Electricity: magnetically operated switches – magnets – and electr – Electromagnetically actuated switches – Automatic circuit-interrupting devices
Reexamination Certificate
2001-04-30
2003-04-01
Donovan, Lincoln (Department: 2836)
Electricity: magnetically operated switches, magnets, and electr
Electromagnetically actuated switches
Automatic circuit-interrupting devices
C200S317000
Reexamination Certificate
active
06542056
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to electrical switching apparatus and, more particularly, to circuit breakers, such as, for example, arc fault circuit breakers.
2. Background Information
Circuit breakers are used to protect electrical circuitry from damage due to an overcurrent condition, such as an overload condition or a relatively high level short circuit or fault condition. In small circuit breakers, commonly referred to as miniature circuit breakers, used for residential and light commercial applications, such protection is typically provided by a thermal-magnetic trip device. This trip device includes a bimetal, which heats and bends in response to a persistent overcurrent condition. The bimetal, in turn, unlatches a spring powered operating mechanism, which opens the separable contacts of the circuit breaker to interrupt current flow in the protected power system.
Subminiature circuit breakers are used, for example, in aircraft electrical systems where they not only provide overcurrent protection but also serve as switches for turning equipment on and off. As such, they are subjected to heavy use and, therefore, must be capable of performing reliably over many operating cycles. They also must be small to accommodate the high-density layout of circuit breaker panels, which make circuit breakers for numerous circuits accessible to a user. Aircraft electrical systems usually consist of hundreds of circuit breakers, each of which is used for a circuit protection function as well as a circuit disconnection function through a push-pull handle.
The circuit breaker push-pull handle is moved from in-to-out in order to open the load circuit. This action may be either manual or, else, automatic in the event of an overload or fault condition. If the push-pull handle is moved from out-to-in, then the load circuit is re-energized. If the load circuit had been automatically de-energized, then the out-to-in operation of the push-pull handle corresponds to a circuit breaker reset action.
Typically, subminiature circuit breakers have only provided protection against persistent overcurrents implemented by a latch triggered by a bimetal responsive to I
2
R heating resulting from the overcurrent. There is a growing interest in providing additional protection, and most importantly arc fault protection. Arc faults are typically high impedance faults and can be intermittent. Nevertheless, such arc faults can result in a fire.
Although many circuit breakers also employ ground fault protection, in aircraft applications, the aircraft frame is ground, and there is no neutral conductor. Some aircraft systems have also provided ground fault protection, but through the use of additional devices, namely current transformers which in some cases are remotely located from the protective relay.
During sporadic arcing fault conditions, the overload capability of the circuit breaker will not function since the root-mean-squared (RMS) value of the fault current is too small to activate the automatic trip circuit. The addition of electronic arc fault sensing to a circuit breaker can add one of the elements required for sputtering arc fault protection—ideally, the output of an electronic arc fault sensing circuit directly trips and, thus, opens the circuit breaker. It is still desirable, however, to provide separate indications in order to distinguish an arc fault trip from an overcurrent-induced trip.
Finally, there is an interest in providing an instantaneous trip in response to very high overcurrents such as would be drawn by a short circuit.
The challenge is to provide alternative protection and separate indications in a very small package, which will operate reliably with heavy use over a prolonged period. A device which meets all the above criteria and can be automatically assembled is desirable.
In aircraft applications, two practical considerations make automatic operation difficult to achieve and, possibly, undesirable. First, the design of a conventional aircraft circuit breaker makes it difficult to add an externally initiated tripping circuit thereto. Second, certain circuits on an aircraft are so critical that manual intervention by a crewmember may be desirable before a circuit is de-energized.
U.S. Pat. No. 5,546,266 discloses a circuit interrupter including ground fault and arcing fault trip circuits, and indicators, such as LEDs, to produce an indication of the cause of the trip.
U.S. Pat. No. 5,831,500 discloses a circuit breaker employing a trip flag, a status insert and a status flag that are viewable through a lens based upon the trip, open, and closed positions, respectively, of the circuit breaker.
U.S. Pat. No. 5,847,913 discloses a circuit breaker employing ground fault interruption and arc fault detecting circuitry. Conduits are provided in the circuit breaker housing for conveying light or reflecting light between light sources, plungers or bimetal disks and an opening of the housing.
U.S. Pat. No. 6,084,756 discloses a tester for an arc fault circuit breaker in which an indicator is extinguished when a circuit breaker responds to an arc fault condition.
There is room for improvement in circuit breakers.
SUMMARY OF THE INVENTION
The present invention is directed to a circuit breaker including an arc fault annunciator. In the event that an arc fault is detected, the annunciator provides a visual indication that an arc fault exists. The visual indication allows identification of the associated circuit breaker that is protecting the arc faulted circuit. In aircraft applications, for example, the aircraft crew can make a decision as to whether or not the circuit should be re-energized or left de-energized. The visual indication may serve as a reminder to perform subsequent aircraft maintenance.
As one aspect of the invention, an aircraft circuit breaker comprises: a housing; separable contacts mounted in the housing; a latchable operating mechanism including a latch member which when unlatched opens the separable contacts; an overcurrent assembly responsive to selected conditions of current flowing through the separable contacts for unlatching the latch member to trip the separable contacts open; a movable and illuminable arc fault indicator having a first portion and a second portion internal to the housing; an arc fault actuator which when energized moves the second portion of the movable and illuminable arc fault indicator; and an arc fault current assembly responsive to selected arc fault conditions of current flowing through the separable contacts for energizing the arc fault actuator to move the second portion of the movable and illuminable arc fault indicator internal to the housing and the first portion of the movable and illuminable arc fault indicator external to the housing, the arc fault current assembly including a light for illuminating the first portion of the movable and illuminable arc fault indicator.
Preferably, the movable and illuminable arc fault indicator further has a spring, which engages the second portion of the movable and illuminable arc fault indicator, and the arc fault actuator includes a latch, which when moved, allows the spring to move the second portion. The first portion of the movable and illuminable arc fault indicator protrudes through an opening of the housing, and the latch, when moved, allows the spring to move the second portion of the movable and illuminable arc fault indicator and, thereby, move the first portion external to the housing.
Preferably, the latchable operating mechanism includes an operating handle, which protrudes through the opening of the housing. The first portion of the movable and illuminable arc fault indicator includes a ring surrounding the operating handle. The latch, when moved, allows the spring to move the ring away from the opening of the housing.
The second portion of the movable and illuminable arc fault indicator may include a light pipe having an end, which is normally proximate the light, with the light pipe being normally illuminated by the light; and the latch, wh
Hall Thomas Michael
Nerstrom Peter Lee
Rollmann Paul Jason
Schmalz Steven Christopher
Wellner Edward Louis
Donovan Lincoln
Eaton Corporation
Union Marvin L.
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