AGN 034 Alternator Reactance

Similar documents
AGN 005 Fault Currents and Short Circuit Decrement Curves

Time constants ( s ) Resistance. Other data - Class H /6600 V kva. Efficiencies ( % )(3 phase - Classe H V kva)

AGN 124 AVR Power Supplies

PI734F - Winding 07. Technical Data Sheet APPROVED DOCUMENT

PI734F - Winding 28. Technical Data Sheet APPROVED DOCUMENT

AGN 124 AVR Power Supplies

PM734D - Winding 312. Technical Data Sheet APPROVED DOCUMENT. Generator Solutions AS

PM734F - Winding 312. Technical Data Sheet APPROVED DOCUMENT

S4L1S-D4 Wdg.17 - Technical Data Sheet

PI734E - Winding 312. Technical Data Sheet APPROVED DOCUMENT

PI734C - Winding 312. Technical Data Sheet APPROVED DOCUMENT

PI734B - Winding 312. Technical Data Sheet APPROVED DOCUMENT

S4L1D-G41 Wdg Technical Data Sheet

WDG 71 - Technical Data Sheet

WDG 61 - Technical Data Sheet

WDG 51 - Technical Data Sheet

WDG 12 - Technical Data Sheet

WDG 12 - Technical Data Sheet

WDG 83 - Technical Data Sheet

WDG 12 - Technical Data Sheet

PM734B - Technical Data Sheet. Generator Solutions AS

S0L1-J1 - Technical Data Sheet

WDG 13 - Technical Data Sheet

WDG 12 - Technical Data Sheet

WDG 07 - Technical Data Sheet

PI734C - Technical Data Sheet

PI734A - Technical Data Sheet

440 (12) 416 (12) 416 (12) 440 (12)

AGN Japanese National Electrical Distribution System

Application Guidance Notes: Technical Information from Cummins Generator Technologies

PARTNER ALTERNATORS LSA 40-4 Pole

AGN 022 Conditions for Parallel Operation

Generator Advanced Concepts

Low Voltage alternators - 4 pole LSA 47.2

PARTNER ALTERNATORS LSA Pole

TAL 049 Low Voltage Alternator - 4 pole

TAL 047 Low Voltage Alternator - 4 pole

LSA Pole. R 726 Mains paralleling

Application Guidance Notes: Technical Information from Cummins Generator Technologies

LSA R & LSA H 49.1 Low Voltage Alternators - 4 pole

ALTERNATOR TECHNICAL DESCRIPTION 1. LSA 53.2 XL13 / 4p. Chargé d'affaire : Karthikeyan GN 1 Moteurs Leroy-Somer +33 (0) xx

INTERCONNECTION REQUEST FOR A LARGE GENERATING FACILITY

AGN 026 Harmonic Voltage Distortion

Low Voltage alternators - 4 pole LSA 46.2

TAL 044 Low Voltage Alternator - 4 pole

Spec Information. Reactances Per Unit Ohms

CHAPTER 2 ELECTRICAL POWER SYSTEM OVERCURRENTS

Spec Information. Reactances Per Unit Ohms

GENERATOR INTERCONNECTION APPLICATION FOR ALL PROJECTS WITH AGGREGATE GENERATOR OUTPUT OF MORE THAN 2 MW

Form B. Connection Impact Assessment Application Form Distribution System

APPENDIX 1 to LGIP INTERCONNECTION REQUEST FOR A LARGE GENERATING FACILITY

GENERATOR INTERCONNECTION APPLICATION FOR ALL PROJECTS WITH AGGREGATE GENERATOR OUTPUT OF MORE THAN 150 KW BUT LESS THAN OR EQUAL TO 550 KW

A Practical Guide to Free Energy Devices

GENERATOR DATA JANUARY 30, 2015

Sizing Generators for Leading Power Factor

GENERATOR INTERCONNECTION APPLICATION Category 3 For All Projects with Aggregate Generator Output of More Than 150 kw but Less Than or Equal to 550 kw

GENERATOR INTERCONNECTION APPLICATION Category 5 For All Projects with Aggregate Generator Output of More Than 2 MW

TABLE OF CONTENT

Code No: R Set No. 1

Impact Assessment Generator Form

NORTH CAROLINA INTERCONNECTION REQUEST. Utility: Designated Contact Person: Address: Telephone Number: Address:

SYNCHRONOUS MACHINES

Initial Application Form for Connection of Distributed Generation (>10kW)

Connection Impact Assessment Application

Issued: September 2, 2014 Effective: October 3, 2014 WN U-60 Attachment C to Schedule 152, Page 1 PUGET SOUND ENERGY

AGN 165 Parallel Operation with Mains Grid Systems

Effects of Harmonic Distortion I

CHIEF ENGINEER REG III/2 MARINE ELECTROTECHNOLOGY

PI144H - Winding 311 APPROVED DOCUMENT. Technical Data Sheet

PAPER-II (Subjective)

Generation Interconnection Study Data Sheet Synchronous Machines

Connection Impact Assessment Application Form

A Guide to the DC Decay of Fault Current and X/R Ratios

BE Semester- VI (Electrical Engineering) Question Bank (E 605 ELECTRICAL POWER SYSTEM - II) Y - Y transformer : 300 MVA, 33Y / 220Y kv, X = 15 %

(2) New Standard IEEE P (3) Core : (4) Windings :

3. What is hysteresis loss? Also mention a method to minimize the loss. (N-11, N-12)

System Protection and Control Subcommittee

AGN Winding and Bearing Temperature Sensors

In Class Examples (ICE)

AGN 008 Vibration DESCRIPTION. Cummins Generator Technologies manufacture ac generators (alternators) to ensure compliance with BS 5000, Part 3.

Contents. About the Authors. Abbreviations and Symbols

Burdens & Current Transformer Requirements of MiCOM Relays. Application Notes B&CT/EN AP/B11. www. ElectricalPartManuals. com

Company Directive STANDARD TECHNIQUE: SD7F/2. Determination of Short Circuit Duty for Switchgear on the WPD Distribution System

VALLIAMMAI ENGINEERING COLLEGE

Single-Phase Transformation Review

3.1.Introduction. Synchronous Machines

IDAHO PURPA GENERATOR INTERCONNECTION REQUEST (Application Form)

EVALUATION OF REACTANCES AND TIME CONSTANTS OF SYNCHRONOUS GENERATOR

Unit 3 Magnetism...21 Introduction The Natural Magnet Magnetic Polarities Magnetic Compass...21

Power Factor. Power Factor Correction.

Preface...x Chapter 1 Electrical Fundamentals

CHAPTER 5 SYNCHRONOUS GENERATORS

Short-Circuit Current Calculations

CONTENTS. 1. Introduction Generating Stations 9 40

Remotes Case 2&3 Form REINDEER Cases 2&3 -Connection Impact Assessment (CIA) Application

Technical Data Sheet for AvK-Alternators

STEADY STATE REACTANCE

OPERATING, METERING AND EQUIPMENT PROTECTION REQUIREMENTS FOR PARALLEL OPERATION OF LARGE-SIZE GENERATING FACILITIES GREATER THAN 25,000 KILOWATTS

CHAPTER 2 D-Q AXES FLUX MEASUREMENT IN SYNCHRONOUS MACHINES

Transcription:

Application Guidance Notes: Technical Information from Cummins Generator Technologies AGN 034 Alternator Reactance DEFINITION Reactance Periods Inherent to the design of an alternator are certain internal dynamic characteristics that influence the performance of the alternator under momentary and steady state load conditions. These characteristics can be individualised to identify behaviour at specific times following load level changes and are collectively referred to as reactances. Each individual reactance characteristic can be influenced at the point of alternator electro-magnetic design. When the alternator s load conditions are suddenly changed the alternator s resulting performance deliberations begin by considering: The sub-transient reactance for time zero response. As time elapses beyond half a cycle, the transient reactance. And finally, the resulting steady state conditions are identified by a qualification of positive, negative and zero sequence components. Sub-Transient Reactance [X d] - The Kick During the first few milliseconds of a sudden load change, the characteristics attributable to X d will result in a response that promotes a rather aggressive reaction to the load change. In the case of a short circuit fault occurring, high levels of current will be generated, which momentarily reach the equivalent to the full load current multiplied by the reciprocal of the subtransient reactance. If the sub-transient reactance is 12%, the peak values will be some 8 x AGN 034 ISSUE B/1/6

rated current and this is described as being the symmetrical condition, with the asymmetrical - absolute maximum - being twice the symmetrical value. Transient Reactance [X d] - The Follow Through After the first few milliseconds of X d influenced behaviour, the alternator s performance becomes dominated by X d and appropriate time constants. In the case of a short circuit fault condition, the high current levels associated with X d decay at a rate controlled by X d in conjunction with various alternator time constants. Synchronous Reactance [Xd] - The Push Modern alternators, fitted with a control system capable of supporting a sustained steady state short circuit current, will typically sustain 2 to 4 x rated current under a steady state three phase short circuit condition. This means that Xd should not be used to determine the third period fault current level, but engineers can deduce a great deal about an alternator s capability from Xd. Xd is, in fact, established by the ratio of the excitation levels established by SCC and OCC tests. The Effect of Reactances The performance of each alternator under short circuit conditions is presented on the alternator s Short Circuit Decrement Curve and this displays the effects of X d, X d and excitation forced, fault current (rms) levels over time. Zero Sequence Reactance [Xo] When an alternator has a grounded Neutral and a fault occurs, thereby shorting phases together and to-earth, resulting phase fault-currents will become in phase: zero phase angle displacement. Negative Sequence Reactance [X 2] This reactance is used to establish alternator performance under unbalanced load, or fault conditions, thereby generating a contra-rotating to normal operation: negative phase sequence. AN ALTERNATOR AND ITS REACTANCES This section is based on a question about the differences between the overload and fault contribution of the UCI or UCM 224G. The answer below explains how a thermal rating does not change the inherent performance of a particular alternator design. The answer covers the UC 224G alternator but is applicable to any STAMFORD or AvK alternator. AGN 034 ISSUE B/2/6

The UC 224G alternator is a standard STAMFORD product with the G being the core length identifying the amount of 'active material' - in the form of lamination steel and copper wire that will be used to build this G core length of frame type 224 alternator. For additional information; the winding number and design for the alternator decides the number of turns required [to give the voltage required] and therefore, this controls the allowable cross sectional area of the conductor for each winding coil turn, that can be fitted into the space available in the stator winding slot, but [almost] regardless of winding design - and so output voltage level required - the active material will always be fully utilised. This is how we design in order to make a cost effective alternator. A decision now has to be made regarding whether the alternator will be operated at the absolute maximum allowable temperatures for the insulation materials and winding assembly, as would be the case with a standard Industrial UCI [I for Industrial] or operated at a reduced and specified operating temperature in order to be compliant with a marine classifying society and so be offered at a lower kva and therefore, become a UCM [M for Marine]. So these basic considerations and factors are used and so, set the alternator's continuous thermal rating nameplated kva. We must remember; it is still the same amount of active materials inside the alternator, so when this machine is subject to an impact load, an overload, or a fault condition, the alternator will always behave in the same way regardless of its nameplated kva or identified application - UCI or UCM. The stored energy dealing with the suddenly changed load condition comes from within the alternator as a product of the active materials within that alternator and a UC 224G, whether it s a UCI or UCM makes no difference. Things that do make a difference: The operating magnetic flux levels. If the UCI and UCM are both working at the same voltage and frequency, the situation is nullified, as the flux levels will be the same. The expressions used to describe an alternator s 'reaction' to a sudden load step change are the Reactances and Time Constants. Perhaps the most commonly used measure of an alternator s capability to respond to a load step change is the value of the alternator s sub-transient reactance X"d. The value of X"d takes into account the operating magnetic flux level therefore, the operating voltage level and frequency, and then this is referred back to a 'base' rating kva, maybe the nameplated kva rating, but on data sheets it is usually based on the Industrial kva rating. So consider the UC 224G operating at 415V, 50Hz; As an Industrial alternator it has a class H rating of 85kVA and a published value for sub-transient reactance X"d of 11% at a Class H temperature rise continuous (base) rating of 85kVA. The same alternator has an industrial Class F temperature rise rating of 75kVA. X"d at the Class F rating is therefore; equal to [75/85] x 11 = 9.7%. AGN 034 ISSUE B/3/6

The same alternator as a Marine alternator has a Class F temperature rise continuous marine rating of 65kVA and so X"d at this marine rating is equal to [65/85] x 11 = 8.4%. At the Class B marine rating of 60kVA, the X"d is equal to [60/85] x 11 = 7.8%. The above explains how as the same alternator has different values of X"d at different kva outputs. But when the 'time zero' fault current is established using the basic formula of [1 / X"d] x base rated current [Amps], the answer will always be the same value of 'symmetrical' fault current for any of the above industrial or marine ratings. This is correct, because it is the same active materials that will use their energy to generate the fault current. The alternators excitation system If the alternator does not have an excitation system that is able to support a steady state short circuit current, then once the 'stored' energy of the magnetics in conjunction with the amount of active material have been expelled, the alternator will stop giving an output. For example; if the AVR type is an AS or an SX type but is not connected to an auxiliary winding. Such an alternator would give a time zero fault current appropriate to its value of X"d and the decay from this initial high value to zero would be described by calculations involving the alternator s transient reactance X'd and various time constants. Note; other reactances would form part of the calculations required to fully display the fault level capabilities of the alternator. If the Excitation system has an AS AVR with Auxiliary winding or MX type AVR [powered by PMG] or Transformer controlled and therefore, a compounded system, then this constitutes an excitation system that will force a sustained short circuit current to be generated. For an example of the UC 224G Winding 311 operating at 50Hz, refer to the Short Circuit Decrement Curve for the appropriate AVR in the alternator s Technical Data Sheet. CHANGING REACTANCE VALUES We have determined that reactance values are a measure of an Alternator s magnetic stiffness and are used as a mathematical modelling tool to help describe the performance of an alternator under the different stages of behaviour during fault conditions. The reactance is set by the electrical design used for the alternator and is a product of the amount of active [electrical] components used within the alternator. Usually, the main requirement of a design is to be as cost effective as possible; provide the maximum kva for the minimum kg of materials; combined with achieving the lowest possible reactance values to provide the best possible performance against modern electronic power controlled Non Linear Loads. Having achieved the above, it often comes as a surprise when higher reactance values are specified. The reasons, allied to the distribution system, are well understood. AGN 034 ISSUE B/4/6

Unfortunately, it is not possible to INCREASE the reactance of an existing cost effective design. Reducing reactance is achieved by going to a LARGER alternator. Offering an alternator to comply with all the requirements of Marine Authorities requires low reactance in order to satisfy the specified short circuit performance, and transient voltage regulation limits set for during motor starting. REACTANCE VALUES FOR PARALLEL ALTERNATORS The performance of alternators operating in parallel is always an interesting topic. Fundamentally, when considering parallel running Generating Sets, it must always be accepted that, under steady state load conditions, a well set-up parallel running alternator should be set to share the total in proportion to the alternators rating. For example; a 500kVA in parallel with 1000kVA Generating Set should both be running at 50% rated kva to support 750kVA of total load. It is worth pointing out at this stage; Engines share the kw, excitation systems share the kvar, thereby Generating Sets share kva. Under load step changes or fault conditions, this transient load will not be shared equally. Here source impedance up to the PCC has a significant effect. Even two similar sized alternators will not equally share an applied 'step-load'. In fact, the share will typically be more like a 45% and 55% contribution. When considering power system reactance values for parallel running Generating Sets, the approach should be similar to considering resistors in parallel and so a reciprocal factor should be used after the reactances for each alternator have been corrected to the base kva of the total system. For example, consider two Generating Sets: G1: 1000kVA output at 415V, 50Hz with X"d of 14%. G2: 500kVA output at 415V, 50Hz with X"d of 12%. G1 & G2 in parallel: Base level 1500kVA G1 now has X"d of 21% (0.21pu) G2 now has X"d of 36% (0.36pu) The 'effective' X"d for the above pair of alternators based on their combined capability of 1500kVA = (0.21-1 + 0.36-1 ) -1 = 0.133pu = 13.3%. SATURATED AND UNSATURATED REACTANCES The table on the next page provides the multiplying factors for each reactance in order to convert that reactance from its Saturated value to its Unsaturated value: AGN 034 ISSUE B/5/6

Reactance - Saturated value Unsaturated value - multiplying factor S0-S7 P80 AvK Direct Axis Synchronous Reactance Xd 1.2 1.15 1.11111 Direct Axis Transient Reactance X'd 1.15 1.235 1 Direct Axis Sub-Transient Reactance X"d 1.17 1.22 1.11111 Quadrature Axis Reactance Xq 1.03 1.03 1.03 Quadrature Axis Transient Reactance X'q 1.03 1.03 1.03 Quadrature Axis Sub-Transient Reactance X"q 1.2 1 Leakage Reactance XL 1.13 1.13 N/A Negative Sequence Reactance X2 1.2 1.165 1.11111 Zero Sequence Reactance X0 1.17 1.15 1.11111 Application Guidance Notes are for information purposes only. Cummins Generator Technologies reserves the right to change the contents of Application Guidance Notes without notice and shall not be held responsible for any subsequent claims in relation to the content. AGN 034 ISSUE B/6/6