GB2486493A - Testing operation of a switching device by using a pulldown device to short a load - Google Patents

Testing operation of a switching device by using a pulldown device to short a load Download PDF

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Publication number
GB2486493A
GB2486493A GB1021453.4A GB201021453A GB2486493A GB 2486493 A GB2486493 A GB 2486493A GB 201021453 A GB201021453 A GB 201021453A GB 2486493 A GB2486493 A GB 2486493A
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GB
United Kingdom
Prior art keywords
switching
load
switching circuit
current
activated
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB1021453.4A
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GB201021453D0 (en
GB2486493B (en
Inventor
Peter Michael Tyler
John Oliver Collins
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GE Aviation Systems Ltd
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GE Aviation Systems Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by GE Aviation Systems Ltd filed Critical GE Aviation Systems Ltd
Priority to GB1021453.4A priority Critical patent/GB2486493B/en
Publication of GB201021453D0 publication Critical patent/GB201021453D0/en
Priority to FR1161734A priority patent/FR2969427B1/en
Priority to CA2762475A priority patent/CA2762475C/en
Priority to BRPI1105402-6A priority patent/BRPI1105402A2/en
Priority to JP2011275229A priority patent/JP6018377B2/en
Priority to DE102011056541.8A priority patent/DE102011056541B4/en
Priority to CN201110463075.XA priority patent/CN102608526B/en
Publication of GB2486493A publication Critical patent/GB2486493A/en
Application granted granted Critical
Publication of GB2486493B publication Critical patent/GB2486493B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/327Testing of circuit interrupters, switches or circuit-breakers
    • G01R31/3277Testing of circuit interrupters, switches or circuit-breakers of low voltage devices, e.g. domestic or industrial devices, such as motor protections, relays, rotation switches
    • G01R31/3278Testing of circuit interrupters, switches or circuit-breakers of low voltage devices, e.g. domestic or industrial devices, such as motor protections, relays, rotation switches of relays, solenoids or reed switches
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/327Testing of circuit interrupters, switches or circuit-breakers
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/26Testing of individual semiconductor devices
    • G01R31/2607Circuits therefor
    • G01R31/2608Circuits therefor for testing bipolar transistors
    • G01R31/2617Circuits therefor for testing bipolar transistors for measuring switching properties thereof
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/005Testing of electric installations on transport means
    • G01R31/008Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Electronic Switches (AREA)
  • Power Conversion In General (AREA)
  • Testing Of Individual Semiconductor Devices (AREA)
  • Testing Of Short-Circuits, Discontinuities, Leakage, Or Incorrect Line Connections (AREA)

Abstract

A switching circuit 1 connecting a load 15 to a voltage source 2 comprises one or more switching devices 6, 7, for switching on and off power to the load, a pulldown device 4 for shorting out the load thereby isolating it from the voltage source, and a controller 3 operable while the source is isolated from the load to activate at least one of the switching devices at a time, wherein a current passes through the or each activated switching device and is measurable to test whether the or each activated switching device is operating correctly. The switching devices are thus tested in situ. The switching devices may form part of a circuit in an aircraft, where the source 2 would be an engine generator.

Description

SWITCHING CIRCUITS AND METHODS OF TESTING
The present invention relates to switching circuits and methods of testing thereof.
Often, switching circuits include several switching devices connected in parallel with one another whereby the current capacity of the switching circuit is the sum of the capacities of each switching device. This is particularly useful for applications in which the power required by the load exceeds the capacity of a single switching device. One example of such switching circuits is found in aircraft power distribution systems, wherein for example 8 solid-state switching devices may be provided in parallel. Generally, the switching devices can fail open or closed. Each switching device has a driver which can be the cause of the failure, if one or more of the switching devices fails open the others can act as backup switches, but potentially may be subjected to current overload, if one or more of the switching devices fails closed, it would not be possible to switch off the switching circuit and it would be readily apparent that such a failure had occurred. if failed open, the failure may be undetectable. Solid-state switching devices are tested thoroughly at the manufacturing stage, but it is desirable to be able to test them in service to ensure that they remain fully functional. This is also known as a built-in-test (BIT).
The present invention provides a switching circuit for connection to a load and to a voltage source, comprising one or more switching devices for switching on and off power to the load, a pulldown device for shorting out the load thereby isolating it from the voltage source and a controller operable while the load is shorted to activate at least one of the switching devices at a time, wherein a current passes through the or each activated switching device and is measurable to test whether the or each activated switching device is operating correctly.
Advantageously, the pulldown device allows the switching devices to be tested without the load, so that the test can be carried out before or after installation of the switching circuit.
Further, the present invention provides a method of testing a switching circuit that connects a load to a voltage source, the switching circuit including one or more switching devices, the method comprising shorting out the load by activating a puildown device, activating one or more of the switching devices, measuring the current through the or each activated switching device and determining from the measured current signal whether the activated switching devices is/are operating correctly.
Embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings, in which: Figure 1 shows schematically a circuit including a switching circuit exemplifying the present invention; and Figure 2 is a graph of current against time during a test procedure carried out on the circuit of Figure 1.
Figure 1 illustrates an example of a circuit comprising a switching circuit 1 connected to a voltage source 2. The circuit has an output 5 which is connected to a load 15. The circuit may, for example, be provided on an aircraft such that the voltage source 2 may be provided by an engine generator and the load 15 may be a component on the aircraft, such as to actuate a landing gear flap or the under carriage or a component within the aircraft such as instrumentation or in-flight entertainment. The switching circuit 1 may comprise an individual switching device 6, or a plurality of switching devices 6, 7, ..., n. The switching devices are connected in parallel. The switching devices may each comprise any suitable solid-state switching device such as a field effect transistor. The switching circuit 1 is used to connect the power source 2 to the load 15. The voltage source 2 and its associated cabling or wiring will have an inherent inductance 11. Likewise, the load and its associated cabling and wiring will have an inherent inductance 14.
The switching circuit further includes a controller 3 which is connected to each of the switching devices 6, 7, ..., n via respective control lines 8,9,10. The controller 3 is also connected to a pulidown device 4 via a pulldown control line 12. The pulldown device 4 is further connected to the load output 5 and the power return line 13. When the pulldown 4 is closed it shuts off the load from the switching circuit, and diverts current through the pulidown 4. The puildown device, also referred to as a puildown circuit or simply a puildown, can include any appropriate switch, including electronic, electromechanical and mechanical switches.
The switching circuit I may comprise a solid-state power controller (SSPC), which may comprise one or a plurality of connected semiconductor devices, If it comprises a plurality of parallel connected semiconductor devices, each device may be switched on and off sequentially so that each of the plurality of devices may be tested individually. Other test sequences can be envisaged, such as activating more than one switching device at once. Individual activation of the switching devices allows fault isolation to an individual switch. The testing sequence can be carried out at any convenient time, such as in between flights. The testing sequence could also be carried out in-flight during times when the load 15 is not required.
Each of the switching devices 6, 7, ..., n includes a respective current limiter 61, 71,..., ni. The current limiters restrict the current passing through the switching devices to on the order of five to ten times the normal maximum operating current to avoid damage to the switching devices. Alternatively, a single current limiter for all of the switching devices could be provided. In a further alternative, a hard current trip could be provided to turn off the switching devices when the trip limit is exceeded.
The pulldown circuit is activated whenever any of the switching devices are activated for the BIT testing routine. Each switching device and its drive circuitry may be fully tested by using the controller 3 to activate one device at a time while simultaneously checking that the current flowing through it and through the pulldown device is within the correct limits. The current measuring circuitry is not shown in Figure 1. In one particular embodiment, the minimum time for which each switching device is activated is chosen to be at feast the time required for the current to become relatively constant to allow consistent measurement of this current to the accuracy required by the BIT system. The time for which each switching device is activated is generally dependent on the maximum total inductance ii in the input power source cable.
However, the system can be operated on shorter timescales if desired.
The pulldown device is designed so that when it sinks the current from a single main switching device during the BIT test, the voltage developed at the output 5 to the load is negligible compared to the normal output voltage when the system is on. This ensures that the load is not subjected to significant voltage when the system is supposed to be off. This is achieved by using a pulidown device 4 that has a lower impedance than each switching device, preferably much lower. In practice, when the current limiters 61, 71, ..., ni are in operation, the switching devices 6, 7, ..., n have a higher effective impedance than the pulldown device 1. During normal system operation, the controller 3 which activates the switching devices 6, 7, ..., n would generally be expected to turn all of the switching devices on and off simultaneously.
Embodiments of the invention apply not only to DC systems but also AC systems. In this case the voltage source 2 would be an alternating voltage. The switching devices would be AC switches (optionally with AC current limiters) and the pulldown circuit would be capable of sinking AC currents. In a DC embodiment, the pulldown device comprises a field effect transistor (PET) or a bipolar transistor, or an insulated gate bipolar transistor for example. Other types of switching device can be used. In an AC embodiment, the pulldown device may comprise a triac or a solid state relay for
example.
Figure 2 illustrates the output current through a switching device when a test procedure is performed. Only one peak is shown, but in an exemplary embodiment eight switching devices are provided so the test would result in a total input current from the voltage source 2 which shows 8 sequential pulses like the single one shown in Fig. 2. The correct operation of each switching device 6, 7, ,.., n may be determined by checking the amplitude of each individual current pulse is within the correct limits.
The test procedure begins by shorting out the load by activating the pulldown device 4. The pulldown device will generally remain on for the duration of the BIT test. The first switching device 6 is closed at about 250 p.s in the example shown, and the current through the switching device 6 quickly rises to that provided by the source 2, in this example approximately 100 Amps. The first switching device 6 is then opened and a short time later, the second switching device 7 is closed and the current through the second switching device 7 is measured. This procedure is repeated in sequence until all of the switching devices have been tested. Differences in the current profiles to the ones shown in Figure 2 may indicate a fault with the corresponding switching device.
Advantageously, embodiments of the invention allow individual assessment of the operation of the switching devices. A simple BIT test which just checks the overall solid state power controller operation would not normally be able to detect a faulty device which was stuck in the open circuit state. A technical advantage of this invention is that not only does it detect single device failures but also can check the current limiting performance of each device individually. The invention can therefore provide complete BIT coverage during in-service operation.
In an alternative embodiment the switching devices do not have current limit control.
In this case the inductance of the power source 2 and cable inductance 11 can be relied on in combination with a fast current trip circuit to prevent the current rising to dangerous levels during the test pulse. In other words, the controller 3 in this embodiment would operate to activate the sequence of opening and closing the switching devices quickly enough to avoid current overload.

Claims (17)

  1. CLAIMS: 1. A switching circuit for connection to a load and to a voltage source, comprising one or more switching devices for switching on and off power to the load, a pulldown device for shorting out the load thereby isolating it from the voltage source and a controller operable while the load is shorted to activate at least one of the switching devices at a time, wherein a current passes through the or each activated switching device and is measurable to test whether the or each activated switching device is operating correctly.
  2. 2. A switching circuit according to claim 1, wherein the pulldown device includes a switch disposed in parallel with the load, and closure of the switch shorts out the load.
  3. 3. A switching circuit according to claim 2, wherein the puildown device includes an electronic, electromechanical andlor mechanical switch, including any one or more of a field effect transistor, a bipolar transistor, an insulated gate bipolar transistor, a triac, and a solid state relay.
  4. 4. A switching circuit according to any of the preceding claims, wherein the or each switching device is activated individually.
  5. 5. A switching circuit according to any of the preceding claims, further comprising a current limiter for restricting the current through the or each switching device.
  6. 6. A switching circuit according to claim 5, wherein the or each switching device has a current limiter disposed therein.
  7. 7. A switching circuit according to any of claims 1 to 4, wherein system inductance is used to restrict the current through the or each switching device.
  8. 8. A switching circuit according to any of the preceding claims, wherein the impedance of the puildown device is less than the impedance of the or each switching device.
  9. 9. A switching circuit according to any of the preceding claims, wherein an output voltage of the switching circuit under test conditions is negligible compared to the output voltage in normal operating conditions.
  10. 10. A switching circuit according to any of the preceding claims, wherein the circuit is connectable to an AC or a DC voltage source.
  11. 11. A switching circuit according to any of the preceding claims, wherein the or each switching device comprises a solid state switching device.
  12. 12. A method of testing a switching circuit that connects a load to a voltage source, the switching circuit including one or more switching devices, the method comprising shorting out the load by activating a pulidown device, activating one or more of the switching devices, measuring the current through the or each switching device that is activated and determining from the measured current signal whether the activated switching devices is/are operating correctly.
  13. 13. A method according to claim 12, wherein the switching devices are activated sequentially one after another.
  14. 14. A method according to claim 12, wherein the one or more switching devices are activated for a time sufficient for the current flowing therethrough to become substantially constant.
  15. 15. A method according to any of claims 12 to 14, further comprising restricting the current that passes through each switching device.
  16. 16. A switching circuit substantially as herein described with reference to the accompanying drawings.
  17. 17. A method of testing a switching circuit substantially as herein described with reference to the accompanying drawings.
GB1021453.4A 2010-12-17 2010-12-17 Switching circuits and methods of testing Active GB2486493B (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB1021453.4A GB2486493B (en) 2010-12-17 2010-12-17 Switching circuits and methods of testing
FR1161734A FR2969427B1 (en) 2010-12-17 2011-12-15 SWITCHING CIRCUIT AND TEST METHOD
CA2762475A CA2762475C (en) 2010-12-17 2011-12-15 Switching circuits and methods of testing
BRPI1105402-6A BRPI1105402A2 (en) 2010-12-17 2011-12-16 SWITCHING CIRCUIT AND TESTING METHOD OF A SWITCHING CIRCUIT
JP2011275229A JP6018377B2 (en) 2010-12-17 2011-12-16 Switching circuit and test method
DE102011056541.8A DE102011056541B4 (en) 2010-12-17 2011-12-16 circuits and test procedures
CN201110463075.XA CN102608526B (en) 2010-12-17 2011-12-16 The method of on-off circuit and test

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1021453.4A GB2486493B (en) 2010-12-17 2010-12-17 Switching circuits and methods of testing

Publications (3)

Publication Number Publication Date
GB201021453D0 GB201021453D0 (en) 2011-02-02
GB2486493A true GB2486493A (en) 2012-06-20
GB2486493B GB2486493B (en) 2016-06-15

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GB1021453.4A Active GB2486493B (en) 2010-12-17 2010-12-17 Switching circuits and methods of testing

Country Status (7)

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JP (1) JP6018377B2 (en)
CN (1) CN102608526B (en)
BR (1) BRPI1105402A2 (en)
CA (1) CA2762475C (en)
DE (1) DE102011056541B4 (en)
FR (1) FR2969427B1 (en)
GB (1) GB2486493B (en)

Cited By (4)

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EP2696502A3 (en) * 2012-08-10 2017-12-13 GS Yuasa International Ltd. Switch failure diagnosis device and electric storage apparatus
EP3384513A1 (en) * 2015-12-18 2018-10-10 Pepperl + Fuchs GmbH Methods and apparatuses for monitoring the functionality of redundantly interconnected contacts
EP3629039A1 (en) * 2018-09-26 2020-04-01 Aptiv Technologies Limited Solid state power switch device
US10749334B2 (en) 2018-07-12 2020-08-18 Ovh Method and power distribution unit for preventing disjunctions

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CN103310853B (en) * 2013-05-24 2016-02-24 南京航空航天大学 A kind of power switch circuit with built-in self-test
US10270241B2 (en) * 2016-05-16 2019-04-23 Varian Semiconductor Equipment Associates, Inc. Fault current limiter having fault checking system for power electronics and bypass circuit
US10340908B2 (en) * 2016-07-25 2019-07-02 Continental Automotive Systems, Inc. Half-bridge driver fault diagnostic system and method
GB2563069B (en) 2017-06-02 2020-07-01 Ge Aviat Systems Ltd Apparatus to detect a fault in a wire
CN108051737B (en) * 2017-12-04 2019-12-06 华北电力大学 switch device screening system and method
CN109828169A (en) * 2019-02-01 2019-05-31 中国矿业大学(北京) Electric fireproof current-limiting protector electric performance test method, apparatus and system
CN110187269B (en) * 2019-06-21 2024-03-29 江苏伊施德创新科技有限公司 Method and device for reducing energy consumption in relay full-load test
EP3767316B1 (en) * 2019-07-19 2022-03-30 Yazaki Corporation Switch failure detection device
CN112255537B (en) * 2020-10-13 2022-03-25 南京大学 Gallium nitride triode switch test circuit and test method

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US6304189B1 (en) * 1997-08-22 2001-10-16 Robert Bosch Gmbh Method for detecting malfunctions of a first relay
US20040160131A1 (en) * 2001-05-22 2004-08-19 Richard Veil Safety switching module and method for testing the switching-off ability of a switching element in a safety switching module
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Cited By (10)

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Publication number Priority date Publication date Assignee Title
EP2696502A3 (en) * 2012-08-10 2017-12-13 GS Yuasa International Ltd. Switch failure diagnosis device and electric storage apparatus
EP3687067A1 (en) * 2012-08-10 2020-07-29 GS Yuasa International Ltd. Switch failure diagnosis device and electric storage apparatus
EP3384513A1 (en) * 2015-12-18 2018-10-10 Pepperl + Fuchs GmbH Methods and apparatuses for monitoring the functionality of redundantly interconnected contacts
US10886086B2 (en) 2015-12-18 2021-01-05 Pepperl+Fuchs Se Methods and apparatuses for monitoring the functionality of redundantly interconnected contacts
EP3384513B1 (en) * 2015-12-18 2024-02-07 Pepperl+Fuchs SE Methods and apparatuses for monitoring the functionality of redundantly interconnected contacts
US10749334B2 (en) 2018-07-12 2020-08-18 Ovh Method and power distribution unit for preventing disjunctions
US10886728B2 (en) 2018-07-12 2021-01-05 Ovh Circuit implementing an AC smart fuse for a power distribution unit
US11233388B2 (en) 2018-07-12 2022-01-25 Ovh Method and power distribution unit for limiting a total delivered power
EP3629039A1 (en) * 2018-09-26 2020-04-01 Aptiv Technologies Limited Solid state power switch device
US11290101B2 (en) 2018-09-26 2022-03-29 Aptiv Technologies Limited Solid state power switch device

Also Published As

Publication number Publication date
BRPI1105402A2 (en) 2019-03-26
CN102608526A (en) 2012-07-25
GB201021453D0 (en) 2011-02-02
JP6018377B2 (en) 2016-11-02
DE102011056541B4 (en) 2022-07-21
FR2969427B1 (en) 2020-02-28
CN102608526B (en) 2016-05-11
JP2012147655A (en) 2012-08-02
CA2762475A1 (en) 2012-06-17
DE102011056541A1 (en) 2012-06-21
GB2486493B (en) 2016-06-15
CA2762475C (en) 2019-01-08
FR2969427A1 (en) 2012-06-22

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