Opening surge current control device suitable for spacecraft power supply and distribution system

A power supply and distribution system and inrush current technology, which is applied in the field of power supply and distribution circuit start-up surge current suppression devices for spacecraft power systems, can solve problems such as inability to suppress inrush current and self-excitation of inductance circuits, and achieve suppression of power-on surges. Inrush current, small saturated on-resistance, and small size

Inactive Publication Date: 2010-12-29
CENT FOR SPACE SCI & APPLIED RES
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0004] The traditional anti-sparking circuit has the device and method of using series resistors and capacitors, and the method of series inductors in the loop, etc., but they cannot completely suppress the surge current to a reasonable range, and the excessive series inductance will also lead to self-excitation of the circuit occur

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  • Opening surge current control device suitable for spacecraft power supply and distribution system
  • Opening surge current control device suitable for spacecraft power supply and distribution system
  • Opening surge current control device suitable for spacecraft power supply and distribution system

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Embodiment Construction

[0024] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions according to the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0025] reference image 3 , Make a start-up surge current suppression device suitable for the spacecraft power supply and distribution system of the present invention. The start-up surge current suppression device is a DC surge current suppression circuit connected between the relay and the electrical equipment and the power return line . The experimental device of the invention is easily realized by using civilian components. The first resistor R1 and the second resistor R2 are respectively commercially available resistors with a resistance value of 1MΩ / 0.25W; the third resistor R3 and the fourth resistor R4 are respectively used The resistance value purchased on the market is a resistance of 470KΩ / 0.25W; the fifth resistan...

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Abstract

The invention relates to a startup surge current suppression device applicable to a spacecraft power distribution system, which is a surge current suppression circuit connected between a relay and electric equipment. The startup surge current suppression device comprises a first fuse, a second fuse, a time-delay fusing resistor, a divider circuit, a first capacitor, a second capacitor and an N-channel field-effect transistor, wherein the first fuse and the second fuse are connected in series in a loop; the first fuse and the time-delay fusing resistor are connected in series, and then connected in parallel with the second fuse; the divider circuit is connected in series in the loop; the first capacitor and the second capacitor are used for adjusting a startup time-delay parameter; the first capacitor and the second capacitor are connected in series, and then connected in parallel with a third resistor; and the N-channel field-effect transistor is connected in series among the fuses, the electric equipment and a power supply loop. The startup surge current suppression device is applicable to an on-off circuit of the spacecraft power distribution system, can effectively reduce startup surge current caused by capacity charge in a starting process, and prolong the service life of contacts of the relay.

Description

Technical field [0001] The invention relates to a start-up surge current suppression device, in particular to a start-up surge current suppression device suitable for power supply and distribution circuits of a spacecraft power supply system. Background technique [0002] As a commonly used control device, the relay has been used for at least several decades, and the contacts of the relay have a service life problem. In industrial applications, a new relay can be replaced after the contacts are damaged, but in aerospace applications, such as satellite parts, it is impossible to repair after going up to the sky. Magnetic latching relays are widely used on spacecraft to switch loads. Because the load power input circuit inevitably uses capacitors, the power supply charges the capacitors at the moment of power-on, and the surge current generated by charging will be as high as several amperes to tens of amperes. The peak surge current is often several to several hundred times the no...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02H9/02H02H3/08
Inventor 周昌义孙辉先陈晓敏安军社余光华
Owner CENT FOR SPACE SCI & APPLIED RES
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