CN209197922U - A kind of flexibility multi-measuring point thermocouple structure - Google Patents

A kind of flexibility multi-measuring point thermocouple structure Download PDF

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Publication number
CN209197922U
CN209197922U CN201822047508.3U CN201822047508U CN209197922U CN 209197922 U CN209197922 U CN 209197922U CN 201822047508 U CN201822047508 U CN 201822047508U CN 209197922 U CN209197922 U CN 209197922U
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China
Prior art keywords
thermocouple
flexible
metallic wiring
wiring box
measuring point
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Active
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CN201822047508.3U
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Chinese (zh)
Inventor
李明
张磊
钱学富
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Suzhou Changfeng Avionics Co Ltd
Suzhou Changfeng Aviation Electronics Co Ltd
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Suzhou Changfeng Aviation Electronics Co Ltd
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Priority to CN201822047508.3U priority Critical patent/CN209197922U/en
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Abstract

The utility model provides a kind of flexible multi-measuring point thermocouple structure, including thermocouple, flexible compensation cable, metallic wiring box, output end socket, wherein thermocouple and corresponding polar flexible compensation cable welding, several flexible compensation cables are connected in parallel in metallic wiring box, and the compensating wire after parallel connection is connect with output end socket.More thermocouples are connected in parallel to the metallic wiring box of sealing by the utility model by compensating wire flexible, the mean temperature of section combustion gas is exported by the output end socket in metallic wiring box, the resistance to Electromagnetic Compatibility of metallic wiring box is strong, and flexible compensation conducting wire is easily installed and fixes.In addition, terminal box is installed on cold end, it is protected from the influence of engine high-temperature environment, is conducive to the selection of connector and nonmetallic materials.The resistance to Electromagnetic Compatibility of the utility model is high, and the market competitiveness is strong, has a extensive future.

Description

A kind of flexibility multi-measuring point thermocouple structure
Technical field
The utility model belongs to thermocouple sensor design field, and in particular to a kind of flexibility multi-measuring point thermocouple junction Structure.
Background technique
For the mean temperature for measuring the section combustion gas of aero-engine temperature, conventional junction as shown in Fig. 3 is generallyd use Structure, specially using the structure of collector ring and several single branch thermocouples, collector ring passes through lug plate and nut and thermocouple Binding post is fixedly connected, by thermocouple signal parallel output.Structure dismounting is complicated, is unfavorable for the maintenance of engine, Er Qieji The junction of electric ring and thermocouple is exposed structure, is not suitable for the environment high applied to EMC Requirements.
There is also rigid multi-measuring point thermocouples at present, as shown in Fig. 4.The thermocouple of such structure not only processes complexity, Installation maintenance is difficult, and use scope is limited to, and applies on the engine that section radius is small, power is small more.
Utility model content
A kind of the purpose of the utility model is to provide structures flexible multi-measuring point thermocouple structure simple, easy for installation, and The environment high suitable for EMC Requirements.
In order to realize above-mentioned purpose of utility model, the utility model provides the following technical solution: a kind of flexible more surveys Point thermocouple structure, including thermocouple, flexible compensation cable, metallic wiring box, output end socket, wherein thermocouple and corresponding pole Property flexible compensation cable welding, several flexible compensation cables are connected in parallel in metallic wiring box, it is in parallel after compensation Conducting wire is connect with output end socket.
Preferably, the thermocouple and flexible compensation cable use the material with indexing, ensure that the precision of measurement.
Preferably, the outside of the flexible compensation conducting wire is equipped with stainless steel metal wired tube, plays the work of electromagnetic shielding With.
Preferably, the metallic wiring box is the can of sealing, nonmetallic materials is filled in box, for sealing and fixing Flexible compensation conducting wire.
The utility model beneficial effect achieved is: the utility model using all-metal sealing structure multi-measuring point Thermocouple, resistance to Electromagnetic Compatibility is high, and the market competitiveness is strong, has a extensive future.
In material selection, original aviation armoured thermocouple cable is replaced using compensating cable flexible, is not only passed through Ji property is good, and simple process, and from being bent, being heat-treated, the production cycle is also greatly improved.
In installation, flexibility multi-measuring point thermocouple provided by the utility model will not generate interference because of pipeline, more It will not be confined to the radius of engine.
In addition, metallic wiring box is installed on the cold end of engine, mainly it is made of nonmetallic materials inside metallic wiring box. It is limited to 300 DEG C of nonmetallic materials and connector for most of High-temperature-respolent polent, can satisfy in the environment of engine cold end Requirement.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model.
Fig. 2 is the top view of Fig. 1.
Fig. 3 is conventional junction composition.
Fig. 4 is rigid multi-measuring point thermocouple junction composition.
In Fig. 1 and Fig. 2: 1, thermocouple;2, flexible compensation cable;3, metallic wiring box;4, output end socket.
In Fig. 3: 31, collector ring;32, thermocouple.
In Fig. 4: 41, thermocouple sensor;42, armored cable;43, metallic wiring box;44, it pops one's head in;45, mounting base;46, Rivet;47, installing tache.
Specific embodiment
It elaborates with reference to the accompanying drawing to this patent:
A kind of flexible multi-measuring point thermocouple structure as shown in Figure 1 and Figure 2, thermocouple 1 are mended with corresponding polar flexibility It repays cable 2 and carries out the logical welding of silver, guarantee that connection is reliable.The thermocouple 1 and flexible compensation cable 2 are using the material with indexing. The outside of the flexible compensation conducting wire 2 is equipped with stainless steel metal wired tube.
Several flexible compensation cables 2 are connected in parallel in metallic wiring box 3, then by after parallel connection conducting wire and output Socket 4 corresponding polar contact pin in end is welded, and the mean temperature of section combustion gas is exported by output end socket 4, guarantees thermoelectricity The signal output engine control system of gesture.
The metallic wiring box 3 is the can of sealing, the nonmetallic materials such as filled silicon rubber in box, for sealing and consolidating Determine flexible compensation conducting wire 2.
The metallic wiring box 3 is installed on cold end, is protected from the influence of engine high-temperature environment, be conducive to connector and The selection of nonmetallic materials.

Claims (4)

1. a kind of flexibility multi-measuring point thermocouple structure, it is characterised in that: including thermocouple (1), flexible compensation cable (2), metal Terminal box (3), output end socket (4), wherein thermocouple (1) is welded with corresponding polar flexible compensation cable (2), several flexibilities Compensating cable (2) is connected in parallel in metallic wiring box (3), and the compensating wire after parallel connection is connect with output end socket (4).
2. a kind of flexible multi-measuring point thermocouple structure as described in claim 1, it is characterised in that: the thermocouple (1) and soft Property compensating cable (2) using with indexing material.
3. a kind of flexible multi-measuring point thermocouple structure as described in claim 1, it is characterised in that: the flexible compensation cable (2) outside is equipped with stainless steel metal wired tube.
4. a kind of flexible multi-measuring point thermocouple structure as described in claim 1, it is characterised in that: the metallic wiring box (3) For the can of sealing, box is interior to fill nonmetallic materials.
CN201822047508.3U 2018-12-07 2018-12-07 A kind of flexibility multi-measuring point thermocouple structure Active CN209197922U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822047508.3U CN209197922U (en) 2018-12-07 2018-12-07 A kind of flexibility multi-measuring point thermocouple structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822047508.3U CN209197922U (en) 2018-12-07 2018-12-07 A kind of flexibility multi-measuring point thermocouple structure

Publications (1)

Publication Number Publication Date
CN209197922U true CN209197922U (en) 2019-08-02

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201822047508.3U Active CN209197922U (en) 2018-12-07 2018-12-07 A kind of flexibility multi-measuring point thermocouple structure

Country Status (1)

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CN (1) CN209197922U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110455427A (en) * 2019-09-23 2019-11-15 中国船舶重工集团公司第七0三研究所 Non-cooled high temperature galvanic couple rake

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110455427A (en) * 2019-09-23 2019-11-15 中国船舶重工集团公司第七0三研究所 Non-cooled high temperature galvanic couple rake

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