structural object 18 including the opposing arc contact 11 and the second shielding wall 15, the arc-extinguishing gas passes through the second shielding wall 15 at a subsonic speed. This is because in a region in the axial direction A in the second shielding wall 15, a sectional area of a space, which becomes a passage of the arc-extinguishing gas, rapidly increases in a region where the structural object 18 is not provided than in a region where the structural object 18 is provided, and as a result, shock waves are generated, thereby decelerating to a subsonic speed. The arc-extinguishing gas at a subsonic speed flows into the through-holes 15a. In
Next, the through-hole 15a is described in detail. If an opening area of the through-hole 15a provided in the second shielding wall 15 is too small, a sufficient amount of arc-extinguishing gas may not be able to flow out to the outside space of the second shielding wall 15. On the contrary, if the opening area of the through-hole 15a is too large, a vortex is likely to be generated at a portion of the through-hole 15a. If a vortex is generated, the flow stagnates in the vortex-generated portion and the state becomes the same as when the opening area of the through-hole 15a is small. Therefore, a sufficient amount of arc-extinguishing gas may not be able to flow out to the outside space of the second shielding wall 15.
Therefore, as illustrated in
Next, an opening area of the through-hole 15a is described with reference to
Next, a case where n through-holes 15a (n is a natural number of 3 or more) are provided sequentially toward the other side of the axial direction A along the axial direction A is described. It is assumed that the opening area of the through-hole 15a1 is S1, the opening area of the through-hole 15a2 is S2, the opening area of the through-hole 15an is Sn, and the total of opening areas of the through-holes 15a1 to 15an is S. At this time, based on a case where there are three through-holes 15a, it is assumed that S1 is S×(0.45×3/n±0.05), and similarly, Sn is S×(0.32×3/n±0.05). The remaining through-holes 15a excluding S1 and Sn are assumed that S2 to Sn−1 have the same opening area and are S×((1−2.31/n)/(n−2)±0.05). The through-holes 15a are provided so that a ratio S1/S of the opening area S1 of each through-hole 15a to the total area S respectively becomes S1/S=0.45×3/n±0.05, S2/S=(1−2.31/n)/(n−2)±0.05, Sn−1/S=(1−2.31/n)/(n−2)±0.05, Sn/S=0.32×3/n±0.05. The area ratio has a margin of 5%, as indicated by ±0.05. By providing this margin, a sufficient amount of arc-extinguishing gas can be caused to flow out to the outside space of the second shielding wall 15 without generating a vortex.
Next, a dimension of the capacity of a space inside of the second shielding wall 15 is described with reference to
Further, in the conventional gas circuit breaker, if an arc-extinguishing gas rapidly flows into the exhaust pipe 13 from the insulation nozzle 50, the pressure of the arc-extinguishing gas rapidly increases in the exhaust pipe 13, to generate a pressure wave. If smooth flow of the arc-extinguishing gas is blocked due to the pressure wave, extinguishing of the arc discharge Ad by the arc-extinguishing gas may not be performed more smoothly or reliably. In this regard, according to the present embodiment, because the first shielding wall 14 and the second shielding wall 15 operate as resistant elements of the gas flow appropriately, a rapid increase of the pressure in the exhaust pipe 13 can be suppressed and generation of the pressure wave and propagation thereof to near the arc contact can be mitigated, as compared to a case where the first shielding wall 14 and the second shielding wall 15 are not provided. Further, according to the present embodiment, a bent passage of an arc-extinguishing gas is formed in the exhaust pipe 13 by the first shielding wall 14 and the second shielding wall 15. Therefore, the first shielding wall 14 and the second shielding wall 15 can be also referred to as “bent-passage forming portion” or “labyrinth forming portion”. The plate-like first shielding wall 14 only needs to intersect with the axial direction A within a range capable of obtaining the effect thereof, and does not need to intersect with the axial direction A completely. Further, the cylindrical second shielding wall 15 only needs to be along the axial direction A within a range capable of obtaining the effect thereof, and does not need to be constant in the entire range in which the sectional shape and the diameter are along the axial direction A.
In the configurations described above, gas flow initially having reached inside of the exhaust pipe 13 from the insulation nozzle 50 flows from the inside of the second shielding wall 15 to the outside of the second shielding wall 15 via the through-holes 15a. According to the present embodiment, because the length h (height) of the through-hole 15a along the axial direction A is within a range from 18 millimeters to 55 millimeters, generation of a vortex is mitigated at the edge of the through-hole 15a, and the gas flow can flow out more smoothly to the outside of the second shielding wall 15 via the through-holes 15a without decreasing a substantial flow-passage sectional area of the through-holes 15a due to the vortex. Therefore, according to the present, embodiment, extinguishing of the arc discharge Ad by an arc-extinguishing gas can be performed more reliably or more efficiently.
Further, if the current value of an interrupting current is large, the pressure ratio between the thermal puffer chamber 25 and the exhaust pipe 13 may become too large to block smooth exhaust of the arc-extinguishing gas. Further, if a gas flow rate from the insulation nozzle 50 to the exhaust pipe 13 increases, pressure is likely to increase in a region close to the first shielding wall 14 inside of the second shielding wall 15. Meanwhile, according to the present embodiment, n through-holes 15a (n is a natural number of 3 or more) are provided along the axial direction A with a space therebetween in the second shielding wall 15. The ratio of the opening area S1 of the through-hole 15a1 closest to the first shielding wall 14, of the n through-holes 15a, to the total (total area) of respective opening areas S1 of the n through-holes 15a is 0.45×3/n±0.05. The ratio of the opening area S3 of the through-hole 15a3 closest to the opposing arc contact 11, of the n through-holes 15a, to the total of the respective opening areas S1 is 0.32×3/n±0.05. Further, the ratio of the opening area S2 of the through-hole 15a2 provided between the through-hole 15a1 closest to the first shielding wall 14 and the through-hole 15a3 closest to the opposing arc contact 11, of the n through-holes 15a, to the total of respective opening areas S1 is (1−2.31/n)/(n−2)±0.05. Accordingly, the gas flow can flow out to the outside of the second shielding wall 15 more smoothly via the through-holes 15a. Consequently, according to the present embodiment, extinguishing of the arc discharge Ad by an arc-extinguishing gas can be performed more reliably or more efficiently.
Further, according to the present embodiment, the opposing arc contact 11 is housed in the second shielding wall 15 and is supported by the second shielding wall 15 via the support member 17. The opposing arc contact 11 and the support member 17 constitute the structural object 18. The length L1 between the end 14a of the first shielding wall 14 on the side of the structural object 18 and the end 18a of the structural object 18 on the side of the first shielding wall 14 along the axial direction A is longer than the length L2 between the end 50b of the insulation nozzle 50 on the side of the first shielding wall 14 and the end 18a of the structural object 18 on the side of the first shielding wall 14 along the axial direction A, in a state in which the movable arc contact 21 and the opposing arc contact 11 are furthermost separated (open) from each other in the axial direction A. Accordingly, a high-temperature arc-extinguishing gas heated by the thermal energy of the arc discharge Ad is mixed with a low-temperature arc-extinguishing gas, thereby enabling to cool the arc-extinguishing gas sufficiently. Therefore, according to the present embodiment, extinguishing of the arc discharge Ad by an arc-extinguishing gas can be performed more reliably or more efficiently.
Further, according to the present embodiment, an arc-extinguishing gas flowing into the second shielding wall 15 passes between the opposing arc contact 11 and the second shielding wall 15 at a supersonic speed. After having passed between the opposing arc contact 11 and the second shielding wall 15, the arc-extinguishing gas passes through the second shielding wall 15 at a subsonic speed, and flows into the through-holes 15a. Accordingly, because the arc-extinguishing gas flows into the through-holes 15a at a subsonic speed, pressure loss can be reduced as compared to a case where the arc-extinguishing gas flows into the through-holes 15a at a supersonic speed. Therefore, according to the present embodiment, extinguishing of the arc discharge Ad by an arc-extinguishing gas can be performed more reliably or more efficiently.
Further, according to the present embodiment, the second shielding wall 15 functions as the guide portion that guides the insulation nozzle 50 in the axial direction A. Therefore, according to the present embodiment, it can be suppressed that the insulation nozzle 50 is deviated from the central axis Ax or is inclined. Further, according to the present embodiment, the insulation nozzle 50 is housed in the second shielding wall 15 movably in the axial direction A with a clearance therebetween. Therefore, for example, by setting the clearance to be relatively narrow such as several micrometers in a diameter difference, leakage of an arc-extinguishing gas along an outer periphery of the insulation nozzle 50 can be suppressed. Therefore, according to the present embodiment, extinguishing of the arc discharge Ad by an arc-extinguishing gas can be performed more reliably or more efficiently.
Further, by the configuration of the gas circuit breaker as described above, the following problem can be solved. That is, if the pressure distribution does not exhibit a monotonous decrease, for example, pressure increases in the middle from the thermal puffer chamber 25 toward a downstream space, and propagation of a pressure wave generated by the arc discharge Ad toward the opposing arc contact 11, and back current or stagnation of the arc-extinguishing gas occur. Consequently, a problem such that outflow of an arc-extinguishing gas is blocked may occur. Such a problem can be solved by the configuration of the gas circuit breaker as described above. Further, by the configuration of the gas circuit breaker as described above, smooth outflow of a high-temperature gas at the time of current cutoff can be realized. Further, by the configuration of the gas circuit breaker as described above, a gas circuit breaker having excellent current cutoff performance can be provided in any current region.
According to the embodiment described above, a case where only the movable contact portion 20 can move in the axial direction A with respect to the airtight container 30 has been illustrated. However, the present invention is not limited thereto. For example, also the opposing contact portion 10 can be configured to be movable in the axial direction A. Further, the thermal puffer chamber 25 and the machine puffer chamber 26 can be integrated with each other, or only one of the thermal puffer chamber 25 and the machine puffer chamber 26 can be provided.
According to the embodiment described above, for example, an example of the configuration in which the opposing contact portion 10 is fixed and only the movable contact portion 20 is moved along the axial direction A has been illustrated. However, the present invention is not limited thereto. For example, a so-called “dual motion mechanism” in which the opposing contact portion 10 is also moved along the axial direction A so that the movable contact portion 20 relatively moves with respect to the opposing contact portion 10 to improve the relative pole (contact portion) opening rate can be used.
Further, according to the embodiment described above, an example of the gas circuit breaker 1 having a configuration in which the thermal puffer chamber 25 being a pressure accumulator space by means of the action of the thermal energy of the arc discharge Ad and the machine puffer chamber 26 being a pressure accumulator space by means of the mechanical action of the drive system are separated by the partition wall 24 and are communicated with each other via the through-holes 24a provided in the partition wall 24 has been illustrated. However, the present invention is not limited thereto. For example, a configuration in which the thermal puffer chamber 25 and the machine puffer chamber 26 are not separated and pressure accumulation is performed by the action of the thermal energy and the mechanical action in the same puffer chamber, a configuration in which pressure accumulation is performed only by the action of the thermal energy, or a configuration in which pressure accumulation is performed only by the mechanical action can be used.
While certain embodiments have been described, these embodiments have been presented by way of example only, and are not intended to limit the scope of the inventions. Indeed, the novel embodiments described herein may be embodied in a variety of other forms; furthermore, various omissions, substitutions and changes in the form of the embodiments described herein may be made without departing from the spirit of the inventions. The accompanying claims and their equivalents are intended to cover such forms or modifications as would fall within the scope and spirit of the inventions.
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