CN1900706A - Detector for boron containing lean oxygen propellant heat value - Google Patents
Detector for boron containing lean oxygen propellant heat value Download PDFInfo
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- CN1900706A CN1900706A CN 200610042932 CN200610042932A CN1900706A CN 1900706 A CN1900706 A CN 1900706A CN 200610042932 CN200610042932 CN 200610042932 CN 200610042932 A CN200610042932 A CN 200610042932A CN 1900706 A CN1900706 A CN 1900706A
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Abstract
The disclosed installation for testing heat value of propelling agent containing boron and deficient oxygen is to overcome shortcoming in prior art that propelling agent is unable to burn fully, and part of oxidation bomb is ablated. The invention has following arrangement: using thick walled vessel as body, exhaust valve, electrode, and charge valve installed on head; electrode insulated to the head; ignition thread connected between the charge valve and the electrode, and ignition thread being as wire with known heat value; through ignition thread, sample enwound and hung on the oxidation bomb; sample apart from crucible a certain distance; crucible is on rank; additive for combustion with known heat value in specified mass is placed on the crucible. The said additive for combustion guarantees complete combustion of the propelling agent. Since the propelling agent with high heat value does not burn inside crucible totally so as to reduce ablation degree for crucible.
Description
(1) technical field under
The present invention relates to a kind of calorific value measurement mechanism, especially be applied to the determining instrument of the thermal value of propellant in propellant, coal, petrochemical complex and the power industry, coal, oil or other pyrogen.
(2) background technology
In the prior art field, measure in the instrument of material thermal value and often adopt oxygen bomb calorimeter, the just usually said oxygen bomb in sample combustion chamber wherein, oxygen bomb comprises body 1, bullet 2, venting valve 3, electrode 4, tripod 5, gas admittance valve 6, gas-filled tube 7, burning baffle plate 8, crucible 9.Oxygen enters oxygen bomb by gas admittance valve 6 and gas-filled tube 7, and the gas after the burning is discharged by venting valve 3, insulation between electrode 4 and the bullet 2, and another electrode is by air intake valve 6 and gas-filled tube 7 double as.Sample is placed in the crucible 9, and during test, the energising igniting makes sample fully burning in oxygen-enriched environment.For boron containing lean oxygen propellant, the wherein fusing point of pure boron and boiling point very high (being respectively 2430K and 2823K), the burning of boron is the burning between a kind of solid phase and gas phase media, wants slow many with respect to the burning between gas phase media, and the boron particles surface is coated with because the B that the boron oxidation forms
2O
3, its boiling point higher (about 2133K) if temperature of combustion is not high enough, melts and the B of the thickness that becomes
2O
3Hindered the diffusion of oxygen, caused boron particles ignition hysteresis (difficulty) to boron and liquid oxidatively bed interface.When boron containing lean oxygen propellant burns in crucible, around in the oxygen atmosphere, a large amount of heat is emitted in the rapid burning of metallic addition that at first is gasifiable binder system and low ignition point, the propellant part reaches very high temperature, the metallic addition of the contour burning-point of boron also takes fire simultaneously, rapid burning along with inflammable component in the boron containing lean oxygen propellant, the oxygen bomb calorimeter is as a good heat-exchange system of heat conductivility, heat wherein scatters and disappears rapidly, temperature is reduced to below the 2133K, the B that causes the boron oxidation to generate
2O
3Can not vaporize but be coated on boron surface, hinder the diffusion of oxygen to boron and liquid oxidatively bed interface, make the part of boron can not perfect combustion in the oxygen bomb of existing calorimeter, the burning liberated heat be the heating power of this boron-propellant.Simultaneously, the calorific value of boron containing lean oxygen propellant is very high, more than 30MJ/Kg, and the tenor height, the combustion temperature is high, the parts of oxygen bomb is seriously ablated, especially crucible 9 and tripod 5.
(3) summary of the invention
Can not clean-burning defective in order to overcome in the prior art boron containing lean oxygen propellant, the present invention has adopted a kind of new thermal value measurement device, can effectively ensure the perfect combustion of fuel rich propellant.
The present invention includes body 1, body is a thick-walled vessel; Venting valve 3 is arranged on the bullet 2, electrode 4, gas filling valve 6, electrode 4 and bullet 2 insulation is characterized in that: connect ignition wire 10 between gas filling valve 6 and the electrode 4, ignition wire 10 adopts the tinsel of known calorific value, sample 11 twines by ignition wire 10 and is suspended in the oxygen bomb, and sample leaves the crucible certain distance, and crucible 12 is placed on the tripod 13, tripod 13 is placed on the bottom of oxygen bomb, support crucible 12.Place the combustion adjuvant of the known calorific value of definite quality on the crucible 12.
When the present invention works, apply 12～24V DC voltage between two electrodes, ignition wire energising heating makes the fuel rich propellant ignition, amount of samples is that the ignition of the boron containing lean oxygen propellant of 0.5g～1.5g is at vacant state, concentrate heat release, the slower metallics of combustion speed can not perfect combustion at vacant state; After the burning some time, ignition wire is blown voluntarily, and fuel rich propellant drops on the crucible subsequently, and the combustion adjuvant that ignites is concentrated at combustion adjuvant under the effect of heat release, makes metallics be in hot environment again, is able to perfect combustion.In this process, the fuel rich propellant of the high combustion temperature of high heat value does not directly burn in crucible, but combustion adjuvant burns in crucible, and the combustion temperature of combustion adjuvant is 2000～3000K, well below the combustion temperature of fuel rich propellant, crucible ablation degree is reduced greatly.Crucible holder does not directly contact with flame, and obtain certain protection by crucible, has overcome the serious problem of oxygen bomb parts ablation.
As a preferred version of the present invention, described oxygen bomb also can not adopt crucible 12 and crucible holder 13, and combustion adjuvant directly is placed on the bottom of oxygen bomb, suitably strengthens the consumption of combustion adjuvant.Apply after the ignition signal, the ignition wire testing sample that ignites, ignition wire is blown voluntarily, and fuel rich propellant drops to the bottom, firing chamber subsequently, the combustion adjuvant burning.The ignition of fuel rich propellant is at vacant state, concentrate heat release, the slower metallics of combustion speed can not perfect combustion at vacant state, under the effect of gravity, fall in the combustion adjuvant of its below, the combustion adjuvant that ignites is concentrated at combustion adjuvant under the effect of heat release, make metallics be in hot environment again, be able to perfect combustion.Owing to do not use crucible 10 and crucible holder 11, therefore do not have the ablation problem of crucible and support thereof.
As another preferred version of the present invention, the distance that described sample leaves crucible is not less than 10mm.
As the 3rd preferred version of the present invention, described combustion adjuvant can be selected Ledate-2 propellant for use, and its calorific value is 11.2MJ/kg; Also can select modified double base propellant 171-25 for use, calorific value is 10.9MJ/kg.Combustion adjuvant should have certain shape, is 10mm such as external diameter, is the propellant charge of 5mm highly, and should is not Powdered, can ensure combustion adjuvant like this in the regular hour internal combustion, rather than all burns down moment.
As the 4th preferred version of the present invention, described crucible 12 is the carbon/carbon compound material of adiabatic anti-ablation, also can select the tungsten crucible of molding sintering.
As the 5th preferred version of the present invention, described tripod 13 encircles crucible holder up and down for heat-resistant anticorrosive erosion NI-CR-MO alloys steel.
The present invention has ensured the perfect combustion of fuel rich propellant by the combustion adjuvant on the crucible, because the fuel rich propellant of high heat value does not burn fully, has reduced the ablation degree to crucible simultaneously in crucible.The present invention is simple in structure, and is stable and reliable for performance, is with a wide range of applications.
(4) description of drawings
Fig. 1 is the oxygen bomb structural drawing of the oxygen bomb calorimeter of prior art
Fig. 2 is a sample ignition device structural drawing of the present invention
Fig. 3 is the oxygen bomb structural drawing of oxygen bomb calorimeter of the present invention
(5) embodiment
Fig. 2 and Fig. 3 have showed application example of the present invention.
Example 1: the present invention has adopted a kind of new thermal value measurement device, comprises body 1, and body is that volume is 300 milliliters a thick cyclinder; Venting valve 3 is arranged on the bullet 2, electrode 4, gas filling valve 6, electrode 4 and bullet 2 insulation connect ignition wire 10 between gas filling valve 6 and the electrode 4, and ignition wire is the nichrome wire of diameter 0.1mm, and calorific value is 3.2J/cm.Sample 11 is the boron containing lean oxygen propellant of 1.0g, be suspended in the oxygen bomb by ignition wire 10 windings, the distance that sample leaves crucible is 15mm, crucible 12 is placed on the tripod 13, crucible 12 is the carbon/carbon compound material of adiabatic anti-ablation, tripod 13 is placed on the bottom of oxygen bomb, support crucible for heat-resistant anticorrosive erosion NI-CR-MO alloys steel encircles crucible holder up and down.Place the combustion adjuvant of the known calorific value of definite quality on the crucible 12, combustion adjuvant is that external diameter is 10mm, highly is Ledate-2 propellant of 5.0mm, and its calorific value is 11.2MJ/kg.With the calorific value of oxygen bomb specimen shown in Figure 3, crucible and tripod do not have ablation phenomen, and recording the sample calorific value is 29.85MJ/Kg, and burning condensed phase product is white powder and a small amount of brown sinter.
Example 2: the present invention includes body 1, body is that volume is 300 milliliters a thick cyclinder; Venting valve 3 is arranged on the bullet 2, electrode 4, gas filling valve 6, electrode 4 and bullet 2 insulation connect ignition wire 10 between gas filling valve 6 and the electrode 4, and ignition wire is the nichrome wire of diameter 0.1mm, and calorific value is 3.2J/cm.Sample 11 is the boron containing lean oxygen propellant of 0.5g, twines by ignition wire 10 to be suspended in the oxygen bomb, and the distance of leaving the oxygen bomb bottom is 60mm, and the bottom combustion adjuvant that is placed on oxygen bomb is Ledate-2 propellant, and its diameter is 50mm, highly is 1.5mm.With not with the calorific value of the oxygen bomb specimen of crucible and crucible holder, recording the sample calorific value is 29.89MJ/Kg, and products of combustion is white powder and a small amount of brown sinter.
Concrete implementation step of the present invention:
1, through calculating, the theoretical calorific value of boron containing lean oxygen propellant is about 30MJ/kg, if the GR3500 type oxygen bomb calorimeter that adopts Bente Instrument Co., Ltd., Changsha to produce, then according to demarcation, its water equivalent is 15000J/K, therefore, gets a certain amount of boron containing lean oxygen propellant (being sample 11 in the accompanying drawing 3), be cut into strip and block (generally to be cut into little cube of bulk), put it into accurately weighing on the analytical balance.
2, measure the ignition wire 10 of 25 centimetres of known calorific values,, the ignition wire hoop is twined in the embedding crack,, also be convenient to improve the igniting reliability so that hang reliably at bulk propellant surface hoop delineation to be measured 3-4 road crack.Again ignition wire two is terminated on the spark electrode in the oxygen bomb head.
3, the quality of weighing combustion adjuvant is put into crucible 12, crucible is placed on the crucible holder 13 again, and the two is put into oxygen bomb.
4, behind the assembling oxygen bomb, charge into the oxygen of about 1.2MPa.
5, on the basis of the experimental apparatus system being regulated, load onto Beckman thermometer.Before Beckman thermometer is installed, need its measurement range is regulated.Can make system temperature about 2 degree that raise by the propellant of the first step about can approximate evaluation 1g, therefore, the measurement range of Beckman thermometer should be able to satisfy the demand of measurement.Observe the initial reading of Beckman thermometer, spend 1 with reading--be advisable between-2 degree, just need to regulate if be higher than 2.5 degree or be lower than 0.5 degree centigrade.
5, oxygen bomb is put into bucket, the igniting signal wire is installed, open the control box power supply, stirrer and Vib. are started working.
6, opening entry initial stage temperature variation, after the system for the treatment of reaches balance, apply ignition signal, ignition wire is lighted sample rapidly, and ignition wire is blown voluntarily, and sample is after losing suspension force, in burning, fall in the crucible below it, the combustion adjuvant that ignites, the heat that the combustion adjuvant burning discharges has ensured that the temperature in the oxygen bomb is on the combustion temperature of sample, has also promptly guaranteed the perfect combustion of sample.Write down main phase temperature variation simultaneously, be recorded to system temperature before no longer rising and beginning to descend till.Then opening entry temperature variation in latter stage, a general record 10---15 data.Experiment finishes, closing control case power supply.
7, take out oxygen bomb, open vent valve and emit waste gas.Open oxygen bomb, observation oxygen bomb inside is attached with a large amount of white powders on the inwall of discovery oxygen bomb, and the brown sinter that also has minute quantity except that white powder is gone up in crucible (example 1) or oxygen bomb bottom (example 2), oxygen bomb interior crucible, crucible holder stand intact no ablation phenomen.Take off the residue ignition wire, measure and record residue igniting filament length degree.The condensed phase products of combustion be the analysis showed that: white powder is B
2O
3With the potpourri of MgO, the brown sinter is the oxide of boric acid and iron, does not find the existence of pure boron.Difficulty combustion metal perfect combustion in the boron containing lean oxygen propellant has been described, has solved the problem in the test of boron containing lean oxygen propellant heating power.
8, clean oxygen bomb, and carry out titration.
9, the processing of experimental data adopts universal method to carry out data processing.Obtain the calorific value of boron containing lean oxygen propellant.
Claims (6)
1, detector for boron containing lean oxygen propellant heat value comprises body (1), and body is a thick-walled vessel; Venting valve (3) is arranged on the bullet (2), electrode (4), gas filling valve (6), electrode (4) and bullet (2) insulation, it is characterized in that: connect ignition wire (10) between gas filling valve (6) and the electrode (4), ignition wire (10) adopts the tinsel of known calorific value, sample (11) twines by ignition wire (10) and is suspended in the oxygen bomb, sample leaves the crucible certain distance, crucible (12) is placed on the tripod (13), tripod (13) is placed on the bottom of oxygen bomb, support crucible (12), and crucible (12) is gone up the combustion adjuvant of the known calorific value of placing definite quality.
2, according to the detector for boron containing lean oxygen propellant heat value of claim 1, it is characterized in that: described oxygen bomb also can not adopt crucible (12) and crucible holder (13), and combustion adjuvant directly is placed on the bottom of oxygen bomb, suitably strengthens the consumption of combustion adjuvant.
3, according to the detector for boron containing lean oxygen propellant heat value of claim 1, it is characterized in that: the distance that described sample leaves crucible is not less than 10mm.
4, according to the detector for boron containing lean oxygen propellant heat value of claim 1 or 2, it is characterized in that: described combustion adjuvant can be selected Ledate-2 propellant for use, and its calorific value is 11.2MJ/kg; Also can select modified double base propellant 171-25 for use, calorific value is 10.9MJ/kg, and combustion adjuvant has certain shape.
5, according to the detector for boron containing lean oxygen propellant heat value of claim 1, it is characterized in that: described crucible (12) is the carbon/carbon compound material of adiabatic anti-ablation, also can select the tungsten crucible of molding sintering.
6, according to the detector for boron containing lean oxygen propellant heat value of claim 1, it is characterized in that: described tripod (13) encircles crucible holder up and down for heat-resistant anticorrosive erosion NI-CR-MO alloys steel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006100429328A CN100501391C (en) | 2006-06-07 | 2006-06-07 | Detector for boron containing lean oxygen propellant heat value |
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|---|---|---|---|
| CNB2006100429328A CN100501391C (en) | 2006-06-07 | 2006-06-07 | Detector for boron containing lean oxygen propellant heat value |
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| CN1900706A true CN1900706A (en) | 2007-01-24 |
| CN100501391C CN100501391C (en) | 2009-06-17 |
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Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102004119A (en) * | 2010-11-04 | 2011-04-06 | 西北工业大学 | Method for measuring combustion heat value of boron powder |
| CN102252344A (en) * | 2011-04-29 | 2011-11-23 | 安徽工业大学 | Novel ignition temperature measuring device for experiment |
| CN102866175A (en) * | 2012-09-10 | 2013-01-09 | 浙江大学 | Boron particle burning observing device for realizing ignition by utilizing high-pressure xenon lamp |
| CN104155341A (en) * | 2014-08-08 | 2014-11-19 | 西北工业大学 | Boron powder combustion heat value testing device |
| CN104995507A (en) * | 2013-02-19 | 2015-10-21 | 大陆汽车有限责任公司 | Device for ascertaining a measure of a calorific value of a gas |
| CN107247074A (en) * | 2017-06-20 | 2017-10-13 | 江苏和顺环保有限公司 | The assay method of low heat value industry dangerous waste combustion heat value |
| CN108278444A (en) * | 2018-04-25 | 2018-07-13 | 工业和信息化部电子第五研究所华东分所 | A kind of titration cup adiabatic apparatus |
| CN110988021A (en) * | 2019-11-19 | 2020-04-10 | 中国农业科学院农产品加工研究所 | Heat value detection sample loading device and food self-heating bag detection method |
| CN111610226A (en) * | 2020-05-29 | 2020-09-01 | 西北工业大学 | Preparation process of boron powder heat value test sample |
| CN112010721A (en) * | 2020-08-06 | 2020-12-01 | 西安近代化学研究所 | Boron-containing fuel-rich propellant and preparation method thereof |
| CN112326712A (en) * | 2020-09-29 | 2021-02-05 | 华能莱芜发电有限公司 | Method for detecting heat productivity of sludge |
| CN112683945A (en) * | 2020-12-22 | 2021-04-20 | 内蒙合成化工研究所 | Novel method for testing combustion heat of high-metal-content structural material |
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2006
- 2006-06-07 CN CNB2006100429328A patent/CN100501391C/en not_active Expired - Fee Related
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102004119A (en) * | 2010-11-04 | 2011-04-06 | 西北工业大学 | Method for measuring combustion heat value of boron powder |
| CN102004119B (en) * | 2010-11-04 | 2012-10-24 | 西北工业大学 | Method for measuring combustion heat value of boron powder |
| CN102252344A (en) * | 2011-04-29 | 2011-11-23 | 安徽工业大学 | Novel ignition temperature measuring device for experiment |
| CN102252344B (en) * | 2011-04-29 | 2013-12-11 | 安徽工业大学 | Novel ignition temperature measuring device for experiment |
| CN102866175A (en) * | 2012-09-10 | 2013-01-09 | 浙江大学 | Boron particle burning observing device for realizing ignition by utilizing high-pressure xenon lamp |
| CN104995507A (en) * | 2013-02-19 | 2015-10-21 | 大陆汽车有限责任公司 | Device for ascertaining a measure of a calorific value of a gas |
| CN104995507B (en) * | 2013-02-19 | 2016-11-30 | 大陆汽车有限责任公司 | For determining the apparatus and method of the value of gas combustion value |
| CN104155341A (en) * | 2014-08-08 | 2014-11-19 | 西北工业大学 | Boron powder combustion heat value testing device |
| CN107247074A (en) * | 2017-06-20 | 2017-10-13 | 江苏和顺环保有限公司 | The assay method of low heat value industry dangerous waste combustion heat value |
| CN108278444A (en) * | 2018-04-25 | 2018-07-13 | 工业和信息化部电子第五研究所华东分所 | A kind of titration cup adiabatic apparatus |
| CN108278444B (en) * | 2018-04-25 | 2023-08-11 | 工业和信息化部电子第五研究所华东分所 | Titration cup heat insulation device |
| CN110988021A (en) * | 2019-11-19 | 2020-04-10 | 中国农业科学院农产品加工研究所 | Heat value detection sample loading device and food self-heating bag detection method |
| CN110988021B (en) * | 2019-11-19 | 2022-07-08 | 中国农业科学院农产品加工研究所 | Heat value detection sample loading device and food self-heating bag detection method |
| CN111610226A (en) * | 2020-05-29 | 2020-09-01 | 西北工业大学 | Preparation process of boron powder heat value test sample |
| CN112010721A (en) * | 2020-08-06 | 2020-12-01 | 西安近代化学研究所 | Boron-containing fuel-rich propellant and preparation method thereof |
| CN112326712A (en) * | 2020-09-29 | 2021-02-05 | 华能莱芜发电有限公司 | Method for detecting heat productivity of sludge |
| CN112683945A (en) * | 2020-12-22 | 2021-04-20 | 内蒙合成化工研究所 | Novel method for testing combustion heat of high-metal-content structural material |
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|---|---|
| CN100501391C (en) | 2009-06-17 |
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Correction item: Inventor Correct: Wang Yinghong|Zhang Xiaohong|Hu Chunbo|Wang Hong|Sun Zhihua|Feng Xiping False: Wang Yinghong|Hu Chunbo|Feng Xiping Number: 24 Page: 1657 Volume: 25 |
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Correction item: Inventor Correct: Wang Yinghong|Zhang Xiaohong|Hu Chunbo|Wang Hong|Sun Zhihua|Feng Xiping False: Wang Yinghong|Hu Chunbo|Feng Xiping Number: 24 Page: The title page Volume: 25 |
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Free format text: CORRECT: INVENTOR; FROM: WANG YINGHONG HU CHUNBO FENG XIPING - TO: WANG YINGHONG ZHANG XIAOHONG HU CHUNBO WANG HONG SUN ZHIHUA FENG XIPING - |
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Granted publication date: 20090617 Termination date: 20130607 |