CN105416592A - Onboard incubator and airplane - Google Patents
Onboard incubator and airplane Download PDFInfo
- Publication number
- CN105416592A CN105416592A CN201510865015.9A CN201510865015A CN105416592A CN 105416592 A CN105416592 A CN 105416592A CN 201510865015 A CN201510865015 A CN 201510865015A CN 105416592 A CN105416592 A CN 105416592A
- Authority
- CN
- China
- Prior art keywords
- casing
- temperature
- airborne
- air inlet
- inlet pipe
- 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.)
- Granted
Links
- 238000010438 heat treatment Methods 0.000 claims description 13
- 230000001737 promoting effect Effects 0.000 claims description 4
- 238000004080 punching Methods 0.000 claims description 3
- 238000001816 cooling Methods 0.000 abstract 1
- 239000010408 film Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0614—Environmental Control Systems with subsystems for cooling avionics
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The invention provides an onboard incubator and an airplane. The onboard incubator comprises an incubator body, and a heater and a heat exchanger are arranged in the incubator body. The incubator body is further provided with an air inlet pipe used for connecting the heat exchanger and an air cold source and is also provided with an air outlet pipe enabling the heat exchanger to be communicated with the outside of the incubator body. When the temperature in the incubator body of the onboard incubator is lower than the lowest temperature limit value, the interior of the incubator body is heated, when the temperature in the incubator body is higher than the highest temperature limit value, the interior of the incubator body is cooled, and therefore it is guaranteed that the temperature in the incubator body is kept between the lowest temperature limit value and the highest temperature limit value all the time, and normal use of onboard products in the incubator body is guaranteed. The air cold source is used for cooling the interior of the incubator body, the overall weight of the incubator is lowered, and the onboard using requirement can be met.
Description
Technical field
The present invention relates to a kind of airborne controlled-temperature cabinet and aircraft.
Background technology
Airborne products ambient temperature crosses over wider range, and temperature traverse is violent, but but need namely could reliable operation between minimum temperature limit value and highest temperature limit value under uniform temperature condition for the internal unit of airborne products, components and parts and optical system.The change of airborne products ambient temperature can make the performance of airborne products change, and such as focal length variations, light shaft offset etc. especially also do not have good terms of settlement for the light shaft offset that temperature traverse is brought.Therefore, need to carry out thermostatic control to airborne products, ensure the temperature of interiors of products equipment, components and parts and optical system within the specific limits.
Summary of the invention
The object of the present invention is to provide a kind of airborne controlled-temperature cabinet being applicable to airborne products, in order to ensure airborne products inner temperature stays constant; Meanwhile, present invention also offers a kind of aircraft using this airborne controlled-temperature cabinet.
In order to solve the problems of the technologies described above, airborne controlled-temperature cabinet of the present invention adopts following technical scheme: a kind of airborne controlled-temperature cabinet, comprise casing, box house is provided with temperature booster and heat exchanger, casing being also provided with the air inlet pipe for connecting heat exchanger and gas low-temperature receiver, casing being also provided with the freeing pipe be communicated with outside heat exchanger and envelope.
The admission port of described air inlet pipe is positioned at outside casing, and the position on air inlet pipe outside casing is provided with the control cock controlling air inlet pipe break-make.
Described temperature booster is film heating sheet.
The blower fan for promoting box house air circulation is also provided with in casing.
Also be provided with temperature sensor in casing, temperature sensor is by controller and blower fan, film heating sheet and control cock control linkage.
Aircraft of the present invention adopts following technical scheme: a kind of aircraft, comprise the airborne controlled-temperature cabinet be located in body, described airborne controlled-temperature cabinet comprises casing, box house is provided with temperature booster and heat exchanger, casing being also provided with the air inlet pipe for connecting heat exchanger and gas low-temperature receiver, casing being also provided with the freeing pipe be communicated with outside heat exchanger and envelope.
The admission port of described air inlet pipe is positioned at outside casing, and the position on air inlet pipe outside casing is provided with the control cock controlling air inlet pipe break-make.
Described admission port is communicated with the wind path of punching press source of the gas or carrier aircraft ring control wind.
The blower fan for promoting box house air circulation is also provided with in casing.
Also be provided with temperature sensor in casing, temperature sensor is by controller and blower fan, film heating sheet and control cock control linkage.
Airborne controlled-temperature cabinet inside of the present invention is provided with temperature booster and heat exchanger, when temperature in casing is lower than minimum temperature limit value, can be heated box house by temperature booster, when temperature in casing is higher than highest temperature limit value, air inlet pipe is filled with cold air and by carrying out interchange of heat in heat exchanger and casing, the thermal current after interchange of heat is discharged by freeing pipe, thus lower the temperature in casing, the temperature this ensures that thered in casing can be between minimum temperature limit value and highest temperature restriction all the time, ensure that the normal use of the airborne products in casing.Carry out heat exchange by gas low-temperature receiver in casing, reduce the overall weight of controlled-temperature cabinet, airborne operating needs can be met.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of airborne controlled-temperature cabinet embodiment one of the present invention;
Fig. 2 is the schematic perspective view of airborne controlled-temperature cabinet embodiment one of the present invention;
Fig. 3 is the inner structure schematic diagram of airborne controlled-temperature cabinet embodiment one of the present invention.
Detailed description of the invention
The embodiment one of aircraft of the present invention: comprise the airborne controlled-temperature cabinet be located in body, airborne products 3 is contained in casing 1, and the upper end of casing 1 is also provided with optical window 2 in the position corresponding to airborne products 3.The structure of airborne controlled-temperature cabinet as Figure 1-3, comprises casing 1, and the cleading that casing 1 is made up of PMAm surrounds, lightweight, good heat-insulation effect, can stop the interchange of heat inside and outside casing.
The inside of casing 1 is also provided with the temperature booster 4 for heating box house environment, in order to ensure radiating effect, alleviate the weight of whole controlled-temperature cabinet, temperature booster in the present embodiment adopts film heating sheet, the side that on thin film heater and casing, area is maximum and front and back sides parallel interval are arranged, farthest can increase the area of thin film heater like this, in actv. cabinet space, improve heating effect.Be provided with in casing 1 for carrying out the heat exchanger 5 of heat exchange with box house environment, heat exchanger 5 is fin type heat exchanger.The forward and backward tank wall of casing 1 is also respectively equipped with air inlet pipe 70 and freeing pipe 71, air inlet pipe 70 and freeing pipe 71 are each passed through tank wall, and it is connected on heat exchanger 5 in one end of box house, film heating sheet are also provided with the resigning hole passed for freeing pipe 71.Air inlet pipe 70 is positioned at admission port outside casing for connecting gas low-temperature receiver, and air inlet pipe 70 is being positioned at the control cock 8 outside casing a section being also provided with and controlling air inlet pipe 70 break-make.Also be provided with blower fan 6 in casing 1, blower fan 6, for accelerating the speed air flow in casing, is convenient to the homogeneous temperature reached in casing, and in the present embodiment, blower fan adopts prerotator.
For the ease of realizing automatic control, be also provided with temperature sensor 9 in casing 1, temperature sensor is preferably arranged on the outside of airborne products 3, and temperature sensor is by controller and blower fan 6, film heating sheet and control cock 8 control linkage.When temperature sensor records casing 1 internal temperature lower than minimum temperature limit value, controller control heater 4 starts, control cock 8 is closed, and heat exchanger can not by carrying out interchange of heat outside tracheae and casing, and in casing, temperature can fast lifting.Now, the casing that cleading is made can stop case intimate heat outwards to run off.When temperature sensor records box interior temperature higher than highest temperature limit value, controller control heater 4 is closed, control cock 8 is opened, gas low-temperature receiver to be filled with in casing 1 by air inlet pipe 70 and to carry out interchange of heat by heat exchanger 5 and casing, thus the ambient temperature in casing is reduced.Now, the casing that cleading is made can stop heat outside casing to box house transmission.
Air inlet pipe can connect punching press source of the gas provides cold air, certainly in order to better simplify structure and the weight of controlled-temperature cabinet, air inlet pipe directly can connect the wind path of carrier aircraft ring control wind, and the extraneous cold wind entered in ring control wind path in flight course by aircraft is as gas low-temperature receiver.
Airborne controlled-temperature cabinet structure of the present invention is simple, small volume, lighter in weight, controls heating in casing and heat radiation by temperature detection, can be good at eliminating aircraft temperature traverse and impact on airborne products in body in flight course.
In above-described embodiment, temperature booster is film heating sheet, can be other forms of temperature booster in other embodiments, as resistive heater; In above-described embodiment, the cleading that casing is made up of PMAm surrounds, and in other embodiments, casing material can be selected according to actual needs, does not specifically limit; In above-described embodiment, blower fan is prerotator, and in other embodiments, blower fan also can be other forms of blower fan.
The embodiment of airborne controlled-temperature cabinet of the present invention: as Figure 1-3, its concrete structure is identical with the airborne controlled-temperature cabinet structure in above-mentioned aircraft embodiment, repeats no more herein.
Claims (10)
1. an airborne controlled-temperature cabinet, it is characterized in that, comprise the casing for loading airborne products, box house is provided with temperature booster and heat exchanger, casing being also provided with the air inlet pipe for connecting heat exchanger and gas low-temperature receiver, casing being also provided with the freeing pipe be communicated with outside heat exchanger and envelope.
2. airborne controlled-temperature cabinet according to claim 1, is characterized in that, the admission port of described air inlet pipe is positioned at outside casing, and the position on air inlet pipe outside casing is provided with the control cock controlling air inlet pipe break-make.
3. airborne controlled-temperature cabinet according to claim 2, is characterized in that, described temperature booster is film heating sheet.
4. airborne controlled-temperature cabinet according to claim 3, is characterized in that, is also provided with the blower fan for promoting box house air circulation in casing.
5. airborne controlled-temperature cabinet according to claim 4, is characterized in that, be also provided with temperature sensor in casing, and temperature sensor is by controller and blower fan, film heating sheet and control cock control linkage.
6. an aircraft, it is characterized in that, comprise the airborne controlled-temperature cabinet be located in airframe, described airborne controlled-temperature cabinet comprises the casing for loading airborne products, box house is provided with temperature booster and heat exchanger, casing being also provided with the air inlet pipe for connecting heat exchanger and gas low-temperature receiver, casing being also provided with the freeing pipe be communicated with outside heat exchanger and envelope.
7. aircraft according to claim 6, is characterized in that, the admission port of described air inlet pipe is positioned at outside casing, and the position on air inlet pipe outside casing is provided with the control cock controlling air inlet pipe break-make.
8. aircraft according to claim 7, is characterized in that, described admission port is communicated with the wind path of punching press source of the gas or carrier aircraft ring control wind.
9. aircraft according to claim 8, is characterized in that, is also provided with the blower fan for promoting box house air circulation in casing.
10. aircraft according to claim 9, is characterized in that, is also provided with temperature sensor in casing, and temperature sensor is by controller and blower fan, film heating sheet and control cock control linkage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510865015.9A CN105416592B (en) | 2015-12-01 | 2015-12-01 | A kind of airborne insulating box and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510865015.9A CN105416592B (en) | 2015-12-01 | 2015-12-01 | A kind of airborne insulating box and aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105416592A true CN105416592A (en) | 2016-03-23 |
| CN105416592B CN105416592B (en) | 2019-01-29 |
Family
ID=55495231
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510865015.9A Active CN105416592B (en) | 2015-12-01 | 2015-12-01 | A kind of airborne insulating box and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105416592B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111874263A (en) * | 2020-07-20 | 2020-11-03 | 上海宇航***工程研究所 | In-situ detector for near-earth space atmospheric environment carried by launch vehicle |
| CN112498652A (en) * | 2021-02-07 | 2021-03-16 | 中国科学院空天信息创新研究院 | Wireless sensor for captive balloon and captive balloon |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2082938U (en) * | 1990-11-30 | 1991-08-14 | 高智 | Multifunctional electric heating pad |
| JP2002320962A (en) * | 2001-04-26 | 2002-11-05 | Japan Science & Technology Corp | Method and device for algiciding |
| CN2802561Y (en) * | 2005-07-07 | 2006-08-02 | 浪潮电子信息产业股份有限公司 | Thremostated container for detecting computer equipment |
| CN101769825A (en) * | 2008-12-29 | 2010-07-07 | 北京卫星环境工程研究所 | Tracking temperature control device for spacecraft thermal vacuum test |
| US20110126565A1 (en) * | 2009-11-30 | 2011-06-02 | Sanyo Electric Co., Ltd. | Incubator |
| CN102161401A (en) * | 2011-02-16 | 2011-08-24 | 青岛澳柯玛股份有限公司 | Novel thermotank |
| CN201993659U (en) * | 2011-03-25 | 2011-09-28 | 山东兆宇电子技术有限公司 | Water cooling intelligent constant-temperature control case |
| CN102213965A (en) * | 2011-04-13 | 2011-10-12 | 苏州捷美电子有限公司 | Thermostatic equipment and control method thereof |
| CN102811518A (en) * | 2011-06-01 | 2012-12-05 | 建碁股份有限公司 | Method for defogging on glass protective cover and display module thereof |
| CN202738131U (en) * | 2012-06-06 | 2013-02-13 | 北京昆仑纵横科技发展有限公司 | Low-temperature-startup film heating device and apparatus using same |
| CN203444369U (en) * | 2013-08-14 | 2014-02-19 | 北京雪迪龙科技股份有限公司 | Constant temperature apparatus |
| CN104808710A (en) * | 2015-04-25 | 2015-07-29 | 北京航空航天大学 | Unmanned helicopter equipment cabin temperature control system capable of utilizing external airflow |
-
2015
- 2015-12-01 CN CN201510865015.9A patent/CN105416592B/en active Active
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2082938U (en) * | 1990-11-30 | 1991-08-14 | 高智 | Multifunctional electric heating pad |
| JP2002320962A (en) * | 2001-04-26 | 2002-11-05 | Japan Science & Technology Corp | Method and device for algiciding |
| CN2802561Y (en) * | 2005-07-07 | 2006-08-02 | 浪潮电子信息产业股份有限公司 | Thremostated container for detecting computer equipment |
| CN101769825A (en) * | 2008-12-29 | 2010-07-07 | 北京卫星环境工程研究所 | Tracking temperature control device for spacecraft thermal vacuum test |
| US20110126565A1 (en) * | 2009-11-30 | 2011-06-02 | Sanyo Electric Co., Ltd. | Incubator |
| CN102161401A (en) * | 2011-02-16 | 2011-08-24 | 青岛澳柯玛股份有限公司 | Novel thermotank |
| CN201993659U (en) * | 2011-03-25 | 2011-09-28 | 山东兆宇电子技术有限公司 | Water cooling intelligent constant-temperature control case |
| CN102213965A (en) * | 2011-04-13 | 2011-10-12 | 苏州捷美电子有限公司 | Thermostatic equipment and control method thereof |
| CN102811518A (en) * | 2011-06-01 | 2012-12-05 | 建碁股份有限公司 | Method for defogging on glass protective cover and display module thereof |
| CN202738131U (en) * | 2012-06-06 | 2013-02-13 | 北京昆仑纵横科技发展有限公司 | Low-temperature-startup film heating device and apparatus using same |
| CN203444369U (en) * | 2013-08-14 | 2014-02-19 | 北京雪迪龙科技股份有限公司 | Constant temperature apparatus |
| CN104808710A (en) * | 2015-04-25 | 2015-07-29 | 北京航空航天大学 | Unmanned helicopter equipment cabin temperature control system capable of utilizing external airflow |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111874263A (en) * | 2020-07-20 | 2020-11-03 | 上海宇航***工程研究所 | In-situ detector for near-earth space atmospheric environment carried by launch vehicle |
| CN112498652A (en) * | 2021-02-07 | 2021-03-16 | 中国科学院空天信息创新研究院 | Wireless sensor for captive balloon and captive balloon |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105416592B (en) | 2019-01-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100510604C (en) | Cooling system and method for expelling heat from a heat source located in the interior of an aircraft | |
| CN105485834B (en) | A kind of temperature control system of near space sealed compartment | |
| CN203771528U (en) | Intelligent IH water heating stove | |
| US9546799B2 (en) | Solar energy collection system | |
| CN104850153A (en) | Stratospheric airship electronic equipment cabin temperature control system and control method | |
| CN109458662A (en) | A kind of air outlet can send the air conditioner indoor unit of different temperatures | |
| CN105416592A (en) | Onboard incubator and airplane | |
| KR101309917B1 (en) | electric hot blast heater | |
| CN106793686B (en) | A kind of temperature control system and its control method of outdoor cabinet | |
| KR20160011724A (en) | Hybrid plain to complex use of air heat and solar thermal | |
| CN206313095U (en) | A kind of electric vehicle heating system | |
| CN101071003A (en) | Movable solar energy storage heating device | |
| CN108562032A (en) | A kind of radiate unifies end with convection | |
| CN204924499U (en) | Heat pipe thermotank | |
| CN204373126U (en) | Based on the automotive air-conditioning system of cooling piece | |
| CN207377868U (en) | A kind of magnetic-suspension high-speed air blower cooling recirculation system | |
| CN207335261U (en) | A kind of fresh commercial semiconductor insulating box | |
| CN108963130A (en) | A kind of new-energy automobile battery warmer | |
| KR101634502B1 (en) | A air-conditioning system for vehicle | |
| CN104566777A (en) | Semiconductor air conditioning device for fixed-point and orientated temperature control | |
| CN209181089U (en) | A kind of air outlet can send the air conditioner indoor unit of different temperatures | |
| CN208887262U (en) | Vacuum tank equipment | |
| CN203366151U (en) | Testing chamber with shared blower motor for heating channel and refrigeration channel | |
| CN207515041U (en) | Electric heater | |
| CN203934242U (en) | A kind of radar emission shelter that can Fast Heating |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |