KR101643989B1 - Two-stage output generator - Google Patents

Two-stage output generator Download PDF

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Publication number
KR101643989B1
KR101643989B1 KR1020160016371A KR20160016371A KR101643989B1 KR 101643989 B1 KR101643989 B1 KR 101643989B1 KR 1020160016371 A KR1020160016371 A KR 1020160016371A KR 20160016371 A KR20160016371 A KR 20160016371A KR 101643989 B1 KR101643989 B1 KR 101643989B1
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South Korea
Prior art keywords
power generation
generation module
assembly
rotor
gear
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KR1020160016371A
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Korean (ko)
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임해섭
임현재
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(주)성우테크
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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K16/00Machines with more than one rotor or stator
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/10Structural association with clutches, brakes, gears, pulleys or mechanical starters
    • H02K7/116Structural association with clutches, brakes, gears, pulleys or mechanical starters with gears

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Retarders (AREA)

Abstract

Disclosed is a two-stage output power generator capable of improving power generation efficiency by minimizing the structural complexity and properly responding to external environmental factors. According to an aspect of the present invention, the two-stage output power generator includes: a first power generation module which includes a first rotor assembly and a first stator assembly; a second power generation module which includes a second rotor assembly and a second stator assembly; and a gear assembly which delivers the rotation power of an input shaft to the first or second power generation module. The first rotor assembly includes: a first rotor shaft which is axially combined with the input shaft; and a first rotor bracket on which one or more first coil blocks are mounted and which includes a ring gear engaged with the gear assembly. The gear assembly includes: a sun gear which is placed on the first rotor shaft; one or more planetary gear which is in outer contact with the sun gear and in inner contact with the ring gear; and a carrier which provides a rotation shaft for the planetary gear and includes a carrier shaft. The second rotor assembly includes a second rotor shaft which is axially combined with the carrier shaft.

Description

{TWO-STAGE OUTPUT GENERATOR}

The present invention relates to a two-stage output type generator, and more particularly, to a two-stage output type generator for converting a rotational force applied from the outside into electric energy.

In general, a generator is configured to generate a designed capacity using a power generation source. Therefore, when the generator is powered by a given power source, it is necessary to use a proper torque or other power generation driving force. If the power generation driving force is not below the standard due to an external factor, the power generation is stopped or the power generation efficiency is lowered. Particularly, such a problem can be remarkably exhibited in the renewable energy field where power generation driving force is easily changed due to external environment factors such as hydroelectric power, wind power, and tidal power. Therefore, in many cases, a method of responding to changes in external environmental factors and improving power generation efficiency through the control of the number of revolutions or torque is adopted. In some cases, a method of allowing a plurality of generators having different design capacities to operate irregularly .

However, in the case of the former, there is a limitation in improvement of the power generation efficiency because it follows the design reference value indirectly through the number of revolutions or torque control within the specification of the limited generator. Therefore, in the latter case, It is not a viable alternative because of rising costs. Therefore, along with the rapid growth of the renewable energy field, there is a demand for a power generation means capable of flexibly coping with varying external factors and capable of generating electricity in response to a power source of a larger capacity.

Japanese Unexamined Patent Application Publication No. 2005-312121 (November 4, 2005) Japanese Patent Application Laid-Open No. 10-2011-0028841 (Mar. 23, 2011)

Embodiments of the present invention provide a two-stage output type generator capable of improving power generation efficiency by appropriately responding to external environmental factors while minimizing structural complexity.

According to an aspect of the present invention, there is provided a power module comprising: a first power generation module having a first rotor assembly and a first stator assembly; A second power generation module having a second rotor assembly and a second stator assembly; And a gear assembly for transmitting rotational driving force of an input shaft to the first power generation module or the second power generation module, wherein the first rotor assembly includes: a first rotor shaft axially coupled to the input shaft; And a first rotor bracket having at least one first winding block mounted thereon and having a ring gear engaged with the gear assembly, the gear assembly including: a sun gear provided on the first rotor shaft; One or more planetary gears circumscribed to the sun gear and inscribed in the ring gear; And a carrier provided with a planetary gear and a carrier shaft, wherein the second rotor assembly is provided with a two-stage output generator including a second rotor shaft axially coupled to the carrier shaft .

According to another aspect of the present invention, there is provided an electric motor including: an input shaft to which a rotational driving force is externally applied; The first and second power generation modules being arranged side by side in the axial direction of the input shaft, wherein at least one of the power generation capacity, the rated output, the rated speed, the rated speed and the rated torque is formed differently; A gear assembly selectively transmitting the rotational driving force to a first rotor assembly of the first power generation module or a second rotor assembly of the second power generation module; And a controller for selectively applying an electrical load to the first power generation module or the second power generation module according to each operation condition.

The two-stage output type generator according to the embodiments of the present invention includes the first and second power generation modules having different power generation capacities and the like, and the first power generation module or the second power generation module can be appropriately selected and driven have. Therefore, the two-stage output type generator according to the embodiments of the present invention can cope with operating conditions and changes in the external environment more flexibly, and can contribute to improvement of the overall power generation efficiency of the system.

In addition, the two-stage output type generator according to the embodiments of the present invention can easily perform the drive switching between the power generation modules through the electrical load control, .

The two-stage output type generator according to the embodiments of the present invention can be formed in an intuitive and simple structure in which the mutually separated first and second power generation modules are sequentially coupled in the axial direction of the input shaft, Switching between 1 and 2 power generation modules and selective drive can be done through gear assemblies inside the device rather than complex link structure or control mechanism, maximizing power generation efficiency and minimizing the structural complexity.

Further, in the two-stage output type generator according to the embodiments of the present invention, a separate acceleration and deceleration means may be omitted by a gear assembly including a planetary gear structure, and each rotor bracket is provided with a modular- It is easy to change the power generation capacity or the like through replacement of the winding block in an assembled manner.

1 is an external perspective view of a two-stage power generator according to an embodiment of the present invention.
2 is a side view of the two-stage output type generator shown in Fig.
3 is a partially cutaway perspective view showing the interior of the two-stage power generator shown in FIG.
4 is an enlarged perspective view of the first power generation module shown in FIG.
5 is a perspective view showing the first rotor assembly and the second stator assembly shown in Fig.
6 is an enlarged perspective view showing the gear assembly shown in Fig.
7 is a perspective view showing a state in which the outer housing is removed from the two-stage output generator shown in FIG.
8 is a side view of the two-stage output generator shown in Fig.
9 is an enlarged perspective view of the second power generation module shown in FIG.
FIG. 10 is a conceptual diagram for explaining the operation of the two-stage output type generator shown in FIGS. 1 to 9. FIG.
Fig. 11 is a block diagram showing a schematic control process of the two-stage output generator shown in Figs. 1 to 9. Fig.

Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings. It is to be understood, however, that the following examples are provided to facilitate understanding of the present invention, and the scope of the present invention is not limited to the following examples. In addition, the following embodiments are provided to explain the present invention more fully to those skilled in the art. Those skilled in the art will appreciate that those skilled in the art, Will be omitted.

1 is an external perspective view of a two-stage output type generator G according to an embodiment of the present invention. 2 is a side view of the two-stage output type generator G shown in Fig. For convenience of explanation, it is noted that the side view of FIG. 2 shows a part of the outer housing H removed from the external perspective view of FIG.

Referring to FIGS. 1 and 2, the two-stage output type generator G according to the present embodiment may include an input shaft R to which a rotational driving force is applied. The rotational driving force applied to the input shaft R may be provided by various power sources, and is not limited to a specific power source. For example, the rotational driving force may be generated and provided by various types of power generation sources such as hydro, wind, tidal, and gas turbines. However, as described below, the two-stage output type generator G according to the present embodiment is capable of achieving high power generation efficiency in spite of variations in the number of revolutions and torque of the input shaft R, It can function more effectively in the renewable energy field where the driving force can be varied.

Meanwhile, the two-stage output type generator G according to the present embodiment may include the first and second power generation modules 10 and 20. The first and second power generation modules 10 and 20 may be arranged in the axial direction with respect to the input shaft R and may be respectively shielded by the outer housing H as shown in FIG. The input shaft R, the first power generation module 10, and the second power generation module 20 may be sequentially arranged in the axial direction of the input shaft R and may be axially coupled to each other. Therefore, the rotational driving force applied to the input shaft R may be provided to the first power generation module 10 and may be supplied to the second power generation module 20 via the first power generation module 10. The driving force transmission between the first and second power generation modules 10 and 20 may be performed through a gear assembly 30 described later.

Further, the first and second power generation modules 10 and 20 may be formed to have different power generation capacities, respectively. Alternatively, the first and second power generation modules 10 and 20 may be formed so that at least one of the rated capacity, the rated speed, and the rated torque is different. Furthermore, any one of the first and second power generation modules 10 and 20 can be selectively driven according to operating conditions. For example, the first power generation module 10 can be selectively driven under the first operation condition, and the second power generation module 20 can be selectively driven under the second operation condition different from the first operation condition.

The difference in the power generation capacity and the like as well as the selective drive enable the power generation modules 10 and 20 capable of achieving optimum performance (for example, power generation efficiency) under the respective operating conditions to be selectively driven to improve the overall power generation efficiency I will. In this embodiment, such a selective drive is performed by a drive force transmission structure between the first and second power generation modules 10 and 20 by the gear assembly 30 and a power transmission structure between the first power generation module 10 and the second power generation module 20 As shown in FIG. That is, in this embodiment, there is a technical advantage in that the device complexity can be minimized while taking the selective driving method of the first and second power generation modules 10 and 20 according to the respective operating conditions. This will be explained in detail in the following description of the detailed configuration.

FIG. 3 is a partially cutaway perspective view showing the interior of the two-stage output generator G shown in FIG. 1. FIG. 4 is an enlarged perspective view of the first power generation module 10 shown in FIG. 5 is a perspective view showing the first rotor assembly 12 and the second stator assembly 21 shown in Fig.

3 to 5, the first power generation module 10 may include a first stator assembly 11. The first stator assembly 11 may be fixed to the housing or the like so that the first stator assembly 11 is rotationally restrained with respect to the axial direction of the input shaft R. [ 5B, the first stator assembly 11 may be formed in a hollow cylindrical shape so that the first rotor assembly 12 may be disposed therein, and the first stator core 11a and the second stator core 11b may be integrally formed. And a first stator coil 11b wound on the first stator coil 11b.

The first power generation module 10 may include a first rotor assembly 12. The first rotor assembly 12 may be disposed inside the hollow cylindrical first stator assembly 11 and may be rotationally driven with respect to the first stator assembly 11 about the axial direction of the input shaft R. [ The first rotor assembly 12 includes a first rotor shaft 12a to which a rotational driving force is applied from an input shaft R and a second rotor shaft 12b that is rotationally driven through a gear assembly 30 coupled to the first rotor shaft 12a. A rotor bracket 12b and a first winding block 12c. 3 and 4, the first rotor shaft 12a may be rotatably supported by at least one bearing, and may be axially coupled to the input shaft R so as to rotate together with the input shaft R. [ Alternatively, the first rotor shaft 12a may extend from the input shaft R and be integrally formed with the input shaft R.

As shown in FIG. 5A, the first rotor bracket 12b may be formed in a hollow cylindrical shape so that the first rotor shaft 12a and the gear assembly 30 to be described later are disposed therein. For convenience of explanation, it is noted that FIG. 5 (a) shows a part of the first rotor bracket 12b and the first winding block 12c is omitted. The first rotor bracket 12b may be provided with a ring gear 12d on its inner peripheral surface. The ring gear 12d is engaged with the planetary gear 32 of the gear assembly 30 to be described later and can transmit the rotational driving force to the first rotor bracket 12b and the first winding block 12c.

A plurality of first winding blocks 12c may be provided, and each first winding block 12c may be coupled to an outer circumferential surface of the first rotor bracket 12b. Each first winding block 12c may be disposed axially on the outer circumferential surface of the first rotor bracket 12b and may be constituted by a first bobbin 12e and a first rotor coil 12f wound on the first bobbin 12e. The plurality of first winding blocks 12c may be disposed along the circumferential direction on the outer circumferential surface of the first rotor bracket 12b so as to be radially formed as a whole. A first slot groove 12g may be formed on an outer circumferential surface of the first rotor bracket 12b to which the first winding block 12c is coupled. A plurality of the rotor brackets 12b may be formed along the circumferential direction on the outer circumferential surface of the first rotor bracket 12b to correspond to the first winding block 12c. Such use of the first winding block 12c makes it possible to easily change the power generation capacity or the like according to the number of windings and the like, thereby enabling a more efficient system configuration.

3, the two-stage output type generator G according to the present embodiment may further include a gear assembly 30. As shown in FIG. The gear assembly 30 transmits the rotational driving force applied to the input shaft R to the first power generation module 10 or the second power generation module 20 to generate the power of the first power generation module 10 or the second power generation module 20 Thereby enabling selective driving.

6 is an enlarged perspective view showing the gear assembly 30 shown in Fig.

6, the gear assembly 30 includes a sun gear 31 provided on the first rotor shaft 12a, a plurality of planetary gears 32 engaged with the sun gear 31, and a carrier 33 Lt; / RTI >

The sun gear 31 can be rotated together with the first rotor shaft 12a. Therefore, while the rotational driving force is applied to the input shaft R, the sun gear 31 can be driven to rotate continuously. The plurality of planetary gears 32 are engaged with the sun gear 31 and can be revolved around the outer periphery of the sun gear 31 or rotated in place. The plurality of planetary gears 32 can be engaged with the ring gear 12d by inserting into the ring gear 12d on the inner circumferential surface of the first rotor bracket 12b. Therefore, when the first power generation module 10 is selectively driven, the rotational driving force applied through the input shaft R is transmitted to the first rotor shaft 12a, the sun gear 31, the plurality of planetary gears 32 and the ring gear 12d To the first rotor bracket 12b and the first winding block 12c.

The carrier 33 is coupled to the plurality of planetary gears 32 to provide rotation shafts to the planetary gears 32 for rotation and to transmit rotational driving force to the second power generation modules 20 at the rear And a carrier shaft 33a. Therefore, when the second power generation module 20 is selectively driven, the rotational driving force applied through the input shaft R is transmitted to the first rotor shaft 12a, the sun gear 31, the plurality of planetary gears 32, And the carrier shaft 33a to the second power generation module 20 at the rear end.

The gear assembly 30 selectively drives the first power generation module 10 or the second power generation module 20 through the revolution or rotation of the planetary gear 32. That is, the gear assembly 30 rotates or rotates the planetary gear 32 in accordance with the operating conditions and the electrical load applied to the power generation modules 10 and 20, whereby the first rotor assembly 12 or The second rotor assembly 22 to be described later is selectively rotated to generate electricity in the first power generation module 10 or the second power generation module 20. Therefore, the two-stage output type generator G according to the present embodiment selectively drives the first power generation module 10 or the second power generation module 20 according to the operating conditions through the gear assembly 30 while minimizing the structural complexity So that the power generation efficiency can be improved.

In addition, since the gear assembly 30 includes a planetary gear structure capable of increasing and decreasing speed, there is no need for a separate accelerator and decelerator outside the apparatus. Therefore, the two-stage output type generator G according to the present embodiment is advantageous in that the acceleration and deceleration means are integrated inside the device, and the entire system and the configuration of the external device can be simplified.

7 is a perspective view showing a state in which the outer housing is removed from the two-stage output type generator G shown in Fig. 8 is a side view of the two-stage output type generator G shown in Fig. 9 is an enlarged perspective view of the second power generation module 20 shown in FIG. It is noted that the first power generation module 10 is omitted in FIG. 8 for convenience of explanation.

Referring to FIGS. 7 to 9, the two-stage output type generator G according to the present embodiment may include a second power generation module 20. The second power generation module 20 may be configured as one independent power generation unit that is different from the first power generation module 10 and may be configured such that the first power generation module 10 and the power generation capacity are different from each other have. This is to improve the power generation efficiency by selectively driving the first power generation module 10 or the second power generation module 20 according to operating conditions.

The second power generation module 20 may include a second rotor assembly 22 and a second stator assembly 21. The second stator assembly 21 includes a second stator core 21a and a second stator coil 21b and may be formed in a hollow cylindrical shape and may be fixed to a housing or the like so as to be rotationally restrained with respect to the axial direction.

The second rotor assembly 22 may include a second rotor shaft 22a, a second rotor bracket 22b, and a plurality of second winding blocks 22c. At this time, the second rotor shaft 22a is axially coupled with the carrier shaft 33a through the coupler C or the like and can receive the rotational driving force from the carrier shaft 33a. The second rotor bracket 22b may be coupled to the second rotor shaft 22a and rotated together with the second rotor shaft 22a and the plurality of second winding blocks 22c may be coupled to the second rotor bracket 22b In the circumferential direction. A plurality of second slot grooves 22d for coupling the second winding block 22c may be provided on the outer circumferential surface of the second rotor bracket 22b as necessary.

The second power generation module 20 is configured such that the rotational driving force is transmitted to the second rotor shaft 22a by the carrier shaft 33a and the second rotor assembly 22 is rotated about the second stator assembly 21 The power generation is performed while being rotationally driven.

Fig. 10 is a conceptual diagram for explaining the operation of the two-stage output type generator G shown in Figs. 1 to 9. Fig. 10 (a) shows the operation when the first power generation module 10 is driven, and FIG. 10 (b) conceptually shows the operation when the second power generation module 20 is driven Leave.

In the meantime, as described above, the first power generation module 10 or the second power generation module 20 is selectively driven in accordance with each operating condition of the two-stage output type generator G according to the present embodiment. Hereinafter, the operating condition in which the first power generation module 10 is driven is referred to as a first operating condition, and the operating condition in which the second power generation module 20 is driven is referred to as a second operating condition. At this time, the selective drive according to each operating condition can be set in consideration of power generation efficiency under the corresponding operating condition of each power generation module 10, 20, and the like.

First, the operation when the first power generation module 10 is driven will be described with reference to FIG. 10 (a) and FIG. 7 described above. The first rotor shaft 12a and the sun gear 31 coupled to the first rotor shaft 12a are rotated. As the sun gear 31 rotates, a plurality of planetary gears 32 meshed with the sun gear 31 are driven. At this time, the respective planetary gears 32 can be rotated in a state in which idle rotation is restricted.

The operation of the planetary gear 32 as described above can be realized by applying a high power generation load to the second power generation module 20 connected to the carrier shaft 33a to generate a rotational resistance in the second rotor shaft 22a. That is, if a power generation load is electrically applied to the second power generation module 20, rotational resistance is generated (i.e., electrically braked) in the second rotor assembly 22 and the second rotor shaft 22a, The axial rotation of the carrier shaft 33a and the carrier 33 connected to the second rotor shaft 22a is restrained. Therefore, each of the planet gears 32 can be rotated only by the carrier 33 with the idle motion restricted.

On the other hand, when the respective planetary gears 32 are rotated, the first rotor bracket 12b engaged with the planetary gear 32 is driven to rotate about the sun gear 31 through the ring gear 12d on the inner peripheral surface, The first rotor assembly 12 is rotated with respect to the first stator assembly 11 in accordance with the rotation of the first rotor bracket 12b and power generation is performed in the first power generation module 10.

Next, the operation when the second power generation module 20 is driven will be described with reference to FIG. 10 (b) and FIG. 7 described above. The rotational driving force of the input shaft R is transmitted to the first rotor shaft 12a and the sun gear 31 when the operating condition is changed to the second operating condition different from the first operating condition. This is the same as the operation under the above-described first operating condition.

That is, in the two-stage output type generator G according to the present embodiment, an external rotational driving force is continuously applied to the input shaft R. The first rotor shaft 12a and the sun gear 31 are connected to the first power generation It can be continuously rotated during operation regardless of the selective drive of the module 10 or the second power generation module 20. [ Therefore, the two-stage output type generator G according to the present embodiment is not required to stop the operation of the apparatus or to change the connection relationship for switching to the power generation modules 10 and 20, The switching to the power generation modules 10 and 20 and the selective driving can be performed.

Meanwhile, when the second power generation module 20 is driven, as the sun gear 31 rotates, the plurality of planetary gears 32 can be idly rotated. At this time, the revolution of the planetary gear 32 can be induced by applying a high power generation load to the first power generation module 10 to generate a rotational resistance in the first rotor bracket 12b. That is, in this operation example, in contrast to the above-described first operating condition, the electric power generation load may be applied to the first power generation module 10, thereby causing a rotational resistance to be generated in the first rotor bracket 12b And the planetary gears 32 revolve about the sun gear 31 with the ring gear 12d being restricted in rotation. As the planetary gear 32 revolves, the carrier 33 and the carrier shaft 33a are rotationally driven about the axial direction of the input shaft R. The rotation of the carrier shaft 33a is transmitted to the second rotor shaft 22a to the second power generation module 20 so that the second power generation module 20 generates power.

As described above, the two-stage power generator (G) according to the present embodiment is provided with the first and second power generation modules (10, 20) having different power generation capacities and rated speeds and are suitable for power generation efficiency The power generation modules 10 and 20 are selected and driven. Particularly, the switching between the first and second power generation modules 10 and 20 is performed by applying an electrical load to the first power generation module 10 or the second power generation module 20 in a state in which the rotational driving force is continuously applied to the input shaft R And can be switched during operation without stopping the operation of the apparatus. In addition, although the plurality of power generation modules 10 and 20 and the switching means (i.e., the gear assembly 30) are integrated to improve the power generation efficiency, in order to minimize the structural complexity, , Durability, maintenance, and parts replacement.

On the other hand, in the case of this embodiment, the case where the switching between the first and second power generation modules 10 and 20 or the selective driving is performed by the electrical braking through the power generation load is exemplified. However, It can be said that.

In addition, the two-stage output type generator G according to the present embodiment may further include a control unit. The control unit can control the switching between the first and second power generation modules 10 and 20 and the selective driving according to each operating condition set by the user.

Fig. 11 is a block diagram showing a schematic control process of the two-stage output type generator G shown in Figs. 1 to 9. Fig.

Referring to FIG. 11, when the rotational driving force is applied to the input shaft R, the controller may check the generator state whether the load control power is equal to or greater than a reference value. As a result of the check, if the load control electric power is lower than the reference value, the controller can receive the load control electric power through the uninterruptible power supply (UPS).

If the load control power is equal to or greater than the reference value, the control unit may analyze at least one of the rotational speed, the rotational speed, and the rotational torque of the input shaft R to match the predetermined operating condition. At this time, the respective operating conditions can be set in consideration of the power generation capacity, rated speed, torque, etc. of the first and second power generation modules 10 and 20, and the first operating condition in which the first power generation module 10 is driven, 2 power generation module 20 is driven.

When the first operation condition is matched (the first power generation requirement is satisfied), the control unit applies a power generation load to the second power generation module 20 through the load control power and electrically brakes the second power generation module 20. [ In this case, the rotation of the carrier 33 is restricted so that the rotational driving force applied to the input shaft R rotates the respective planetary gears 32, and correspondingly, the first rotor assembly 12 is driven to rotate 1 power generation module 10 (Fig. 7 (a)). In addition, the control unit analyzes the power generation amount and transmits the generated power to the UPS or the power grid (transmission tower).

On the other hand, when the rotational speed of the input shaft R is analyzed to find that it matches the second operating condition (satisfying the second-stage power generation requirement), the control unit applies a power generation load to the first power generation module 10 via the load control power Thereby electrically braking the first power generation module 10. The rotation of the first rotor bracket 12b can be restricted and the rotational driving force of the input shaft R is transmitted to the carrier shaft 33a through the idle motion of the respective planetary gears 32 b)). Accordingly, the second rotor shaft 22a and the second rotor assembly 22 are rotationally driven to generate electric power from the second power generation module 20.

As described above, the two-stage output type generator G according to the embodiments of the present invention includes the first and second power generation modules 10 and 20 having different power generation capacities and the like, So that the module 10 or the second power generation module 20 can be appropriately selectively driven. Therefore, the two-stage output type generator G according to the embodiments of the present invention can cope more flexibly with operating conditions and external environment changes, and can contribute to enhancement of the overall power generation efficiency of the system. In addition, the drive switching between the power generation modules 10 and 20 can be performed easily through the electric load control, and it is advantageous in that switching between the power generation modules 10 and 20 in the operating state and switching of continuous driving are very easy.

The two-stage output type generator G according to the embodiments of the present invention has a structure in which the first and second power generation modules 10 and 20 of mutually separated form are sequentially coupled in the axial direction of the input shaft R, And the switching between the first and second power generation modules 10 and 20 and the selective driving can be accomplished through the gear assembly 30 disposed inside the apparatus rather than a complicated link structure or control mechanism, The efficiency can be maximized while the structural complexity can be minimized.

Furthermore, the two-stage output type generator G according to the embodiments of the present invention can omit the additional acceleration and deceleration means by the gear assembly 30 including the planetary gear structure, and the rotor brackets 12b, 22b are modularly shaped and the winding blocks 12c, 22c are assembled and assembled. It is also easy to change the power generation capacity or the like by replacing the winding blocks 12c, 22c.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, many modifications and changes may be made by those skilled in the art without departing from the spirit and scope of the invention as defined in the appended claims. The present invention can be variously modified and changed by those skilled in the art, and it is also within the scope of the present invention.

G: Two-speed output type generator R: Input shaft
10: first power generation module 12: first power assembly
12a: first rotor shaft 12b: first rotor bracket
12d: ring gear 12c: first winding block
11: first stator assembly 11a: first stator core
11b: first stator coil 20: second power generation module
22: second rotor assembly 22a: second rotor shaft
22b: second rotor bracket 22c: second winding block
21: second stator assembly 21a: second stator core
21b: second stator coil 30: gear assembly
31: sun gear 32: planetary gear
33: carrier 33a: carrier shaft

Claims (6)

A first power generation module (10) having a first electronic assembly (12) and a first stator assembly (11);
A second power generation module (20) having a second rotor assembly (22) and a second stator assembly (21); And
And a gear assembly (30) for transmitting rotational driving force of the input shaft (R) to the first power generation module (10) or the second power generation module (20)
The first rotor assembly (12)
A first rotor shaft (12a) axially coupled to the input shaft (R); And
And a first rotor bracket (12b) having at least one first winding block (12c) mounted thereon and having a ring gear (12d) meshing with the gear assembly (30)
The gear assembly (30)
A sun gear 31 provided on the first rotor shaft 12a;
One or more planet gears (32) circumscribed to the sun gear (31) and inscribed in the ring gear (12d); And
And a carrier (33) that provides a rotation shaft to the planetary gear (32) and that has a carrier shaft (33a)
The second rotor assembly (22)
And a second rotor shaft (22a) axially coupled to the carrier shaft (33a)
In the first operating condition, the first power generation module 10 is selectively driven,
The second power generation module 20 is selectively driven under a second operating condition different from the first operating condition,
In the first operating condition, the planetary gear 32 rotates to rotate the first rotor assembly 12,
Wherein the planetary gear (32) is revolved to rotate the second rotor assembly (22) under the second operating condition.
A first power generation module (10) having a first electronic assembly (12) and a first stator assembly (11);
A second power generation module (20) having a second rotor assembly (22) and a second stator assembly (21); And
And a gear assembly (30) for transmitting rotational driving force of the input shaft (R) to the first power generation module (10) or the second power generation module (20)
The first rotor assembly (12)
A first rotor shaft (12a) axially coupled to the input shaft (R); And
And a first rotor bracket (12b) having at least one first winding block (12c) mounted thereon and having a ring gear (12d) meshing with the gear assembly (30)
The gear assembly (30)
A sun gear 31 provided on the first rotor shaft 12a;
One or more planet gears (32) circumscribed to the sun gear (31) and inscribed in the ring gear (12d); And
And a carrier (33) that provides a rotation shaft to the planetary gear (32) and has a carrier shaft (33a)
The second rotor assembly (22)
And a second rotor shaft (22a) axially coupled to the carrier shaft (33a)
In the first operating condition, the first power generation module 10 is selectively driven,
The second power generation module 20 is selectively driven under a second operating condition different from the first operating condition,
Under the first operating condition, an electrical load is applied to the second power generation module 20 to generate a rotational resistance in the carrier 33,
Wherein an electrical load is applied to the first power generation module (10) under the second operating condition to generate rotational resistance in the ring gear (12d).
The method according to claim 1 or 2,
Wherein the first and second power generation modules (10, 20) are formed such that at least one of a power generation capacity, a rated output, a rated speed, a rated speed and a rated torque is different.
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KR1020160016371A 2016-02-12 2016-02-12 Two-stage output generator KR101643989B1 (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101920890B1 (en) * 2018-06-18 2018-11-21 (주)성우테크 Generator and Control Method for the same
KR101920889B1 (en) * 2018-06-18 2018-11-21 (주)성우테크 Generator and Control Method for the same
KR102026207B1 (en) * 2019-03-28 2019-11-04 (주)성우테크 Generator and Control Method for the same
WO2019245064A1 (en) * 2018-06-18 2019-12-26 (주)성우테크 Generator and generator control method

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JP2003028034A (en) * 2001-07-16 2003-01-29 Hitachi Unisia Automotive Ltd Starter-generator
JP2005312121A (en) 2004-04-19 2005-11-04 Toyota Motor Corp Rotary electric machine having planet change gear and method for manufacturing rotor supporting shaft constituting rotary electric machine
JP2008182875A (en) * 2006-10-26 2008-08-07 Deere & Co Control of dual rotor electromagnetic apparatus
KR20110028841A (en) 2009-09-14 2011-03-22 (주)에스아이엠 Apparatus of power transmission and generation

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Publication number Priority date Publication date Assignee Title
JP2003028034A (en) * 2001-07-16 2003-01-29 Hitachi Unisia Automotive Ltd Starter-generator
JP2005312121A (en) 2004-04-19 2005-11-04 Toyota Motor Corp Rotary electric machine having planet change gear and method for manufacturing rotor supporting shaft constituting rotary electric machine
JP2008182875A (en) * 2006-10-26 2008-08-07 Deere & Co Control of dual rotor electromagnetic apparatus
KR20110028841A (en) 2009-09-14 2011-03-22 (주)에스아이엠 Apparatus of power transmission and generation

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101920890B1 (en) * 2018-06-18 2018-11-21 (주)성우테크 Generator and Control Method for the same
KR101920889B1 (en) * 2018-06-18 2018-11-21 (주)성우테크 Generator and Control Method for the same
WO2019245064A1 (en) * 2018-06-18 2019-12-26 (주)성우테크 Generator and generator control method
KR102026207B1 (en) * 2019-03-28 2019-11-04 (주)성우테크 Generator and Control Method for the same

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