CN110987217A - Temperature measurement clothes and temperature sensor - Google Patents

Temperature measurement clothes and temperature sensor Download PDF

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Publication number
CN110987217A
CN110987217A CN201911183167.5A CN201911183167A CN110987217A CN 110987217 A CN110987217 A CN 110987217A CN 201911183167 A CN201911183167 A CN 201911183167A CN 110987217 A CN110987217 A CN 110987217A
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CN
China
Prior art keywords
temperature
measurement
lead
sensing element
suit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201911183167.5A
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Chinese (zh)
Inventor
王鹏
任侃
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Suzhou Changfeng Avionics Co Ltd
Suzhou Changfeng Aviation Electronics Co Ltd
Original Assignee
Suzhou Changfeng Aviation Electronics Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Suzhou Changfeng Aviation Electronics Co Ltd filed Critical Suzhou Changfeng Aviation Electronics Co Ltd
Priority to CN201911183167.5A priority Critical patent/CN110987217A/en
Publication of CN110987217A publication Critical patent/CN110987217A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K7/00Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements
    • G01K7/16Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements using resistive elements
    • G01K7/18Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements using resistive elements the element being a linear resistance, e.g. platinum resistance thermometer
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K1/00Details of thermometers not specially adapted for particular types of thermometer
    • G01K1/02Means for indicating or recording specially adapted for thermometers
    • G01K1/024Means for indicating or recording specially adapted for thermometers for remote indication
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K1/00Details of thermometers not specially adapted for particular types of thermometer
    • G01K1/02Means for indicating or recording specially adapted for thermometers
    • G01K1/026Means for indicating or recording specially adapted for thermometers arrangements for monitoring a plurality of temperatures, e.g. by multiplexing

Abstract

The embodiment of the disclosure provides a temperature measurement suit and a temperature sensor, which belong to the technical field of temperature measurement, the temperature measurement suit in the embodiment of the disclosure is applied to the measurement of the ambient temperature of a pilot, the temperature measurement suit comprises a measurement suit body, at least two temperature sensors arranged in the measurement suit body, a lead connected with the temperature sensors and a data transmitter, the at least two temperature sensors are converged to the data transmitter through the lead, and the data transmitter is used for collecting data detected by the temperature sensors and transmitting the data to equipment connected to the data transmitter. According to the method, the cross-linking between the aircraft cabin data acquisition and recording system is omitted, wiring in a narrow space of an aircraft cabin is not needed, and therefore the operation action of a pilot can be completely unaffected.

Description

Temperature measurement clothes and temperature sensor
Technical Field
The present disclosure relates to the field of temperature measurement technology, and in particular, to a temperature measurement garment and a temperature sensor.
Background
When the environmental temperature fields of the cabin and other parts in the field of airplane temperature measurement have measurement requirements, the positions are generally complex in layout and limited in structure, no structure capable of being mechanically mounted exists in the measuring point position, and the temperature measuring surface has complex mounting surface conditions such as a curved surface and a cylindrical surface besides a plane, so that the problem of measuring the environmental temperature in the areas is solved. At present, the temperature field in the cabin of a domestic passenger plane is measured by adopting a simple distributed wiring measurement mode, namely a temperature sensor is arranged at the front end, and a sensor signal is sent to a rear-end acquisition device through wiring.
It can be seen that the existing measuring instruments for collecting temperature in the passenger compartment have the problems of disordered distribution and obstruction to the operation of the pilot.
Disclosure of Invention
In view of the above, embodiments of the present disclosure provide a temperature measurement garment and a temperature sensor, which at least partially solve the problems in the prior art.
In a first aspect, the disclosed embodiment provides a temperature measurement suit, which is applied to measurement of ambient temperature of a pilot, and the temperature measurement suit comprises a measurement suit body, at least two temperature sensors arranged in the measurement suit body, a lead connected with the temperature sensors, and a data transmitter, wherein the at least two temperature sensors are converged to the data transmitter through the lead, and the data transmitter is used for collecting data detected by the temperature sensors and transmitting the data to equipment connected to the data transmitter.
According to a specific implementation manner of the embodiment of the disclosure, the lead is fixed on the outer side of the measurement suit body.
According to a specific implementation manner of the embodiment of the disclosure, the wire is made of teflon.
According to a specific implementation manner of the embodiment of the present disclosure, the temperature measurement suit further includes a wire fixing groove for fixing the wire.
According to a specific implementation manner of the embodiment of the present disclosure, the number of the temperature sensors is 13, and the 13 temperature sensors are set at positions corresponding to different regions of the human body according to the acquisition requirement.
According to a specific implementation manner of the embodiment of the present disclosure, 13 temperature sensors are respectively disposed in regions corresponding to a left shoulder, a right shoulder, a left chest, a right chest, an abdomen, a left knee, a right knee, a left ankle, a right ankle, and a head of a human body.
According to a specific implementation manner of the embodiment of the disclosure, the part of the measurement suit body where the data transmitter is installed is of an interlayer structure with an opening, and the data transmitter is installed in the interlayer.
According to a specific implementation manner of the embodiment of the present disclosure, the temperature sensor is a platinum resistance temperature sensor.
According to a specific implementation manner of the embodiment of the present disclosure, the temperature sensor includes a temperature measuring area located at the front end, a middle-end transition area, and a connection area located at the tail end;
the temperature measuring area comprises a temperature sensing element, and the temperature sensing element is used for sensing the surface temperature of the object to be measured; the transition area comprises a polyimide film, an adhesive and a copper foil, and the connecting area comprises a lead; the flexible structure formed by the polyimide film, the adhesive and the copper foil is used for bearing a temperature sensing element of the temperature measuring area at the front end and a lead of the connecting area at the tail end, and the temperature sensing element and the lead realize signal transmission through the copper foil.
In a second aspect, the embodiments of the present disclosure provide a temperature sensor applied to the temperature measurement suit according to any one of claims 1 to 9; the temperature sensor comprises a temperature measuring area positioned at the front end, a middle-end transition area and a connecting area at the tail end;
the temperature measuring area comprises a temperature sensing element, and the temperature sensing element is used for sensing the surface temperature of the object to be measured; the transition area comprises a polyimide film, an adhesive and a copper foil, and the connecting area comprises a lead; the flexible structure formed by the polyimide film, the adhesive and the copper foil is used for bearing a temperature sensing element of the temperature measuring area at the front end and a lead of the connecting area at the tail end, and the temperature sensing element and the lead realize signal transmission through the copper foil.
The temperature measurement suit in the embodiment of the disclosure is applied to measurement of ambient temperature of pilots, and comprises a measurement suit body, at least two temperature sensors arranged in the measurement suit body, a lead connected with the temperature sensors and a data transmitter, wherein the at least two temperature sensors are converged to the data transmitter through the lead, and the data transmitter is used for acquiring data detected by the temperature sensors and transmitting the data to equipment connected to the data transmitter. According to the method, the cross-linking between the integrated temperature measurement device and an airplane airborne data acquisition and recording system is omitted, wiring in a narrow space of an airplane cabin is not needed, therefore, the operation action of a pilot can be completely unaffected, in addition, the temperature measurement points are arranged on the pilot's one-piece suit to measure the temperature, the temperature can meet the cold and heat feeling of the pilot as much as possible, and the distribution of the temperature field around the pilot can be truly and objectively reflected.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present disclosure, the drawings needed to be used in the embodiments will be briefly described below, and it is apparent that the drawings in the following description are only some embodiments of the present disclosure, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic diagram of an arrangement of sensors in a temperature measurement garment provided by an embodiment of the present disclosure;
FIG. 2 is a front cross-sectional view of a temperature sensor provided by an embodiment of the present disclosure;
fig. 3 is a top view of a flexible patch temperature sensor provided by embodiments of the present disclosure.
Summary of reference numerals:
1-temperature sensing element, 2-PI polyimide film, 3-adhesive, 4-copper foil, 5-limit frame, 6-high temperature resistant silicon rubber and 7-lead
Detailed Description
The embodiments of the present disclosure are described in detail below with reference to the accompanying drawings.
The embodiments of the present disclosure are described below with specific examples, and other advantages and effects of the present disclosure will be readily apparent to those skilled in the art from the disclosure in the specification. It is to be understood that the described embodiments are merely illustrative of some, and not restrictive, of the embodiments of the disclosure. The disclosure may be embodied or carried out in various other specific embodiments, and various modifications and changes may be made in the details within the description without departing from the spirit of the disclosure. It is to be noted that the features in the following embodiments and examples may be combined with each other without conflict. All other embodiments, which can be derived by a person skilled in the art from the embodiments disclosed herein without making any creative effort, shall fall within the protection scope of the present disclosure.
It is noted that various aspects of the embodiments are described below within the scope of the appended claims. It should be apparent that the aspects described herein may be embodied in a wide variety of forms and that any specific structure and/or function described herein is merely illustrative. Based on the disclosure, one skilled in the art should appreciate that one aspect described herein may be implemented independently of any other aspects and that two or more of these aspects may be combined in various ways. For example, an apparatus may be implemented and/or a method practiced using any number of the aspects set forth herein. Additionally, such an apparatus may be implemented and/or such a method may be practiced using other structure and/or functionality in addition to one or more of the aspects set forth herein.
It should be noted that the drawings provided in the following embodiments are only for illustrating the basic idea of the present disclosure, and the drawings only show the components related to the present disclosure rather than the number, shape and size of the components in actual implementation, and the type, amount and ratio of the components in actual implementation may be changed arbitrarily, and the layout of the components may be more complicated.
In addition, in the following description, specific details are provided to facilitate a thorough understanding of the examples. However, it will be understood by those skilled in the art that the aspects may be practiced without these specific details.
Referring to fig. 1, the temperature measurement suit provided by the embodiment of the present disclosure is applied to measurement of ambient temperature of a pilot, and includes a measurement suit body, at least two temperature sensors disposed in the measurement suit body, a wire connected to the temperature sensors, and a data transmitter, wherein the at least two temperature sensors are converged to the data transmitter through the wire, and the data transmitter is configured to collect data detected by the temperature sensors and transmit the data to a device connected to the data transmitter. The method of the embodiment of the disclosure omits the cross-linking with the airborne data acquisition and recording system of the airplane, and does not need to wire in the narrow space of the airplane cockpit, so that the operation action of the pilot can be completely unaffected, the generalization is realized, the method can be popularized to other airplanes for use, the difficulty of airplane test modification is reduced, the cost is reduced, and the test progress of the domestic airliner is accelerated. In addition, the temperature measurement points are arranged on the pilot's coverall to measure the temperature, so that the temperature can meet the cold and hot feeling of the pilot as much as possible, and the temperature field distribution around the pilot can be truly and objectively reflected.
Specifically, the temperature measurement suit of the embodiment of the disclosure is a suit customized by adopting a specific material, when the ambient temperature in the cabin of the airplane is measured, a pilot wears the temperature measurement suit before entering the cabin, a connector of a temperature measurement system is in butt joint with a connector of an onboard wire, and finally a module is fixed by tying a belt, the airplane takes off, and a temperature acquisition system of the temperature measurement suit records temperature parameters. Therefore, the temperature measurement suit of the embodiment of the disclosure can completely avoid influencing the operation action of the pilot.
The temperature measurement clothes of the embodiment of the disclosure comprise a measurement clothes body, at least two temperature sensors arranged in the measurement clothes body, a wire connected with the temperature sensors and a data transmitter, wherein the basic working principle of the temperature measurement clothes body is that the temperature of the surrounding environment of a pilot is sensed by the temperature sensors arranged in the measurement clothes body, the collected data is transmitted to the data transmitter through the wire, the data transmitter is provided with a data interface and can be connected with external equipment, and the temperature data transmitted by the temperature sensors is transmitted to the external equipment through the data transmitter. In addition, the data transmission device only transmits data externally connected equipment, except for the wired transmission through the data interface, the data transmission can also be performed in a wireless transmission mode, for example, wireless transmission through bluetooth, Wifi wireless transmission and the like.
It should be noted that the data transmitter may be disposed at a corresponding waist position of the temperature measurement suit, and preferably, at the position, the temperature measurement suit is designed to have a sandwich structure, and the sandwich structure has an opening, a plurality of wires may be gathered to the data transmitter, and are gathered together by the sandwich structure, so that the arrangement of the plurality of wires does not appear cluttered, and the operation action of the pilot is not affected by the arrangement of the plurality of wires. The opening design of the sandwich structure is also convenient for the insertion of a data interface of the data transmitter and the connection of external equipment and the data transmitter.
In addition, the temperature measurement clothes of the embodiment of the disclosure are one-piece clothes, the measurement clothes body comprises a hat, a coat and trousers, and the hat, the coat and the trousers are of an integrated structure. The temperature measurement suit adopts the form of one-piece suit, and firstly, the suit is convenient for the pilot to wear, and in addition, the design of the one-piece suit also facilitates the wiring arrangement of a plurality of wires.
In different embodiments, the arrangement mode of the wires in the temperature measurement suit is different, and in the embodiment, the wires of the temperature measurement suit are arranged on the outer side of the measurement suit body, namely on the outer surface of the measurement suit body. Of course, in other embodiments, the wires may be arranged inside the measurement suit body. The embodiment arranges the wire at the surface of measuring clothes body, and mainly be for the convenience fix with the wire and dismantle, still is provided with the wire fixed slot at the surface of measuring clothes body, and this wire fixed slot is used for fixed wire, and the wire fixed slot adopts the cloth to make up at measuring clothes body surface, and the wire passes under this wire fixed slot, lays in the surface of measuring clothes body snugly.
In the above embodiment, the wires are made of teflon, and the wires made of teflon have good flexibility and can be folded, so that the wires can be conveniently wired on the measuring clothes body.
In this embodiment, the number of the temperature sensors is 13, and the 13 temperature sensors are set at positions corresponding to different regions of the human body according to the acquisition requirements. 13 the temperature sensors are respectively arranged in the areas corresponding to the left shoulder, the right shoulder, the left chest, the right chest, the abdomen, the left knee, the right knee, the left ankle, the right ankle and the head of the human body. The temperature monitoring suit comprises a wire harness, 10 temperature sensors, a flying suit cap, 13 temperature sensors, a belt, a power supply and a power supply, wherein the 10 temperature sensors are respectively arranged at the left shoulder, the right shoulder, the chest, the abdomen, the left knee, the right knee, the left ankle and the right ankle of the wire harness; and the data is transmitted to monitoring equipment through a gathering wire for monitoring the ambient temperature of the pilot.
Wherein, the temperature sensor is a platinum resistance temperature sensor. The temperature sensor comprises a temperature measuring area positioned at the front end, a middle-end transition area and a connecting area at the tail end;
the temperature measuring area comprises a temperature sensing element, and the temperature sensing element is used for sensing the surface temperature of the object to be measured; the transition area comprises a polyimide film, an adhesive and a copper foil, and the connecting area comprises a lead; the flexible structure formed by the polyimide film, the adhesive and the copper foil is used for bearing a temperature sensing element of the temperature measuring area at the front end and a lead of the connecting area at the tail end, and the temperature sensing element and the lead realize signal transmission through the copper foil.
Referring to fig. 2 and 3, the overall size of the temperature sensor is small, and the temperature sensor can be adapted to a limited installation space; the total thickness is not more than 0.113mm, the flexible glass has excellent flexibility and certain strength, and can resist the temperature in the range of-55 ℃ to 260 ℃; the temperature measuring regions belong to flexible and flexible regions within the length range of 20mm, the flexible angle range reaches 0-270 degrees, and the temperature measuring regions can be well adapted to special installation surfaces such as curved surfaces, cylindrical surfaces and the like; the connection between the temperature sensing element and the lead is carried by the flexible structure, and on the premise of ensuring signal transmission, the bending and twisting during installation can not influence the positions of two welding points, so that the welding points can be prevented from being acted by external stress, and the reliability and the service life of a product can be ensured; the temperature-sensing element and the high-temperature-resistant silicon rubber coated at the welding point of the lead can play a role in fixing and protecting, so that the welding point is further protected from being damaged by external stress; the flexible structure is in a modular design, under the condition that the structure of the flexible structure is not changed, the function of changing output signals can be realized by changing temperature sensing elements with different scales, and the output function of a two-wire system, a three-wire system or a four-wire system can be realized by changing the specification of the number of the wire cores.
The embodiment of the invention provides a temperature sensor, referring to fig. 2 and 3, a temperature sensor main body is supported by a flexible structure, the front end of the temperature sensor main body is a temperature measuring area, and the temperature sensor comprises a platinum resistance temperature sensing element 1 which is directly arranged on a temperature measuring surface and used for sensing the temperature of the temperature measuring surface; the middle section is a transition area and comprises a PI polyimide film 2, an adhesive 3 and a copper foil 4, the connection of a front-end temperature measuring area and a tail-end connecting area is realized through a flexible structure, and the transition area is used for bending and twisting transition during installation; the tail end is a connection area which comprises a limit frame 5, high-temperature-resistant silicon rubber 6 and a lead 7 and is used for connecting and fixing an output lead.
The flexible structure mainly comprises a polyimide film 2, an adhesive 3 and a copper foil 4, wherein the thickness of the polyimide film 2 is 25 micrometers, the polyimide film is divided into 2 pieces, the polyimide film is divided into a polyimide base material and a polyimide cover film, the surface of the polyimide cover film needs to be provided with square holes, the positions of the holes are shown in figure 2, the temperature measuring areas are 2, and the connecting areas are 4; the adhesive 3 has two thicknesses of 20 micrometers and 25 micrometers, is 2 sheets, is also divided into an adhesive base material and an adhesive covering film, and the adhesive covering film also needs to be subjected to hole opening treatment and has the same position and quantity as the polyimide covering film; the copper foil is 18 μm thick and has 2 pieces, and 3 square bonding pads are processed on the copper foil, and are respectively arranged at two ends (C, D and E, F) and a middle section (A, B) as shown in fig. 2, and the bonding pads are connected in pairs. Covering an adhesive base material on a polyimide base material, symmetrically pasting 2 copper foils 4 on the adhesive base material according to the central line position shown in figure 2, wherein a pad in the middle section is positioned in a temperature measuring area, pads at two ends are positioned in a connecting area, covering an adhesive covering film and the polyimide covering film on the copper foils 4 in sequence, ensuring that the position of an opening is consistent with the position of the copper foil pad, exposing the pad, finally hot-pressing at high temperature of 160 ℃, cooling and solidifying to complete the bonding of the PI polyimide film 2 and the copper foils 4, wherein the total thickness of the assembly is not more than 0.113 mm. And performing electroless nickel-gold treatment on the assembly to protect the exposed bonding pad from oxidation corrosion, wherein the thickness of the gold layer is 0.03-0.09 mu m, the thickness of the nickel layer is 2-6 mu m, and cleaning after welding. And finally, bonding the limiting frame on the surface of the assembly connecting area by using high-temperature-resistant glue to complete the assembly of the flexible structure assembly.
According to the requirement of an output signal, the platinum resistance temperature sensing element 1 adopts two indexing specifications of PT100 or PT1000, after the specification of the element is determined, the length of a pin of the platinum resistance temperature sensing element 1 is trimmed to 2-3 mm, the pin is arranged to be capable of simultaneously contacting a pad A, B of a temperature measuring area shown in figure 2, the pin of the platinum resistance temperature sensing element 1 is welded by an electric soldering iron at the pad by adopting high-temperature soldering tin, and the condition of burrs and false soldering is not required to exist in the post-welding inspection. And preparing high-temperature-resistant silicon rubber, coating the back surface and the pins of the platinum resistance temperature sensing element 1, and curing at normal temperature for 8 hours.
The specification of the wire 7 is selected according to the output form requirement. When two-wire output is needed, a 2-core shielding cable is selected, sheaths and shielding layers at two ends of a lead 7 are stripped, 2 core conductors and insulating layers are exposed, one end of the lead 7 is arranged in a connecting area limiting frame and is close to the surface of the flexible structure assembly, and the core conductors of the lead 7 are welded at a welding pad D, E by using an electric iron through high-temperature soldering tin; when three-wire output is needed, a 3-core shielded cable is selected, the processing technology of the lead 7 is the same as that of the shielded cable, and a lead conductor of the lead 7 is welded at the welding pad C, D, E by using an electric iron through high-temperature soldering tin; when four-wire system output is needed, a 4-core shielding cable is selected, the treatment process of the wire 7 is the same as that of the shielding cable, and the wire 7 core conductor is welded at the welding disc C, D, E, F by using an electric iron through high-temperature soldering tin. And after welding, preparing high-temperature-resistant silicon rubber, coating and filling the high-temperature-resistant silicon rubber in the limiting frame to be as high as the limiting frame, so that the conductor and the insulating layer of the wire core of the lead 7 are not exposed, and curing at normal temperature for 8 hours to finish the final assembly of the sensor.
The above description is only for the specific embodiments of the present disclosure, but the scope of the present disclosure is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present disclosure should be covered within the scope of the present disclosure. Therefore, the protection scope of the present disclosure shall be subject to the protection scope of the claims.

Claims (10)

1. The temperature measurement suit is characterized by being applied to measurement of ambient temperature of a pilot, and comprising a measurement suit body, at least two temperature sensors arranged in the measurement suit body, a lead connected with the temperature sensors and a data transmitter, wherein the at least two temperature sensors are converged to the data transmitter through the lead, and the data transmitter is used for collecting data detected by the temperature sensors and transmitting the data to equipment connected to the data transmitter.
2. The temperature measurement suit of claim 1, wherein said wires are fixed to the outside of said measurement suit body.
3. The temperature measurement garment of claim 1, wherein the wire is made of teflon.
4. The temperature measurement garment of claim 1, further comprising a wire securing slot for securing the wire.
5. The temperature measurement garment of claim 1, wherein the number of the temperature sensors is 13, and the 13 temperature sensors are set at positions corresponding to different regions of the human body according to acquisition requirements.
6. The temperature measuring garment of claim 5, wherein 13 temperature sensors are respectively provided in regions corresponding to a left shoulder, a right shoulder, a left chest, a right chest, an abdomen, a left knee, a right knee, a left ankle, a right ankle, and a head of the human body.
7. The temperature measurement suit of claim 1, wherein the portion of the measurement suit body where the data transmitter is installed is a sandwich structure having an opening, and the data transmitter is installed in the sandwich.
8. The temperature measurement garment of any one of claims 1 to 7, wherein the temperature sensor is a platinum resistance temperature sensor.
9. The temperature measurement garment of claim 8, wherein the temperature sensor comprises a temperature measurement zone at a front end, a middle end transition zone, and a connection zone at a rear end;
the temperature measuring area comprises a temperature sensing element, and the temperature sensing element is used for sensing the surface temperature of the object to be measured; the transition area comprises a polyimide film, an adhesive and a copper foil, and the connecting area comprises a lead; the flexible structure formed by the polyimide film, the adhesive and the copper foil is used for bearing a temperature sensing element of the temperature measuring area at the front end and a lead of the connecting area at the tail end, and the temperature sensing element and the lead realize signal transmission through the copper foil.
10. A temperature sensor, which is applied to the temperature measurement suit according to any one of claims 1 to 9; the temperature sensor comprises a temperature measuring area positioned at the front end, a middle-end transition area and a connecting area at the tail end;
the temperature measuring area comprises a temperature sensing element, and the temperature sensing element is used for sensing the surface temperature of the object to be measured; the transition area comprises a polyimide film, an adhesive and a copper foil, and the connecting area comprises a lead; the flexible structure formed by the polyimide film, the adhesive and the copper foil is used for bearing a temperature sensing element of the temperature measuring area at the front end and a lead of the connecting area at the tail end, and the temperature sensing element and the lead realize signal transmission through the copper foil.
CN201911183167.5A 2019-11-27 2019-11-27 Temperature measurement clothes and temperature sensor Pending CN110987217A (en)

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CN201911183167.5A CN110987217A (en) 2019-11-27 2019-11-27 Temperature measurement clothes and temperature sensor

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112689431A (en) * 2020-12-21 2021-04-20 苏州长风航空电子有限公司 Triaxial MEMS chip assembly quality

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Publication number Priority date Publication date Assignee Title
JPS60209157A (en) * 1984-04-03 1985-10-21 Matsushita Electric Ind Co Ltd Device for evaluating environment
CN201767079U (en) * 2010-09-17 2011-03-23 东华大学 Inner wear capable of monitoring temperature
CN103282754A (en) * 2011-01-07 2013-09-04 株式会社村田制作所 Temperature sensor and structure having temperature sensor attached thereto
CN104026770A (en) * 2014-06-25 2014-09-10 襄阳宏伟航空器有限责任公司 Pilot clothes with environment temperature feedback function
CN205333216U (en) * 2015-10-23 2016-06-22 中国飞行试验研究院 Temperature measurement wire clothes around pilot's human body
KR20170115710A (en) * 2016-04-08 2017-10-18 하상균 A heatproof clothing for firefighting
CN109632123A (en) * 2018-12-07 2019-04-16 苏州长风航空电子有限公司 A kind of flexible paste chip temperature sensor

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60209157A (en) * 1984-04-03 1985-10-21 Matsushita Electric Ind Co Ltd Device for evaluating environment
CN201767079U (en) * 2010-09-17 2011-03-23 东华大学 Inner wear capable of monitoring temperature
CN103282754A (en) * 2011-01-07 2013-09-04 株式会社村田制作所 Temperature sensor and structure having temperature sensor attached thereto
CN104026770A (en) * 2014-06-25 2014-09-10 襄阳宏伟航空器有限责任公司 Pilot clothes with environment temperature feedback function
CN205333216U (en) * 2015-10-23 2016-06-22 中国飞行试验研究院 Temperature measurement wire clothes around pilot's human body
KR20170115710A (en) * 2016-04-08 2017-10-18 하상균 A heatproof clothing for firefighting
CN109632123A (en) * 2018-12-07 2019-04-16 苏州长风航空电子有限公司 A kind of flexible paste chip temperature sensor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112689431A (en) * 2020-12-21 2021-04-20 苏州长风航空电子有限公司 Triaxial MEMS chip assembly quality

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