Generators, such as aircraft generators, require a brushless architecture for voltage control as the speed fluctuates along with fast voltage disconnection in failure modes (e.g., armature winding inter-turn short circuit). Contemporary implementations utilize a wound-field synchronous generator with brushless exciter and permanent magnet sub-exciter (e.g., three-machine set); yet, these contemporary implementations have limited performance.
According to an embodiment, a generator comprises a rotor comprising a plurality of slots; a three-phase winding configured to produce a first magnetic field; and an excitation winding comprising a material filling in the plurality of slots and configured to produce a second magnetic field, wherein a rotation of the generator occurs in accordance with an interaction between the first and second magnetic fields of the three-phase winding and the excitation winding.
Additional features and advantages are realized through the techniques of the present invention. Other embodiments and aspects of the invention are described in detail herein and are considered a part of the claimed invention. For a better understanding of the invention with the advantages and the features, refer to the description and to the drawings.
The subject matter which is regarded as the present disclosure is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the present disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
In view of the above, embodiments here relate to variable speed constant frequency applications where a doubly-fed alternating current generator provides better performance than contemporary implementations.
Turning now to
The rotor 114 of the doubly-fed alternating current generator 110 is driven by the prime mover 112. As the rotor 114 rotates, an alternating voltage is induced in the three-phase winding 116 by a magnetic flux of the rotor 114. The stator excitation winding 118 excites the rotor 114 with magnetic flux. That is, the rotor 114 locks in with a rotating magnetic field of the three-phase windings 116 and rotates along with it. A three-phase current carried by the three-phase winding 116 produces the rotating magnetic field. Note that once the rotor 114 locks in with the rotating magnetic field, the doubly-fed alternating current generator 110 can be referred to as in a synchronization operation. Once the rotor 114 is in operation, the frequency in the three-phase winding 116 is dependent on the rotor 114 speed. The controlled rectifier 122 converts alternating current power from the three-phase grid 105 to a direct current field excitation current. The current control 124 adjusts the direct current field excitation current to produce an output current to the excitation winding 118. The microcontroller can be a small computer on a single integrated chip including a processor core, memory, and programmable instructions. The microcontroller 126 is configured to monitor real time voltage and current of all windings and provide a control signal to the current control 124 based on this monitoring (in accordance with the programmable instructions). This control signal causes the current control 124 to adjust the direct current field excitation current. Thus, the excitation system 120 can provide a stable current to the excitation winding 118 during excitation.
The rotor 114, driven by the prime mover 112, induces an alternating voltage in the three-phase winding 116. The excitation winding 118 excites the magnetic flux in the rotor 114. In an embodiment, the three-phase windings 116 can include 2pp poles, be referred to as a power winding (three-phase winding 116), and be directly connected to the three-phase grid 105. Further, the excitation winding 118 can include 2pc poles, be referred to as a control winding, and provide excitation for the environment 100. The rotor 114 with magnetic flux barriers-replaces contemporary implementations of cage windings, such that the bars and segments of end rings of a cage winding can be divided into rotor nests. The rotor 114 can also be equipped with additional cage winding (hybrid rotor). For instance, the rotor can be a combination of magnetic flux barriers as described below and cage windings (“nests”).
A number of rotor nests can be calculated according to Equation 1.
N=pp+pc Equation 1
where N is the number of rotor nests and pp and pc are the number of pole pairs of the power and control winding, respectively. A rotational speed n can be determined by frequencies fp and fc and the numbers of pole pairs pp and pc of the power and control winding, respectively, according to Equation 2. In the case of direct current excitation of the winding 118, the frequency fc=0.
The rotor 114 can be of reluctance type with magnetic flux barriers (see
pp≠pc Equation 3
From reliability point of view, it is better to place both the armature three-phase winding and the field excitation winding in the stator slots, embodiments of which are now described with respect to
In view of the above,
Technical effects and benefits of embodiments herein include a rotor with magnetic flux barriers that are an easy to manufacture structure with a high reliability and high electromechanical energy conversion efficiency. That is, no rotor excitation losses occur to the magnetic flux barriers as any power losses are dissipated in the stator (which also allows for good heat transfer).
Further, the technical effects and benefits of embodiments herein include a brushless design in which a direct current is delivered to the stator field excitation winding while the rotor is not fed with electric current; an adjustable field excitation current where an output rms voltage of this generator system is stable; and regulated reactive power. Note that the maximum and minimum field excitation current can be controlled (lowered or limited) to prevent over-excitation and under-excitation problems. Also, when a malfunction or failure occurs inside a generator, e.g., inter-turn short circuit, embodiments herein can cut off the field excitation current to prevent damaging corresponding or coupled electrical systems.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the present disclosure is not limited to such disclosed embodiments. Rather, the present disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the present disclosure. Additionally, while various embodiments of the present disclosure have been described, it is to be understood that aspects of the present disclosure may include only some of the described embodiments. Accordingly, the present disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
2966623 | Mishkin | Dec 1960 | A |
4477767 | Cotzas | Oct 1984 | A |
5493201 | Baker | Feb 1996 | A |
5512813 | Uchinami | Apr 1996 | A |
5594322 | Rozman | Jan 1997 | A |
5656922 | LaVelle | Aug 1997 | A |
5719487 | Sato | Feb 1998 | A |
5886504 | Scott | Mar 1999 | A |
6018200 | Anderson | Jan 2000 | A |
6118186 | Scott | Sep 2000 | A |
6160384 | Inaba | Dec 2000 | A |
6784634 | Sweo | Aug 2004 | B2 |
6933625 | Feddersen | Aug 2005 | B2 |
8432137 | Rozman | Apr 2013 | B2 |
20010002777 | Ravinovici et al. | Jun 2001 | A1 |
20050162030 | Shah et al. | Jul 2005 | A1 |
20100181969 | Gieras | Jul 2010 | A1 |
20110133703 | Rozman | Jun 2011 | A1 |
20160056674 | Buettner | Feb 2016 | A1 |
Number | Date | Country |
---|---|---|
103166402 | Jun 2013 | CN |
2301143 | Nov 2011 | EP |
101318152 | Oct 2013 | KR |
WO 2009150464 | Dec 2009 | WO |
2014166555 | Oct 2014 | WO |
WO 2014166555 | Oct 2014 | WO |
Entry |
---|
Extended European Search Report for EP Application No. 16197258.3-1809, dated Mar. 24, 2017, pp. 1-29. |
Number | Date | Country | |
---|---|---|---|
20170126158 A1 | May 2017 | US |