Ground fault interrupts for solid state power controllers
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H02H-003/00
H02H-009/08
H02H-009/00
출원번호
UP-0478906
(2006-06-30)
등록번호
US-7609492
(2009-11-10)
발명자
/ 주소
Maier, Josef
출원인 / 주소
Hamilton Sundstrand Corporation
대리인 / 주소
Carlson, Gaskey & Olds
인용정보
피인용 횟수 :
5인용 특허 :
3
초록▼
A solid state power control scheme is provided with a ground fault interrupt function. Essentially, if a neutral wire is associated with the power supply, the current is sensed in that neutral wire. The sensed neutral wire current is subtracted from a summed current on the power supply lines. If tha
A solid state power control scheme is provided with a ground fault interrupt function. Essentially, if a neutral wire is associated with the power supply, the current is sensed in that neutral wire. The sensed neutral wire current is subtracted from a summed current on the power supply lines. If that result is greater than a predetermined limit, then the ground fault function is actuated and the circuit is opened. For power supplies, both those with and without neutral wires, the current is sensed by a shunt resistor on the power supply line.
대표청구항▼
What is claimed is: 1. A solid state power controller having a ground fault interrupt function comprising: a controller for receiving at least one power supply line, and having at least one neutral wire, there being a sensor for sensing current in said at least one power supply line, and a separate
What is claimed is: 1. A solid state power controller having a ground fault interrupt function comprising: a controller for receiving at least one power supply line, and having at least one neutral wire, there being a sensor for sensing current in said at least one power supply line, and a separate sensor for sensing current in said at least one neutral wire, said controller being operable to receive a sensed current in said at least one power supply line, and in said neutral line, and compare the at least two received currents to a predetermined limit, said controller being operable to interrupt power supply to said at least one power supply line should the limit be exceeded; and said at least one power supply line includes at least two power supply lines, with said at least two power supply lines each being provided with separate sensors. 2. The controller as set forth in claim 1, wherein said neutral line is provided with a current sensor at a location remote from said controller. 3. The controller as set forth in claim 1, wherein said at least two power supply lines include three power supply lines at three different phases, with said three power supply lines each being provided with separate sensors. 4. The controller as set forth in claim 3, wherein the sensed currents in each of said three power supplies is summed, and then the neutral current is subtracted from the summed current to determine whether the predetermined limit is exceeded. 5. The controller as set forth in claim 1, wherein a resistor is associated with each said power supply line, and said resistor sensing the current flowing through said at least one power supply line. 6. The controller as set forth in claim 1, wherein said controller comparing a difference in the at least two received currents to the predetermined limit. 7. A plurality of components associated with an aircraft comprising: a plurality of components each being provided with a solid state power controller for supplying power to said plurality of components, at least one of said solid state power controllers including a controller for receiving at least one power supply line, and at least one neutral wire, there being a sensor for sensing current in said at least one power supply line, and a separate sensor for sensing current in said at least one neutral wire, said controller being operable to receive a sensed current in said at least one power supply line, and in said neutral line, and compare the at least two received currents to a predetermined limit, said controller being operable to interrupt power supply to said at least one power supply line should the limit be exceeded; and said at least one power supply line includes at least two power supply lines, with said at least two power supply lines each being provided with separate sensors. 8. The plurality of components as set forth in claim 7, wherein said neutral line is provided with a current sensor at a location remote from said controller. 9. The plurality of components as set forth in claim 7, wherein said at least two power supply lines include three power supply lines at three different phases, with said three power supply lines each being provided with separate sensors. 10. The plurality of components as set forth in claim 9, wherein the sensed currents in each of said three power supplies is summed, and then the neutral current is subtracted from the summed current to determine whether the predetermined limit is exceeded. 11. The plurality of components as set forth in claim 7, wherein a resistor is associated with said at least one power supply line, and said resistor sensing the current flowing through said at least one power supply line. 12. The plurality of components as set forth in claim 7, wherein said controller comparing a difference in the at least two received currents to the predetermined limit.
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이 특허에 인용된 특허 (3)
Elliott Stephen H. ; Miller John A. ; Kosciusko Norman, Aircraft ground power loss of neutral and over-voltage detector.
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