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

A technology of power supply and distribution system and inrush current, which is applied in the field of inrush current suppression device for power supply and distribution circuit of spacecraft power system, which can solve the problems of inductive circuit self-excitation and inability to suppress inrush current, and achieve saturated conduction The resistance is small, the power-on surge current is suppressed, and the effect of ensuring performance

Inactive Publication Date: 2009-06-10
NAT SPACE SCI CENT CAS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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 are further described in detail below with reference to the accompanying drawings.

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

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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 power-on surge current suppressing device, in particular to a power-on surge current suppressing device suitable for a power supply and distribution circuit of a spacecraft power supply system. Background technique [0002] Relays have been used for at least several decades as a common control device, and the contacts of relays have a problem of service life. In industrial applications, a new relay can be replaced with a new relay after the contact is damaged, but in aerospace applications, such as parts on satellites, it is impossible to repair after the sky. Magnetic latching relays are widely used on spacecraft to switch the load on and off. Since the load power input circuit inevitably uses a capacitor, the power supply charges the capacitor at the moment of startup, and the surge current generated by charging will be as high as several amperes to tens of amperes. This The peak surge current is often several to several h...

Claims

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Application Information

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IPC IPC(8): H02H9/02H02H3/08
Inventor 周昌义孙辉先陈晓敏安军社余光华
Owner NAT SPACE SCI CENT CAS
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