Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Astronautic programmable thermocouple temperature transmitter

A technology for temperature transmitters and thermocouples, applied to thermometers, thermometers, and electrical devices that use directly heat-sensitive electric/magnetic components, etc., can solve problems such as low intelligence, cumbersome debugging process, and inconsistent hardware , to achieve the effect of simple debugging process, suitable for mass production, and high degree of intelligence

Active Publication Date: 2014-04-02
BEIJING RES INST OF TELEMETRY +1
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] 1) The measuring range of the existing products is adjusted by the resistance value of the internal resistance, the hardware of the same series of products is inconsistent, the production efficiency is low, and it is not suitable for mass production;
[0005] 2) Existing products require hardware debugging due to differences in components, and the debugging process is cumbersome;
[0006] 3) After the assembly of existing products is completed, the measuring range cannot be changed, and the degree of intelligence is low

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Astronautic programmable thermocouple temperature transmitter
  • Astronautic programmable thermocouple temperature transmitter
  • Astronautic programmable thermocouple temperature transmitter

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0036] Below in conjunction with accompanying drawing and specific embodiment, the present invention is described in further detail:

[0037] like figure 1Shown is the circuit working schematic diagram of the thermocouple temperature transmitter of the present invention. The thermocouple temperature transmitter product of the present invention is powered by a single power supply with a wide voltage of 6-15V, the input is a thermocouple signal, and the output voltage range is 0-5V. As can be seen from the figure, the thermocouple temperature transmitter circuit is composed of a power supply circuit, a programmable amplifier circuit, a programmable cold junction compensation circuit, an operational amplifier circuit, and an output protection circuit. The power supply circuit supplies power to the programmable amplifier circuit, the programmable cold junction compensation circuit, and the operational amplifier circuit to realize the functions of power supply filtering, reverse co...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention relates to an astronautic programmable thermocouple temperature transmitter. A circuit part is composed of a power circuit, a programmable amplifying circuit, a programmable cold junction compensation circuit, an operation amplifying circuit and an output protecting circuit, wherein the functions of power filtering, reverse connection protection, transient impact protection, and the like, are achieved by the power circuit; a thermocouple signal is adjusted to be in a suitable voltage range by the programmable amplifying circuit; the programmable cold junction compensation circuit is used for sensing the temperature of a cold junction of the thermocouple, converting a temperature signal of the cold junction into a voltage signal and compensating the temperature of the cold junction of the thermocouple; output signals of the programmable amplifying circuit and the programmable cold junction compensation circuit are operated and amplified to be 0-5V by the operation amplifying circuit; and the output protecting circuit is used for limiting an output voltage within a scope of -0.5V to +6.5V and protecting a next-stage system from being damaged when the circuit is in fault. The astronautic programmable thermocouple temperature transmitter has the advantages of high intelligent degree, adjustable range, no requirement for hardware debugging, suitability for batch production and suitability for thermocouples of K type, E type, T type and tungsten rhenium type.

Description

technical field [0001] The invention relates to a programmable thermocouple temperature transmitter for aerospace, belonging to the field of electromechanical integration. Background technique [0002] Temperature is an important measurement parameter in aerospace vehicles and weapon models. Thermocouple is one of the main principles of temperature measurement, among which K, E, T and tungsten-rhenium types account for more than 98% of thermocouple products. The number of thermocouples for single-shot carrier and weapon models can reach dozens, even close to 100, and the temperature range can reach dozens. With the high-density launch requirements of aerospace vehicles and weapon models, the number of matching thermocouple temperature transmitters has increased rapidly, which puts forward the requirements for intelligent and mass production. [0003] Existing models of thermocouple temperature transmitters are difficult to meet the above requirements, mainly in: [0004] 1...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): G01K7/02G01K7/13G01K7/026
Inventor 杨显涛王丽萍刘希宝陈青松郑帮林
Owner BEIJING RES INST OF TELEMETRY
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products