The present disclosure relates generally to generator modules for aircraft, and more particularly to fault detection current transformers for use in the same.
Generator modules, and particularly aircraft generator modules, are subject to internal and external short circuits (faults) that affect the operation of the generator module. In order to detect short circuits internal or external to the generator module, an internal current transformer is used to determine an internal current of the generator module. An external current transformer is simultaneously used to determine a current exiting the generator module. When the current measurements of the external current transformer and the internal current transformer differ by more than a predefined threshold, a controller determines that a fault exists internal or external to the generator module, and appropriate action is taken by the controller. The internal current transformer is physically located on the neutral side of the generator phase windings to include the generator windings in the protected zone.
Current transformers have a saturation point at which the secondary output of the current transformer no longer increases linearly despite a continued increase in the primary current passing through the current transformer. When saturation of the internal current transformer occurs, the difference between the internal current transformer measurement and the external current transformer measurement during a short circuit can exceed the threshold, resulting in the controller failing to detect the fault when a fault exists, or, falsely sensing a fault when no fault exists.
Disclosed is a current transformer having a ring shaped magnetic core defining an axis, a plurality of windings wound around the core, a ring shaped housing encompassing the core and the windings, and a pair of output leads connected to the windings. The ring shaped magnetic core has a rectangular cross sectional area defining a range of axial heights and a range of radial widths operable to provide a suitable current transformer current rating.
Also disclosed is a generator module for an aircraft having a generator, an internal current transformer operable to detect an internal current of the generator module, and operable to output the detected internal current to a controller. The current transformer has a ring shaped magnetic core defining an axis, a plurality of windings wound around the core, a ring shaped housing encompassing the core and the windings, and a pair of output leads connected to the windings. The ring shaped magnetic core has a rectangular cross sectional area defining a range of axial heights and a range of radial widths operable to provide a suitable current transformer current rating.
Also disclosed is a method of assembling a generator module having the steps of: determining a maximum short circuit current through a generator module, installing an internal current transformer in the generator module, wherein the current transformer has a core cross sectional area sufficient to accommodate a primary current rating of the internal current transformer in excess of the maximum short circuit current through the generator module, and connecting the internal current transformer to a controller, wherein the controller is further connected to a corresponding external current transformer, such that the controller can compare an internal current of the generator module and an output current of the generator module and determine when a fault is present in the system.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
Connected to the generator module 10, and measuring an output current of the generator module 10, is an external current transformer 30. Both the internal current transformer 20 and the external current transformer 30 are connected to a controller 40. The controller 40 reads the detected currents from each of the internal current transformer 20 and the external current transformer 30, and identifies an internal or external fault when the detected currents vary by an amount greater than a predetermined threshold. Both the internal current transformer 20 and the external current transformer 30 have an identical primary to secondary current ratio. By appropriate sectioning of the secondary turns in the windings of each of the current transformers 20, 30, a designer can ensure that the current transformers 20, 30 have the same ratio of input primary current to output secondary current, and thereby ensure that an accurate comparison is performed.
Current transformers, such as internal current transformer 20, have a saturation threshold. The saturation threshold of the current transformer depends on the amount of core material in the current transformer core, as well as other factors. When primary current passing through the current transformer exceeds the saturation threshold, the secondary output of the current transformer (the current measurement) peaks and stops increasing in a linear fashion. This affect causes a saturated current transformer to be unable to give an accurate current reading above the current saturation threshold, and necessarily impacts the fault detection of the controller 40. One of skill in the art, in light of this disclosure, would understand that increasing the amount of the core material, with consideration for the differences in properties between the cores of the internal and external current transformers or the number of turns in the winding, increases the current saturation threshold of the current transformer without impacting the ratio of input current to output current.
In the particular example illustrated in
In order to fit properly within the packaging of a generator module 10, the current transformer 100 has a maximum axial height 140 and a maximum outer radius 150 that the ring shaped body 106 should not exceed. In a specific example, the ring shaped body 106 has an outer radius 150 of 0.475 inches and an inner radius 178 of 0.115 inches, resulting in a radial width 174 of 0.360 inches. In the specific example, the housing 130 has a cross sectional area of 0.187 square inches.
When determining the type and construction of the improved current transformer 100, it is recognized that varying magnetic core materials and varying numbers of secondary turns within the windings will affect an input current to output current ratio. As such, it is desirable to match the number of winding 120 turns in the improved current transformer 100 to the composition of the core and the number of winding turns in the external current transformer 30 (illustrated in
Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.