CN204033668U - Novel medical calorstat - Google Patents
Novel medical calorstat Download PDFInfo
- Publication number
- CN204033668U CN204033668U CN201420257395.9U CN201420257395U CN204033668U CN 204033668 U CN204033668 U CN 204033668U CN 201420257395 U CN201420257395 U CN 201420257395U CN 204033668 U CN204033668 U CN 204033668U
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- China
- Prior art keywords
- calorstat
- temperature
- circuit
- main body
- body frame
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- Expired - Fee Related
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Abstract
Novel medical calorstat, belongs to technical field of medical instrument.The technical solution of the utility model is: comprise fuselage main body frame, it is characterized in that being provided with chamber door on fuselage main body frame, chamber door is provided with groove, be provided with calorstat on and off switch on the right side of chamber door, above on and off switch, be provided with temperature adjustment knob, above temperature adjustment knob, be provided with time-setting mechanism, display screen is provided with above time-setting mechanism, display screen is provided with time display apparatus, is provided with temperature indicating device on the right side of time display apparatus, is provided with siren on the right side of temperature indicating device.This utility model structure is simple, easy to use, when needs provide a kind of isoperibol to patient, easy and simple to handle, time saving and energy saving, alleviates the work difficulty of medical personnel.
Description
Technical field: this utility model belongs to technical field of medical instrument is a kind of Novel medical calorstat concretely.
Background technology: at present, the calorstat that most of hospital adopts is all more traditional calorstat, calorstat is with low content of technology, most calorstat only has a thermostatic chamber and cool room, make thermostatic chamber there is dead angle like this, and temperature distributing disproportionation is even, and circuit design also exists a lot of irrational place, so heat insulation effect is undesirable, very complicated in operation, add work difficulty to medical personnel.
Summary of the invention: the purpose of this utility model is to provide a kind of when needs provide a kind of isoperibol to patient, easy and simple to handle, time saving and energy saving Novel medical calorstat.
The technical solution of the utility model is: comprise fuselage main body frame, it is characterized in that being provided with chamber door on fuselage main body frame, chamber door is provided with groove, calorstat on and off switch is provided with on the right side of chamber door, temperature adjustment knob is provided with above calorstat on and off switch, time-setting mechanism is provided with above temperature adjustment knob, display screen is provided with above time-setting mechanism, display screen is provided with time display apparatus, temperature indicating device is provided with on the right side of time display apparatus, siren is provided with on the right side of temperature indicating device, fuselage main body frame is provided with thermal-insulating body, thermal-insulating body is provided with thermostatic chamber, thermostatic chamber is provided with temperature sensor, return air inlet is provided with below temperature sensor, guidewire port is provided with on the left of return air inlet, constant voltage room is provided with above thermostatic chamber, constant voltage room is provided with air guide hole, air guide hole is provided with airduct, airduct is provided with airduct mouth, orifice plate is provided with below airduct mouth, constant voltage is provided with dividing plate on the left of room, cool room is provided with on the left of dividing plate, cool room is provided with ac fan, semiconductor chilling plate is provided with below ac fan, instrument placing trough is provided with below semiconductor chilling plate, insulating interlayer is provided with on the left of semiconductor chilling plate, insulating interlayer is provided with heat-preservation cotton, circuit box is provided with on the left of thermal-insulating body, Single Chip Microcomputer (SCM) system is provided with in circuit box, temperature-control circuit is provided with on the left of Single Chip Microcomputer (SCM) system, temperature-control circuit is provided with thyristor gating circuit, resistance wire is provided with on the left of thyristor gating circuit, display circuit is provided with on the right side of Single Chip Microcomputer (SCM) system, circuit for alarming is provided with on the right side of display circuit.
As preferably, described fuselage main body frame adopts stainless steel material manufacture.
As preferably, described display screen is set to LCDs.
As preferably, described instrument placing trough adopts elastomeric material manufacture.。
This utility model beneficial effect is: this utility model structure is simple, easy to use, when needs provide a kind of isoperibol to medical personnel, easy and simple to handle, time saving and energy saving, alleviates the work difficulty of medical personnel.
Accompanying drawing illustrates:
Accompanying drawing 1 is this utility model structural representation.
Accompanying drawing 2 this utility model circuit box schematic diagram.
In figure 1, fuselage main body frame, 2, chamber door, 3, groove, 4, calorstat on and off switch, 5, temperature adjustment knob, 6, time-setting mechanism, 7, display screen, 8, time display apparatus, 9, temperature indicating device, 10, siren, 11, thermal-insulating body, 12, thermostatic chamber, 13, temperature sensor, 14, return air inlet, 15, guidewire port, 16, constant voltage room, 17, air guide hole, 18, airduct, 19, airduct mouth, 20, orifice plate, 21, dividing plate, 22, cool room, 23, ac fan, 24, semiconductor chilling plate, 25, instrument placing trough, 26, insulating interlayer, 27, heat-preservation cotton, 28, circuit box, 29, Single Chip Microcomputer (SCM) system, 30, temperature-control circuit, 31, thyristor control circuit, 32, resistance wire, 33, display circuit, 34, circuit for alarming.
Detailed description of the invention: comprise fuselage main body frame 1, it is characterized in that being provided with chamber door 2 on fuselage main body frame 1, chamber door 2 is provided with groove 3, calorstat on and off switch 4 is provided with on the right side of chamber door 2, temperature adjustment knob 5 is provided with above calorstat on and off switch 4, time-setting mechanism 6 is provided with above temperature adjustment knob 5, display screen 7 is provided with above time-setting mechanism 6, display screen 7 is provided with time display apparatus 8, temperature indicating device 9 is provided with on the right side of time display apparatus 8, siren 10 is provided with on the right side of temperature indicating device 9, fuselage main body frame 1 is provided with thermal-insulating body 11, thermal-insulating body 11 is provided with thermostatic chamber 12, thermostatic chamber 12 is provided with temperature sensor 13, return air inlet 14 is provided with below temperature sensor 13, guidewire port 15 is provided with on the left of return air inlet 14, constant voltage room 16 is provided with above thermostatic chamber 12, constant voltage room 16 is provided with air guide hole 17, air guide hole 17 is provided with airduct 18, airduct 18 is provided with airduct mouth 19, orifice plate 20 is provided with below airduct mouth 119, dividing plate 21 is provided with on the left of constant voltage room 16, cool room 22 is provided with on the left of dividing plate 21, cool room 22 is provided with ac fan 23, semiconductor chilling plate 24 is provided with below ac fan 23, instrument placing trough 25 is provided with below semiconductor chilling plate 24, insulating interlayer 26 is provided with on the left of semiconductor chilling plate 24, insulating interlayer 26 is provided with heat-preservation cotton 27, circuit box 28 is provided with on the left of thermal-insulating body 11, Single Chip Microcomputer (SCM) system 29 is provided with in circuit box 28, temperature-control circuit 30 is provided with on the left of Single Chip Microcomputer (SCM) system 29, temperature-control circuit 30 is provided with thyristor gating circuit 31, resistance wire 32 is provided with on the left of thyristor gating circuit 31, display circuit 33 is provided with on the right side of Single Chip Microcomputer (SCM) system 29, circuit for alarming 34 is provided with on the right side of display circuit 33.Medical personnel by the temperature regulating temperature adjustment knob 5 control in calorstat, can understand the temperature inside the box by siren 10 too high or too low to be regulated temperature, air guide hole 17 can make air-flow enter calorstat after more even.
As preferably, described fuselage main body frame 1 adopts stainless steel material manufacture.Such setting, fuselage main body frame 1 quality of the present utility model is light, easy to clean.
As preferably, described display screen 7 is set to LCDs, arranges like this, and the display effect of display screen 7 of the present utility model will be finer and smoother, clear.
As preferably, described instrument placing trough 25 adopts elastomeric material manufacture, arranges like this, and instrument placing trough 25 of the present utility model will be more wear-resisting, corrosion-resistant, and noiselessness during place tool.
Claims (4)
1. Novel medical calorstat, comprise fuselage main body frame (1), it is characterized in that: on fuselage main body frame (1), be provided with chamber door (2), chamber door (2) is provided with groove (3), chamber door (2) right side is provided with calorstat on and off switch (4), calorstat on and off switch (4) top is provided with temperature adjustment knob (5), temperature adjustment knob (5) top is provided with time-setting mechanism (6), time-setting mechanism (6) top is provided with display screen (7), display screen (7) is provided with time display apparatus (8), time display apparatus (8) right side is provided with temperature indicating device (9), temperature indicating device (9) right side is provided with siren (10), fuselage main body frame (1) is provided with thermal-insulating body (11), thermal-insulating body (11) is provided with thermostatic chamber (12), thermostatic chamber (12) is provided with temperature sensor (13), temperature sensor (13) below is provided with return air inlet (14), return air inlet (14) left side is provided with guidewire port (15), thermostatic chamber (12) top is provided with constant voltage room (16), constant voltage room (16) is provided with air guide hole (17), air guide hole (17) is provided with airduct (18), airduct (18) is provided with airduct mouth (19), airduct mouth (19) below is provided with orifice plate (20), left side, constant voltage room (16) is provided with dividing plate (21), dividing plate (21) left side is provided with cool room (22), cool room (22) is provided with ac fan (23), ac fan (23) below is provided with semiconductor chilling plate (24), semiconductor chilling plate (24) below is provided with instrument placing trough (25), semiconductor chilling plate (24) left side is provided with insulating interlayer (26), insulating interlayer (26) is provided with heat-preservation cotton (27), thermal-insulating body (11) left side is provided with circuit box (28), Single Chip Microcomputer (SCM) system (29) is provided with in circuit box (28), Single Chip Microcomputer (SCM) system (29) left side is provided with temperature-control circuit (30), temperature-control circuit (30) is provided with thyristor control circuit (31), thyristor control circuit (31) left side is provided with resistance wire (32), Single Chip Microcomputer (SCM) system (29) right side is provided with display circuit (33), display circuit (33) right side is provided with circuit for alarming (34).
2. Novel medical calorstat according to claim 1, is characterized in that: fuselage main body frame (1) adopts stainless steel material manufacture.
3. Novel medical calorstat according to claim 1, is characterized in that: display screen (7) is set to LCDs.
4. Novel medical calorstat according to claim 1, is characterized in that: instrument placing trough (25) adopts elastomeric material manufacture.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420257395.9U CN204033668U (en) | 2014-05-13 | 2014-05-13 | Novel medical calorstat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420257395.9U CN204033668U (en) | 2014-05-13 | 2014-05-13 | Novel medical calorstat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204033668U true CN204033668U (en) | 2014-12-24 |
Family
ID=52234386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420257395.9U Expired - Fee Related CN204033668U (en) | 2014-05-13 | 2014-05-13 | Novel medical calorstat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204033668U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105004038A (en) * | 2015-07-21 | 2015-10-28 | 南京鼎瑞医疗器械有限公司 | Medical liquid constant-temperature box |
| CN107233671A (en) * | 2017-08-09 | 2017-10-10 | 宁波戴维医疗器械股份有限公司 | A kind of Icterus treatment box and its temperature control method |
-
2014
- 2014-05-13 CN CN201420257395.9U patent/CN204033668U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105004038A (en) * | 2015-07-21 | 2015-10-28 | 南京鼎瑞医疗器械有限公司 | Medical liquid constant-temperature box |
| CN107233671A (en) * | 2017-08-09 | 2017-10-10 | 宁波戴维医疗器械股份有限公司 | A kind of Icterus treatment box and its temperature control method |
| CN107233671B (en) * | 2017-08-09 | 2019-09-06 | 宁波戴维医疗器械股份有限公司 | A kind of Icterus treatment box and its temperature control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141224 Termination date: 20150513 |
|
| EXPY | Termination of patent right or utility model |