CN106833762A - A kind of low freezing point fuel and preparation method thereof - Google Patents
A kind of low freezing point fuel and preparation method thereof Download PDFInfo
- Publication number
- CN106833762A CN106833762A CN201611256823.6A CN201611256823A CN106833762A CN 106833762 A CN106833762 A CN 106833762A CN 201611256823 A CN201611256823 A CN 201611256823A CN 106833762 A CN106833762 A CN 106833762A
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- Prior art keywords
- freezing point
- liquid
- low freezing
- point fuel
- hydrogen peroxide
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Links
- 230000008014 freezing Effects 0.000 title claims abstract description 45
- 238000007710 freezing Methods 0.000 title claims abstract description 45
- 239000000446 fuel Substances 0.000 title claims abstract description 39
- 238000002360 preparation method Methods 0.000 title claims abstract description 15
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 claims abstract description 59
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000007788 liquid Substances 0.000 claims abstract description 25
- 238000003756 stirring Methods 0.000 claims abstract description 14
- FEWJPZIEWOKRBE-UHFFFAOYSA-N Tartaric acid Natural products [H+].[H+].[O-]C(=O)C(O)C(O)C([O-])=O FEWJPZIEWOKRBE-UHFFFAOYSA-N 0.000 claims abstract description 11
- 229960003540 oxyquinoline Drugs 0.000 claims abstract description 11
- MCJGNVYPOGVAJF-UHFFFAOYSA-N quinolin-8-ol Chemical compound C1=CN=C2C(O)=CC=CC2=C1 MCJGNVYPOGVAJF-UHFFFAOYSA-N 0.000 claims abstract description 11
- 235000002906 tartaric acid Nutrition 0.000 claims abstract description 11
- 239000011975 tartaric acid Substances 0.000 claims abstract description 11
- 238000002156 mixing Methods 0.000 claims abstract description 9
- 238000000034 method Methods 0.000 claims abstract description 7
- 239000005725 8-Hydroxyquinoline Substances 0.000 claims description 10
- 230000008569 process Effects 0.000 claims description 6
- 230000008901 benefit Effects 0.000 abstract description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 3
- 229910052799 carbon Inorganic materials 0.000 abstract description 3
- 238000004140 cleaning Methods 0.000 abstract description 3
- 238000009826 distribution Methods 0.000 abstract description 3
- 239000002920 hazardous waste Substances 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 239000000567 combustion gas Substances 0.000 abstract description 2
- 239000003380 propellant Substances 0.000 description 5
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 229910052739 hydrogen Inorganic materials 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 4
- 239000007800 oxidant agent Substances 0.000 description 4
- FEWJPZIEWOKRBE-JCYAYHJZSA-N Dextrotartaric acid Chemical compound OC(=O)[C@H](O)[C@@H](O)C(O)=O FEWJPZIEWOKRBE-JCYAYHJZSA-N 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- WFPZPJSADLPSON-UHFFFAOYSA-N dinitrogen tetraoxide Chemical compound [O-][N+](=O)[N+]([O-])=O WFPZPJSADLPSON-UHFFFAOYSA-N 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 231100000252 nontoxic Toxicity 0.000 description 2
- 230000003000 nontoxic effect Effects 0.000 description 2
- -1 peroxide hydrogen Chemical class 0.000 description 2
- 239000003381 stabilizer Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 150000002978 peroxides Chemical class 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 230000001988 toxicity Effects 0.000 description 1
- 231100000419 toxicity Toxicity 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L1/00—Liquid carbonaceous fuels
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L1/00—Liquid carbonaceous fuels
- C10L1/02—Liquid carbonaceous fuels essentially based on components consisting of carbon, hydrogen, and oxygen only
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L1/00—Liquid carbonaceous fuels
- C10L1/10—Liquid carbonaceous fuels containing additives
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L10/00—Use of additives to fuels or fires for particular purposes
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L1/00—Liquid carbonaceous fuels
- C10L1/10—Liquid carbonaceous fuels containing additives
- C10L1/14—Organic compounds
- C10L1/18—Organic compounds containing oxygen
- C10L1/182—Organic compounds containing oxygen containing hydroxy groups; Salts thereof
- C10L1/183—Organic compounds containing oxygen containing hydroxy groups; Salts thereof at least one hydroxy group bound to an aromatic carbon atom
- C10L1/1837—Organic compounds containing oxygen containing hydroxy groups; Salts thereof at least one hydroxy group bound to an aromatic carbon atom hydroxy attached to a condensed aromatic ring system
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L1/00—Liquid carbonaceous fuels
- C10L1/10—Liquid carbonaceous fuels containing additives
- C10L1/14—Organic compounds
- C10L1/18—Organic compounds containing oxygen
- C10L1/188—Carboxylic acids; metal salts thereof
- C10L1/1881—Carboxylic acids; metal salts thereof carboxylic group attached to an aliphatic carbon atom
Landscapes
- Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Liquid Carbonaceous Fuels (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Abstract
The present invention relates to a kind of low freezing point fuel and preparation method thereof, the low freezing point fuel includes the component of following weight portion content：Hydrogen peroxide 60~95, ethanol 40~5, the oxyquinoline 0.01~0.2 of tartaric acid 0.01~0.2,8；The said goods are prepared by the following method and form：During tartaric acid added into hydrogen peroxide, and stir, obtain first liquid；During 8 oxyquinolines are added into ethanol, and stir, obtain second liquid.Again by first liquid and second liquid mixing and stirring, that is, obtain purpose product.Compared with prior art, there is the present invention low temperature not freeze, and low temperature adaptability is good, and good stability, corrosivity is small, combustion gas cleaning non-scaling, not carbon distribution, the advantages of production process is generated without hazardous waste.
Description
Technical field
The present invention relates to a kind of fuel, more particularly, to a kind of low freezing point fuel and preparation method thereof.
Background technology
The usage history of hydrogen peroxide is alreadyd exceed more than 100 years, and it is obtained extremely in industrial circles such as Aero-Space, national defence
It is widely applied.Militarily it is initially paid attention to and is developed due to being applied to rocketry and national defence weapon, particularly
During the Second World War and the cold war initial stage.With carrying space expense, propellant for a long time can depot, security, nontoxic pollution-free, can
Reuse, rapid fire etc. require more and more higher, and high-strength hydrogen peroxide receives more and more wider again in propulsion field
General concern.
At present, hydrogen peroxide Push Technology is widely studied in Deng Guoge mechanisms of American and Britain, such as：NASA, USAF,
Boeing, Aerojet, railway technology company, Orbital Sciences Corporation, Purdue University, Surrey satellite technologies company etc..And, fire
One of developing direction of arrow propulsion field propellant is to reduce hydrazine, the use of dinitrogen tetroxide, so hydrogen peroxide would is that mesh
One of preceding and propulsion field in the future research and development emphasis.
Hydrogen peroxide have high density specific impulse, environmental protection, normal temperature can store, easy-to-operate, can single group unit decompose
With can spontaneous combustion the advantages of, be highly suitable as the propellant of modern rocket engine.Hydrogen peroxide has as liquid propellant
Following significant good characteristic：
(1) it is nontoxic, pollution-free.
(2) can for a long time be stored under the normal temperature condition in ground or space.
(3) density and density ratio are leapt high.
(4) oxidant of bipropellant is can not only be used for, again can be as SP.
(5) good hot physical property.
(6) multipurpose.
But the freezing point of hydrogen peroxide propellant, such as 85% hydrogen peroxide are -15 DEG C, 95% hydrogen peroxide is -5 DEG C, is held
The inferior position for easily freezing limits extensive use, takes Insulation to increased system weight and complexity, use environment temperature
It is required that making its advantage to be embodied.
The content of the invention
The purpose of the present invention is exactly to provide a kind of with low-temperature adaptation for the defect for overcoming above-mentioned prior art to exist
Property it is good, corrosivity is small, combustion gas cleaning non-scaling, not carbon distribution, low freezing point combustion the advantages of production process is generated without hazardous waste
Material and preparation method thereof, the fuel can be applied to aero-engine, airspace engine, vehicle, robot, gas generating unit,
Energy generating apparatus, carbon dioxide generating device and other extraordinary power-equipments.
The purpose of the present invention can be achieved through the following technical solutions：
A kind of low freezing point fuel, including following weight portion content component：
Each component is reagent grade materials.
Preferably, its freezing point is -60~-10 DEG C.
Preferably, the low freezing point fuel includes the component of following weight portion content：
Preferably, its freezing point is -60~-50 DEG C.
The preparation method of the low freezing point fuel, comprises the following steps：
(1) in tartaric acid being added into hydrogen peroxide by proportioning, and stir, obtain first liquid；
(2) in 8-hydroxyquinoline being added into ethanol by proportioning, and stir, obtain second liquid；
(3) first liquid and second liquid are mixed and stirred for uniformly obtaining described low freezing point fuel.
Preferably, rotating speed is 60~4000 revs/min in each step whipping process, and mixing time is 60~200 minutes, temperature
Degree control is at -20 DEG C~50 DEG C.
The present invention reduces peroxidating by adding the relatively low ethanol of freezing point (freezing point is less than -100 DEG C) in hydrogen peroxide
The freezing point of hydrogen, ethanol is cheap and easy to get, is dissolved each other with hydrogen peroxide, can effectively reduce its freezing point so that the freezing point of hydrogen peroxide compared with
It is adjustable in big scope, while ethanol can also be good as fuel, fuel oxidizer mixing compatibility, comprising double elements and list
Constituent element fuel advantage.
Because hydrogen peroxide has oxidisability, store and during spacecraft use, external environment is changeful, peroxide
Change hydrogen unstable, easily decompose, a small amount of tartaric acid and 8-hydroxyquinoline carry out stable peroxide hydrogen, prevented as stabilizer
The decomposition of hydrogen oxide., by complex reaction come stable peroxide hydrogen, tartaric acid is a kind of good for tartaric acid and 8-hydroxyquinoline
Stabilizer of hydrogen peroxide, while in acidity, which increasing the meltage of 8-hydroxyquinoline.In preparation process, respectively by tartaric acid
In addition hydrogen peroxide, and by 8-hydroxyquinoline addition ethanol, the compatibility between material is make use of, make to be not easy directly
The 8-hydroxyquinoline being dissolved in hydrogen peroxide is by being first dissolved in ethanol, then mixes with hydrogen peroxide, is allowed to be dissolved in body
In system.
Compared with prior art, the invention has the advantages that：
(1) low freezing point：As a result of the proportioning of science, the freezing point of the fuel product drops than the freezing point of single hydrogen peroxide
It is low 5~20 DEG C, -60~-10 DEG C are reached, can normally use at low ambient conditions.
(2) good stability, can for a long time preserve the fuel product at ambient temperature.
(3) fuel small toxicity of the invention, corrosivity are small, environmental protection, product cleaning non-scaling, not carbon distribution, production after burning
Process is generated without hazardous waste.
(4) fuel oxidizer mixing compatibility is good, comprising double elements and monoreactant chemical advantage.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.
Embodiment 1
A kind of low freezing point fuel, including following weight portion content component：
The preparation method of the low freezing point fuel, comprises the following steps：
(1) in tartaric acid being added into hydrogen peroxide by proportioning, and stir, obtain first liquid；
(2) in 8-hydroxyquinoline being added into ethanol by proportioning, and stir, obtain second liquid；
(3) first liquid and second liquid are mixed and stirred for uniformly obtaining described low freezing point fuel.
Rotating speed is 60~4000 revs/min in each step whipping process, and mixing time is 60~200 minutes, is controlled normal
Carried out under temperature.
Embodiment 2
A kind of low freezing point fuel, including following weight portion content component：
The preparation method of the low freezing point fuel, comprises the following steps：
(1) in tartaric acid being added into hydrogen peroxide by proportioning, and stir, obtain first liquid；
(2) in 8-hydroxyquinoline being added into ethanol by proportioning, and stir, obtain second liquid；
(3) first liquid and second liquid are mixed and stirred for uniformly obtaining described low freezing point fuel.
Rotating speed is 60~4000 revs/min in each step whipping process, and mixing time is 60~200 minutes, is controlled normal
Carried out under temperature.
Embodiment 3
A kind of low freezing point fuel, including following weight portion content component：
The preparation method of the low freezing point fuel, comprises the following steps：
(1) in tartaric acid being added into hydrogen peroxide by proportioning, and stir, obtain first liquid；
(2) in 8-hydroxyquinoline being added into ethanol by proportioning, and stir, obtain second liquid；
(3) first liquid and second liquid are mixed and stirred for uniformly obtaining described low freezing point fuel.
Rotating speed is 60~4000 revs/min in each step whipping process, and mixing time is 60~200 minutes, is controlled normal
Carried out under temperature.
Embodiment 4
This implementation is substantially the same manner as Example 1, and difference is that temperature is controlled in the present embodiment preparation process at 0 DEG C.
Embodiment 5
This implementation is substantially the same manner as Example 1, and difference is that temperature is controlled in the present embodiment preparation process -20
℃。
Embodiment 6
This implementation is substantially the same manner as Example 1, and difference is that temperature is controlled in the present embodiment preparation process 50
℃。
Comparative example 1
By hydrogen peroxide and ethanol according to 30:70 mass ratio stirs.
Comparative example 2
95% hydrogen peroxide.
The low freezing point fuel of the hydrogen peroxide mixture of above-mentioned comparative example 1~2 and embodiment 1~3 is detected, as a result
It is shown in Table 1.
Table 1
As seen from the above table, the present invention is produced low temperature resistant, fuel oxidizer mixing compatibility is good, comprising double elements and
The low freezing point fuel product of monoreactant chemical advantage has the advantages that good low freezing point, high stability, according to the performance to it
Test and practice principle, the freezing point reduction by 5~20 DEG C of the freezing point than single hydrogen peroxide of the fuel product, reach -60~-10
DEG C, can normally use at low ambient conditions, the fuel product can be for a long time preserved at ambient temperature.Suitable for aviation
Engine, airspace engine, vehicle, robot, gas generating unit, energy generating apparatus, carbon dioxide generating device, other
The use of the high-end fields such as extraordinary power-equipment, military project, scientific research.
Claims (6)
1. a kind of low freezing point fuel, it is characterised in that the component including following weight portion content：
2. a kind of low freezing point fuel according to claim 1, it is characterised in that its freezing point is -60~-10 DEG C.
3. a kind of low freezing point fuel according to claim 1, it is characterised in that the component including following weight portion content：
4. a kind of low freezing point fuel according to claim 3, it is characterised in that its freezing point is -60~-50 DEG C.
5. the preparation method of a kind of low freezing point fuel according to claim 1, it is characterised in that comprise the following steps：
(1) in tartaric acid being added into hydrogen peroxide by proportioning, and stir, obtain first liquid；
(2) in 8-hydroxyquinoline being added into ethanol by proportioning, and stir, obtain second liquid；
(3) first liquid and second liquid are mixed and stirred for uniformly obtaining described low freezing point fuel.
6. the preparation method of a kind of low freezing point fuel according to claim 5, it is characterised in that in each step whipping process
Rotating speed is 60~4000 revs/min, and mixing time is 60~200 minutes, and temperature control is at -20 DEG C~50 DEG C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611256823.6A CN106833762B (en) | 2016-12-30 | 2016-12-30 | A kind of low freezing point fuel and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611256823.6A CN106833762B (en) | 2016-12-30 | 2016-12-30 | A kind of low freezing point fuel and preparation method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106833762A true CN106833762A (en) | 2017-06-13 |
| CN106833762B CN106833762B (en) | 2018-09-04 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611256823.6A Expired - Fee Related CN106833762B (en) | 2016-12-30 | 2016-12-30 | A kind of low freezing point fuel and preparation method thereof |
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| Country | Link |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107266274A (en) * | 2017-06-30 | 2017-10-20 | 上海哈勃化学技术有限公司 | A kind of low temperature gas-forming agent and preparation method thereof |
| CN107325850A (en) * | 2017-06-30 | 2017-11-07 | 上海哈勃化学技术有限公司 | A kind of special fuel product and its preparation |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001009063A2 (en) * | 1999-07-29 | 2001-02-08 | Atlantic Research Corporation | Premixed liquid monopropellant solutions and mixtures |
| CN1775931A (en) * | 2005-12-07 | 2006-05-24 | 东北大学 | Fuel combined combustion method by adding hydrogen peroxide combustion adjuvant |
| CN1908133A (en) * | 2005-08-01 | 2007-02-07 | 葛明龙 | Group substituted silanes spaceflight fuel |
| CN102658066A (en) * | 2012-04-26 | 2012-09-12 | 葛明龙 | Catalytic decomposition low-concentration hydrogen peroxide reactor, combustion chamber and application thereof |
| KR20130133341A (en) * | 2012-05-29 | 2013-12-09 | 이승현 | The combusitive liquid mixed with the bio or methanol and water |
-
2016
- 2016-12-30 CN CN201611256823.6A patent/CN106833762B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001009063A2 (en) * | 1999-07-29 | 2001-02-08 | Atlantic Research Corporation | Premixed liquid monopropellant solutions and mixtures |
| CN1908133A (en) * | 2005-08-01 | 2007-02-07 | 葛明龙 | Group substituted silanes spaceflight fuel |
| CN1775931A (en) * | 2005-12-07 | 2006-05-24 | 东北大学 | Fuel combined combustion method by adding hydrogen peroxide combustion adjuvant |
| CN102658066A (en) * | 2012-04-26 | 2012-09-12 | 葛明龙 | Catalytic decomposition low-concentration hydrogen peroxide reactor, combustion chamber and application thereof |
| KR20130133341A (en) * | 2012-05-29 | 2013-12-09 | 이승현 | The combusitive liquid mixed with the bio or methanol and water |
Non-Patent Citations (1)
| Title |
|---|
| 王万军等: "绿色过氧化氢双组元自燃推进剂", 《化学推进剂与高分子材料》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107266274A (en) * | 2017-06-30 | 2017-10-20 | 上海哈勃化学技术有限公司 | A kind of low temperature gas-forming agent and preparation method thereof |
| CN107325850A (en) * | 2017-06-30 | 2017-11-07 | 上海哈勃化学技术有限公司 | A kind of special fuel product and its preparation |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106833762B (en) | 2018-09-04 |
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