CN1465957A - High temp. resisting thermal-insulating method for data recording instrument - Google Patents

High temp. resisting thermal-insulating method for data recording instrument Download PDF

Info

Publication number
CN1465957A
CN1465957A CNA021215669A CN02121566A CN1465957A CN 1465957 A CN1465957 A CN 1465957A CN A021215669 A CNA021215669 A CN A021215669A CN 02121566 A CN02121566 A CN 02121566A CN 1465957 A CN1465957 A CN 1465957A
Authority
CN
China
Prior art keywords
layer
heat
datalogger
vaporization cooling
insulation
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
CNA021215669A
Other languages
Chinese (zh)
Inventor
刘日新
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CNA021215669A priority Critical patent/CN1465957A/en
Publication of CN1465957A publication Critical patent/CN1465957A/en
Pending legal-status Critical Current

Links

Landscapes

  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

The invention belongs to the field of instrument, providing an adiabatic structure able to make the recorder's data normally work under the high-temperature and adverse circumstances. It adopts multilayer heat-insulating structure outside the data recorder, which can continually work for 18 hours under 100-1650 deg.c.

Description

The high temperature resistant insulation method of a kind of datalogger
The invention belongs to instrument field.
In ship's navigation, need the various aeronautical datas of record, when occurring as various accidents such as fire, boats and ships require the data in the registering instrument intact, so that culprit is analyzed according to the data of preserving in the registering instrument.
The purpose of this invention is to provide the data registering instrument is incubated adiabatic a kind of method, be characterized in datalogger externally temperature can be 100~1650 ℃, the duration can reach 18 hours.Data are excellent in the registering instrument.
The gordian technique that the present invention takes is that the outside MULTILAYER COMPOSITE heat insulating construction that adopts of datalogger carries out thermal insulation.Fig. 1 is the heat insulating construction synoptic diagram.Datalogger (1) is placed on the center of whole instrument, and the innermost layer of heat insulating construction is single or multiple lift vacuum heat-insulating layer (2), and vacuum tightness is 10 -3~10 -7Pa, vaporization cooling sandwith layer (3) guarantees that the temperature of vacuum layer outside is not higher than the boiling point of the cooling medium of vaporizing, cooling medium adopts water.Liquid coolant is added by cooling medium heating gate (5), and the steam of cooling medium is also discharged from (5), becomes solid-stately after water adds, and also can not discharge from adding inlet in the ship motion process.Outer for individual layer or become refractory masses (4) more, forms by refractory fibre or other fire resistive material, low temperature time is used glass wool, under the high temperature with the heat-insulating material of alumina silicate or mullite material, like this can heatproof, can obtain good insulation effect again.External application steel shell (6) encapsulation.
The present invention is when externally temperature is 100~1650 ℃, and the duration can reach 18 hours.
Fig. 1 is a datalogger heat insulating construction synoptic diagram
1 datalogger, 2 vacuum heat-insulating layers, 3 vaporization cooling jackets, 4 fire resistive material heat insulation layers, 5 chilled waters add inlet/steam outlet 6 shells.
The a certain example of the present invention is: overall dimensions are external diameter 300mm, high 450mm, are lower than 75 ℃ in the temperature of 260 ℃ ten hours, 1100 ℃ internal record instrument after a hour.

Claims (4)

1. the composite heat preserving and thermal insulating method of a datalogger can make continuous operate as normal of datalogger or data preserve under 100~1650 ℃ temperature and reach 18 hours.It is characterized in that carrying out adiabatic heat-insulation at the outside multiple layer heat insulation structure that adopts of datalogger.Nexine is vacuum heat-insulating layer or vacuum multilayer insulation layer, and middle is the vaporization cooling layer, and the vaporization cooling medium is solidificated in the vaporization cooling sandwith layer, also can not overflow when shaking appears in registering instrument.Skin is the fire resistive material thermal insulating warm-keeping layer.
2. as claims 1 described datalogger complex heat-preservation method, adiabatic nexine is the single or multiple lift vacuum heat-insulating layer.
3. as claims 1 described datalogger complex heat-preservation method, the vaporization cooling jacket adopts water or other coolant cools, liquid other cooling medium of water also can be solidificated in the vaporization cooling sandwith layer, and water or other cooling medium can not overflow yet when registering instrument vibration or rotation and after being heated to 100 ℃.
4. as claims 1 described datalogger complex heat-preservation method, the single or multiple lift composite adiabatic layer that the secondary insulation layer is made up of fire resistive material.Both high temperature resistant, good insulation effect is arranged again.
CNA021215669A 2002-06-26 2002-06-26 High temp. resisting thermal-insulating method for data recording instrument Pending CN1465957A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNA021215669A CN1465957A (en) 2002-06-26 2002-06-26 High temp. resisting thermal-insulating method for data recording instrument

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNA021215669A CN1465957A (en) 2002-06-26 2002-06-26 High temp. resisting thermal-insulating method for data recording instrument

Publications (1)

Publication Number Publication Date
CN1465957A true CN1465957A (en) 2004-01-07

Family

ID=34142203

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA021215669A Pending CN1465957A (en) 2002-06-26 2002-06-26 High temp. resisting thermal-insulating method for data recording instrument

Country Status (1)

Country Link
CN (1) CN1465957A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102222372A (en) * 2010-04-13 2011-10-19 塔莱斯公司 Movable device for recording flight data
CN102261963A (en) * 2011-04-29 2011-11-30 上海宝钢工业检测公司 Thermal detection tracking device for high-temperature object
CN103108516A (en) * 2012-12-24 2013-05-15 江苏海兰船舶电气系统科技有限公司 Marine data protective unit heat insulation barrel
CN105080000A (en) * 2015-09-01 2015-11-25 启东晋盛大公化工有限公司 Data protection unit for ship
CN105079995A (en) * 2015-09-01 2015-11-25 上海康霆机电有限公司启东二公司 Data protection device
CN105107107A (en) * 2015-09-01 2015-12-02 启东晋盛大公化工有限公司 Data protector
CN105126273A (en) * 2015-09-01 2015-12-09 上海康霆机电有限公司启东二公司 Electronic data protection unit
CN111114045A (en) * 2019-12-17 2020-05-08 辽宁省轻工科学研究院有限公司 Vehicle-mounted data protection device and preparation method thereof
WO2022056714A1 (en) * 2020-09-16 2022-03-24 上海三利数字技术有限公司 Data disaster recovery storage device and vehicle
CN114373486A (en) * 2021-12-17 2022-04-19 天津爱玛车业科技有限公司 Thermal protection device

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102222372A (en) * 2010-04-13 2011-10-19 塔莱斯公司 Movable device for recording flight data
CN102222372B (en) * 2010-04-13 2016-10-05 塔莱斯公司 Movable equipment for record flight data
CN102261963A (en) * 2011-04-29 2011-11-30 上海宝钢工业检测公司 Thermal detection tracking device for high-temperature object
CN103108516A (en) * 2012-12-24 2013-05-15 江苏海兰船舶电气系统科技有限公司 Marine data protective unit heat insulation barrel
CN103108516B (en) * 2012-12-24 2016-07-06 江苏海兰船舶电气系统科技有限公司 Marine data protective unit heat insulation barrel
CN105126273A (en) * 2015-09-01 2015-12-09 上海康霆机电有限公司启东二公司 Electronic data protection unit
CN105107107A (en) * 2015-09-01 2015-12-02 启东晋盛大公化工有限公司 Data protector
CN105079995A (en) * 2015-09-01 2015-11-25 上海康霆机电有限公司启东二公司 Data protection device
CN105080000A (en) * 2015-09-01 2015-11-25 启东晋盛大公化工有限公司 Data protection unit for ship
CN111114045A (en) * 2019-12-17 2020-05-08 辽宁省轻工科学研究院有限公司 Vehicle-mounted data protection device and preparation method thereof
WO2022056714A1 (en) * 2020-09-16 2022-03-24 上海三利数字技术有限公司 Data disaster recovery storage device and vehicle
CN114373486A (en) * 2021-12-17 2022-04-19 天津爱玛车业科技有限公司 Thermal protection device
CN114373486B (en) * 2021-12-17 2023-10-20 天津爱玛车业科技有限公司 Heat protection device

Similar Documents

Publication Publication Date Title
US4813632A (en) Ballast management system for lighter than air craft
CN1465957A (en) High temp. resisting thermal-insulating method for data recording instrument
RU2009105501A (en) THERMAL ENERGY FLOW DEVICE
CN105570614B (en) A kind of high-temperature vacuum heat insulation composite material of internal addition infrared reflecting layer
TW200620330A (en) Super-conducting cable circuit
US9853301B2 (en) Thermal conditioning fluids for an underwater cryogenic storage vessel
CN2579800Y (en) High temperature insulation structure for data recorder for ship
Nast et al. Development of gas gap cryogenic thermal switch
JP4677313B2 (en) Cryostat for magnetic field generator
SU932094A1 (en) Cryogenic liquid evaporator
RU2763917C1 (en) Apparatus for heat protection of an aircraft
CN2570754Y (en) High-temperature resistant intelligent temperature recorder
US3376918A (en) Cooling of turbine blades
USH140H (en) Carbon/carbon combustor external insulation
CN2570756Y (en) High-temperature resistant intelligent temperature recorder
SU875178A1 (en) Heat insulation structure for pipelines
JPS5311482A (en) Liquefied gas carrying vessel
CN112963649A (en) Anti-icing and heat-preserving design method for airplane water supply pipeline
RU2269170C1 (en) Device for thermal and mechanical protection of object
Kasagi et al. Effects of the wall curvature on the full-coverage film cooling effectiveness
RU2269168C1 (en) Protective device
JPH1077952A (en) Extraction method of magma energy
Godefroy et al. Thin film and high temperature thermal sensors deposited by RF cathodic sputtering
RU43712U1 (en) MICROELECTRON RECORDER PROTECTION DEVICE
RU2269166C1 (en) Device for thermal and mechanical protection of object

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication