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Digital control apparatus of micro gas turbine

A micro gas turbine and control device technology, which is applied in the direction of fuel control, charging system, engine components, etc. Complicated issues

Active Publication Date: 2013-05-08
HARBIN DONGAN ENGINE GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Mechanical fuel regulators have high requirements on shape and position tolerances and material properties, and the structure is complex
Analog circuit controller has large temperature drift and poor environmental adaptability
At the same time, the two are generally only suitable for micro gas turbines with specific performance. After the control law changes, it is difficult to adjust: the mechanical fuel regulator often needs to redesign the structural size of the internal components, and the processing cycle is long and the cost is high.

Method used

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  • Digital control apparatus of micro gas turbine
  • Digital control apparatus of micro gas turbine
  • Digital control apparatus of micro gas turbine

Examples

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Effect test

Embodiment Construction

[0016] As shown in the figure, the control device includes a micro gas turbine operation panel 1, a micro gas turbine system status element 2, a micro gas turbine measurement component 3, a micro gas turbine switching value execution component 4, a micro gas turbine analog execution component 14, a digital signal processor DSP11, a power supply Module 5, switch input level conversion / isolation module 6, switch output level conversion / isolation module 7, digital / analog conversion module 8, signal conditioning module 9, host computer 10, reset button 17, crystal oscillator 18. The digital signal processor DSP11 is provided with a general input and output module 12 , an analog / digital conversion module 13 , an external interface XINTF15 , a serial communication interface 16 , and an address line and data line 20 .

[0017] The micro gas turbine operation panel 1 and the micro gas turbine system state element 2 are respectively connected to the switching value input level conversio...

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Abstract

The invention relates to a digital control apparatus of a micro gas turbine. A micro gas turbine operation panel and a micro gas turbine system state element are connected with a general input and output module, a micro gas turbine measurement part is connected with a signal modulation module and then is connected with an analog / digital conversion module, and the general input and output module is connected with a micro gas turbine switch value executing part; and an external interface (XINTF) is connected with a micro gas turbine analog quantity executing part, and a digital signal processor (DSP) is connected with an upper computer through a serial communication interface. The digital control apparatus which allows hardware resources to have a certain margin and the interface to be designed in standardization can be used for a plurality of micro gas turbines, can automatically adjust the starting, shutdown, cold running, loading running and the like of the micro gas turbines, satisfies the requirements of the micro gas turbines in economy and service life, can realize the modification of control parameters through software, and can also be used for micro gas turbines having different performances.

Description

technical field [0001] The invention relates to a control device, in particular to a digital control device for a micro gas turbine. Background technique [0002] Most of the existing micro gas turbine controllers use a mechanical fuel regulator or an analog circuit controller to adjust the fuel and then control the micro gas turbine speed and exhaust temperature after the turbine. Mechanical fuel regulators have high requirements on shape and position tolerances and material properties, and their structures are complex. The analog circuit controller has large temperature drift and poor environmental adaptability. At the same time, the two are generally only suitable for micro gas turbines with specific performance. After the control law changes, it is difficult to adjust: the mechanical fuel regulator often needs to redesign the structural size of the internal components, and the processing cycle is long and the cost is high. The analog circuit controller needs to replace...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C9/48
Inventor 何民耿加民仝云峰刘丛红张宏杰张琳琳潘振宇刘雯雯栾兰
Owner HARBIN DONGAN ENGINE GRP
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