CN110689640A - Risk judgment method for composite propellant mixed torque - Google Patents
Risk judgment method for composite propellant mixed torque Download PDFInfo
- Publication number
- CN110689640A CN110689640A CN201910892377.5A CN201910892377A CN110689640A CN 110689640 A CN110689640 A CN 110689640A CN 201910892377 A CN201910892377 A CN 201910892377A CN 110689640 A CN110689640 A CN 110689640A
- Authority
- CN
- China
- Prior art keywords
- torque
- formula
- hybrid
- explosion
- early warning
- 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
- 238000000034 method Methods 0.000 title claims abstract description 46
- 239000003380 propellant Substances 0.000 title claims abstract description 28
- 239000002131 composite material Substances 0.000 title claims abstract description 21
- 238000004880 explosion Methods 0.000 claims abstract description 75
- 230000035945 sensitivity Effects 0.000 claims abstract description 49
- 238000002156 mixing Methods 0.000 claims abstract description 38
- 238000012937 correction Methods 0.000 claims abstract description 29
- 239000000203 mixture Substances 0.000 claims description 39
- 238000009472 formulation Methods 0.000 claims description 31
- 239000002002 slurry Substances 0.000 claims description 24
- 238000004364 calculation method Methods 0.000 claims description 10
- 235000008216 herbs Nutrition 0.000 claims description 6
- 238000012360 testing method Methods 0.000 claims description 6
- 239000002360 explosive Substances 0.000 claims description 5
- 238000012502 risk assessment Methods 0.000 claims description 2
- 102220213553 rs1026192345 Human genes 0.000 claims description 2
- 239000003814 drug Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 229940079593 drug Drugs 0.000 description 3
- 239000000654 additive Substances 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000007800 oxidant agent Substances 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 1
- 230000003712 anti-aging effect Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012795 verification Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C3/00—Registering or indicating the condition or the working of machines or other apparatus, other than vehicles
- G07C3/005—Registering or indicating the condition or the working of machines or other apparatus, other than vehicles during manufacturing process
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
- G06Q10/063—Operations research, analysis or management
- G06Q10/0635—Risk analysis of enterprise or organisation activities
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q50/00—Information and communication technology [ICT] specially adapted for implementation of business processes of specific business sectors, e.g. utilities or tourism
- G06Q50/04—Manufacturing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/30—Computing systems specially adapted for manufacturing
Landscapes
- Business, Economics & Management (AREA)
- Engineering & Computer Science (AREA)
- Human Resources & Organizations (AREA)
- Strategic Management (AREA)
- General Physics & Mathematics (AREA)
- Economics (AREA)
- Physics & Mathematics (AREA)
- Entrepreneurship & Innovation (AREA)
- Theoretical Computer Science (AREA)
- Marketing (AREA)
- Manufacturing & Machinery (AREA)
- General Business, Economics & Management (AREA)
- Tourism & Hospitality (AREA)
- Educational Administration (AREA)
- Quality & Reliability (AREA)
- Operations Research (AREA)
- Game Theory and Decision Science (AREA)
- Development Economics (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Primary Health Care (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Medicinal Preparation (AREA)
Abstract
The invention belongs to the field of composite propellants, and particularly discloses a risk judgment method for composite propellant mixed torque, which comprises the steps of obtaining a torque early warning value coefficient and a torque safety value coefficient of a formula A; calculating the friction sensitivity degree of the formula A mixed explosion, the friction sensitivity degree of the formula A explosion critical point and the friction sensitivity degree of the formula B explosion critical point; calculating a torque early warning value correction coefficient and a torque safety value correction coefficient by using the parameters; and finally, determining a hybrid torque early warning value and a hybrid torque safety value, judging whether the actual hybrid torque is smaller than the hybrid torque safety value, if so, ensuring the safety of the hybrid process, otherwise, ensuring the safety of the hybrid process, and setting to stop the machine when the actual hybrid torque is larger than the hybrid torque early warning value. The invention sets a complete risk judgment method aiming at the torque representing the mixing safety, and can be suitable for various working conditions of all vertical mixers, thereby effectively eliminating the potential safety hazard in the mixing process and preventing explosion.
Description
Technical Field
The invention belongs to the field of composite propellants, and particularly relates to a risk judgment method for composite propellant mixing torque.
Background
The main components of the composite propellant are high polymer adhesive, inorganic oxidant and combustion agent, in addition, high-energy additive, plasticizer, curing agent, curing catalyst, anti-aging agent, combustion catalyst and technological additives. The process of preparing composite propellant is to use high polymer adhesive as elastic matrix, to mix large amount of oxidant and metal fuel powder, and to extrude viscous fluid onto the surface of multiphase mixture through mechanical mixing. The mechanical mixing is a process of coating, passivating and reducing the sense of the flammable and explosive powder by mechanical force, and is an indispensable very dangerous process in the production of the explosive.
The vertical mixer is a key device for completing the mixing process of the composite propellant, the mixing safety (whether the slurry is exploded or not) of the vertical mixer is related to the sensitivity of the propellant, the volume of the slurry, the solid content, the state of the slurry, the mixing rotating speed, the viscosity of the slurry, structural parameters of the mixer and other factors, and the mixing torque value represents the magnitude of the external force acting on the slurry and is an important quantitative index of the safety. The documents on the safety research aspect of the mixed composite propellant are less reported, and no complete risk judgment method aiming at the safety of the mixture, particularly the torque safety value is formed at present. However, as the composite propellant is developed to high energy and high burning speed, its various sensitivities are increased, the danger degree is also increased, and the requirements for the safety, stability and mixing quality of mixing are increased correspondingly. In recent years, the explosion accidents of the domestic mixing machine are almost once a year, and great loss is brought to the propellant manufacturing aspect.
How to combine the past accident record, the mixed structure parameter, the process parameter and the slurry formula characteristic to establish the risk judgment method of the composite propellant mixed torque to prevent the occurrence of explosion events has great and profound significance.
Disclosure of Invention
In view of the above-mentioned drawbacks and/or needs for improvement in the prior art, the present invention provides a method for determining the risk of hybrid torque of a composite propellant, in which a friction sensitivity number is used as a determination index, and a hybrid torque warning value and a hybrid torque safety value are obtained through calculation, so as to determine the risk of hybrid torque of the composite propellant, and thus, the method is particularly suitable for applications such as the preparation of composite propellants.
In order to achieve the above object, the present invention provides a method for determining the risk of hybrid torque of a composite propellant, comprising the following steps:
s1, determining a torque explosion value, a torque early warning value and a torque safety value of the formula A according to the torque historical data of the mixed accident, and thus obtaining a torque early warning coefficient and a torque safety coefficient of the formula A;
s2, calculating the friction sensitivity degree of the mixed explosion of the formula A, the friction sensitivity degree of the explosion critical point of the formula A and the friction sensitivity degree of the explosion critical point of the formula B according to the force increment and the speed increment of the paddle;
s3, calculating a torque early warning value correction coefficient and a torque safety value correction coefficient by using the torque early warning coefficient and the torque safety coefficient of the formula A obtained in the step S1, and the friction sensitivity number of the formula A mixed explosion, the friction sensitivity number of the formula A explosion critical point and the friction sensitivity number of the formula B explosion critical point obtained in the step S2;
s4, determining a hybrid torque early warning value and a hybrid torque safety value according to the torque early warning value correction coefficient and the torque safety value correction coefficient obtained in the step S3, judging whether the actual hybrid torque is smaller than the hybrid torque safety value, if so, the hybrid process is safe, if not, the hybrid process is unsafe, and setting the device to stop when the actual hybrid torque is larger than the hybrid torque early warning value.
As a further preferred option, in step S1, the formula a torque warning coefficient is calculated by using the following formula,
in the formula k1Torque early warning coefficient, T, for formulation aA-mixed explosionTorque explosion value, T, for formulation AA-early warningThe torque early warning value of formula A;
the formula a torque safety factor was calculated using the following formula,
in the formula k2Torque safety factor, T, for formulation aA-safetyTorque safety values for formulation a.
As a further preferred, in step S2, the calculating the friction sensitivity number of the formula a mixed explosion includes the following sub-steps:
s21 calculation of the increment of force Δ P of the mixed explosive slurry of formulation A using the following formulaSlurry-mix explosion,
In the formula (d)BladeIs the diameter of the blade, SArea ofIs the effective stressed area of the blade;
s22 calculation of slurry velocity increment Δ v using the following equationCombination of Chinese herbs,
ΔvCombination of Chinese herbs=(πNPublicdPublic+πNFromdBlade)
In the formula, NPublicRevolution speed of the blade, dPublicIs the revolution diameter of the blade, NFromThe rotation speed of the paddle is the rotation speed;
s23 Using Δ P obtained in the step S21Slurry-mix explosionAnd Δ v obtained in said step S22Combination of Chinese herbsThe degree of frictional sensitivity E of the mixed explosion of formulation A was calculated according to the following formulaA-mixed explosion,
As a further preferred, in step S2, the step of calculating the friction sensitivity number of the explosion critical point of formula a includes the following sub-steps:
s24 test for the stress increment delta P of the formula A at the explosion critical point, namely the explosion probability of 17 percentA-criticalAnd the velocity increment of the slurry Δ vA-critical;
S25 the degree of frictional sensitivity E at the explosion critical point of formulation A was calculated according to the following formulaA-critical,
As a further preferred, in step S2, the step of calculating the friction sensitivity number of the explosion critical point of formula B includes the following sub-steps:
s26 test for the stress increment delta P of the formula B when the explosion critical point, namely the explosion probability is 17 percentB-criticalAnd the velocity increment of the slurry Δ vB-critical;
S27 the degree of frictional sensitivity E at the explosion critical point of formulation B was calculated according to the following formulaB-critical,
As a further preference, the step S3 includes the following sub-steps:
S31A coefficient k for correcting the degree of friction sensitivity of formulation A was calculated according to the following equation3,
S32 judging degree of friction sensitivity E of formula B mixed explosionB-criticalWhether or not the degree of frictional sensitivity E is less than or equal to the explosion critical point of the formula AA-criticalIf yes, go to step S33, otherwise, go to step S34;
s33 setting a correction coefficient k of the torque early warning valueEarly warning=k1k3While setting a torque safety value correction coefficient kSecurity=k2k3;
S34 setting a correction coefficient k of the torque early warning valueEarly warning=nk1k3While setting a torque safety value correction coefficient kSecurity=nk2k3,n>1。
More preferably, the value of n in step S34 is preferably 1.5-2.
As a further preference, the step S4 includes the following sub-steps:
s41 Using E obtained in the step S2B-criticalCalculating the torque threshold T for formulation B according toB-critical,
S42 using the TB-critical、kEarly warningAnd kSecurityRespectively calculating a hybrid torque early warning value T according to the following formulaHybrid early warningAnd a hybrid torque safety value THybrid security,
S43 judges the actual hybrid torque TActual mixing torqueWhether it is less than the safe value T of the mixed torqueHybrid securityIf yes, the mixing process is safe, if no, the mixing process is unsafe, and the actual mixing torque T is setActual mixing torqueIs greater thanThe hybrid torque early warning value THybrid early warningAnd stopping the machine.
Generally, compared with the prior art, the above technical solution conceived by the present invention mainly has the following technical advantages:
1. the friction sensitivity number is used as a safety judgment index, and a complete risk judgment method is formulated aiming at the torque representing the mixing safety, so that guidance is provided for determining the early warning value and the safety value of the mixing torque, the method can be suitable for various working conditions of all vertical mixing machines, such as different structural parameters, process parameters and formula characteristics, further the potential safety hazard in the mixing process is effectively eliminated, the explosion accident is prevented, and the reliability is higher through the engineering verification of multiple formulas of multiple sets of vertical mixing systems;
2. particularly, the critical friction sensitivity number of the formula A and the critical friction sensitivity number of the formula B are compared to determine whether the formula B is more dangerous than the formula A, so that the torque early warning correction coefficient and the torque safety value correction coefficient are determined, the mixed torque early warning value and the mixed torque safety value can be accurately optimized, and the risk judgment is more accurate and reliable.
Drawings
Fig. 1 is a flow chart of a risk assessment method for composite propellant mixing torque provided by a preferred embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention. In addition, the technical features involved in the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.
As shown in fig. 1, an embodiment of the present invention provides a method for determining a risk of hybrid propellant torque, the method including the steps of:
s1 determining the torque explosion value of formula A according to the torque history data of the mixed accidentTA-mixed explosionTorque early warning value TA-early warningAnd a torque safety value TA-safetyCalculating formula A torque early warning coefficient k by respectively using formula (1) and formula (2)1And formulation A Torque safety factor k2,
S2 the degree of friction sensitivity E of the mixed explosion of formula A was calculated using the formula (3)A-mixed explosionThe degree of frictional sensitivity E at the explosion critical point of formulation AA-criticalDegree of Friction with explosion Critical Point of formulation BB-critical,
In the formula EFeeling of massageIs degree of frictional sensitivity, Δ POar with a rotating shaftDelta v is the increment of the drug pulp stress (average pressure of the pulp leaves to the drug pulp)Combination of Chinese herbsThe formula can comprehensively consider the influence of the structural parameters, the process parameters and the formula characteristics of the medicinal slurry on the medicinal slurry speed increment (taking the maximum linear speed of the tip of the blade);
s3 utilizes the torque early warning coefficient k of the formula A obtained in the step S11Torque safety factor k2And the degree of frictional sensitivity E of the mixed explosion of the formulation A obtained in the step S2A-mixed explosionThe degree of frictional sensitivity E at the explosion critical point of formulation AA-criticalDegree of Friction with explosion Critical Point of formulation BB-criticalCalculating a torque early warning value correction coefficient kEarly warningAnd a torque safety value correction coefficient kSecurity;
S4 uses the torque warning value correction coefficient k obtained in step S3Early warningAnd a torque safety value correction coefficient kSecurityDetermining a hybrid torque warning value THybrid early warningAnd a hybrid torque safety value THybrid securityDetermining the actual hybrid torque TPractical mixing torqueMomentWhether it is less than the safe value T of the mixed torqueHybrid securityIf yes, the mixing process is safe, if no, the mixing process is unsafe, and the actual mixing torque T is setActual mixing torqueGreater than the early warning value T of the mixed torqueHybrid early warningAnd stopping the machine.
Further, step S2 includes the following sub-steps:
s21 calculation of stress increment DeltaP of mixed explosive slurry of formula A according to formula (4)Slurry-mix explosion,
In the formula (d)BladeIs the diameter of the blade, SArea ofIs the effective stressed area of the blade, SArea ofThe calculation can be carried out by adopting the formula (5), and the calculation can also be obtained by carrying out simulation measurement on a three-dimensional model,
in the formula, H is a function of material height, the expression is shown in formula (6), delta is the height of the gap of the bottom of the pan, F (x) is a function of blade height, G (y) is a function of the blade width expansion line,
in the formula, WMedicineRho is the density of the medicinal slurry (rho is 100/∑ (mi/di), mi is the mass percent of the components in the formula, di is the density value of the components in the formula), V is the weight of the mixed medicinal slurryEfficient bladeThe total volume r of the paddle immersed in the slurryOar with a rotating shaftIs the blade radius (r)Oar with a rotating shaft=dOar with a rotating shaft/2);
S22 calculation of slurry velocity increment Deltav according to equation (7)Combination of Chinese herbs,
ΔvCombination of Chinese herbs=(πNPublicdPublic+πNFromdBlade) (7)
In the formula NPublicRevolution speed of the blade, dPublicIs the revolution diameter of the blade, NFromThe rotation speed of the paddle is the rotation speed;
s23 Using Δ P obtained in step S21Slurry-mix explosionAnd Δ v obtained in step S22Combination of Chinese herbsThe degree of frictional sensitivity E of the mixed explosion of the formulation A was calculated from the formula (8)A-mixed explosion,
S24 testing stress increment delta P of the drug slurry when the explosion critical point, namely the explosion probability is 17 percent, of the formula A through a friction sensitivity instrumentA-criticalAnd the velocity increment of the slurry Δ vA-critical;
S25 the degree of frictional sensitivity E at the explosion critical point of formulation A was calculated from the formula (9)A-critical,
S26 testing the stress increment delta P of other formula, such as formula B, at the explosion critical point, i.e. the explosion probability of 17%B-criticalAnd the velocity increment of the slurry Δ vB-critical;
S27 is based on the formulaCalculating the degree of frictional sensitivity E of the explosion critical point of the formula BB-critical。
Further, step S3 includes the following sub-steps:
s31 is based on the formulaCalculating the frictional sensitivity number correction coefficient k of formula A3;
S32 judges whether or not formula B is more sensitive (dangerous) than formula A, i.e., satisfies EB-critical≤EA-criticalIf yes, the formula B is safer than the formula A, the step is switched to S33, and if not, the formula B is more dangerous than the formula A, the step is switched to S34;
S33 setting a torque early warning value correction coefficient kEarly warning=k1k3While setting a torque safety value correction coefficient kSecurity=k2k3;
S34 setting a correction coefficient k of the torque early warning valueEarly warning=nk1k3While setting a torque safety value correction coefficient kSecurity=nk2k3N is greater than 1, and more preferably 1.5 to 2.
Further, step S4 includes the following sub-steps:
s41 Using E obtained in step S2B-criticalAccording to the formulaCalculate Torque threshold T for formulation BB-criticalThe calculation formula is suitable for all vertical mixers;
s42 uses TB-critical、kEarly warningAnd kSecurityAccording to the formula respectivelyCalculating a hybrid torque early warning value THybrid early warningAnd a hybrid torque safety value THybrid security;
S43 judges the actual hybrid torque TActual mixing torqueWhether it is less than the safe value T of the mixed torqueHybrid securityIf yes, the mixing process is safe, if no, the mixing process is unsafe, and the actual mixing torque T is setActual mixing torqueGreater than the early warning value T of the mixed torqueHybrid early warningAnd stopping the machine.
It will be understood by those skilled in the art that the foregoing is merely a preferred embodiment of the present invention, and is not intended to limit the invention, and that any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included within the scope of the present invention.
Claims (8)
1. A risk assessment method for hybrid propellant torque is characterized by comprising the following steps:
s1, determining a torque explosion value, a torque early warning value and a torque safety value of the formula A according to the torque historical data of the mixed accident, and thus obtaining a torque early warning coefficient and a torque safety coefficient of the formula A;
s2, calculating the friction sensitivity degree of the mixed explosion of the formula A, the friction sensitivity degree of the explosion critical point of the formula A and the friction sensitivity degree of the explosion critical point of the formula B according to the force increment and the speed increment of the paddle;
s3, calculating a torque early warning value correction coefficient and a torque safety value correction coefficient by using the torque early warning coefficient and the torque safety coefficient of the formula A obtained in the step S1, and the friction sensitivity number of the formula A mixed explosion, the friction sensitivity number of the formula A explosion critical point and the friction sensitivity number of the formula B explosion critical point obtained in the step S2;
s4, determining a hybrid torque early warning value and a hybrid torque safety value according to the torque early warning value correction coefficient and the torque safety value correction coefficient obtained in the step S3, judging whether the actual hybrid torque is smaller than the hybrid torque safety value, if so, the hybrid process is safe, if not, the hybrid process is unsafe, and setting the device to stop when the actual hybrid torque is larger than the hybrid torque early warning value.
2. The method for determining the risk of hybrid torque of a composite propellant according to claim 1, wherein in step S1, a formula A torque warning coefficient is calculated using the following formula,
in the formula k1Torque early warning coefficient, T, for formulation aA-mixed explosionTorque explosion value, T, for formulation AA-early warningThe torque early warning value of formula A;
the formula a torque safety factor was calculated using the following formula,
in the formula k2Torque safety factor, T, for formulation aA-safetyTorque safety values for formulation a.
3. The method for determining the risk of hybrid propellant torque as claimed in claim 1 or 2, wherein the step S2 of calculating the friction sensitivity number of the formula a hybrid explosion includes the following sub-steps:
s21 calculation of the increment of force Δ P of the mixed explosive slurry of formulation A using the following formulaSlurry-mix explosion,
In the formula (d)BladeIs the diameter of the blade, SArea ofIs the effective stressed area of the blade;
s22 calculation of slurry velocity increment Δ v using the following equationCombination of Chinese herbs,
ΔvCombination of Chinese herbs=(πNPublicdPublic+πNFromdBlade)
In the formula, NPublicRevolution speed of the blade, dPublicIs the revolution diameter of the blade, NFromThe rotation speed of the paddle is the rotation speed;
s23 Using Δ P obtained in the step S21Slurry-mix explosionAnd Δ v obtained in said step S22Combination of Chinese herbsThe degree of frictional sensitivity E of the mixed explosion of formulation A was calculated according to the following formulaA-mixed explosion,
4. The method for determining the risk of hybrid propellant torque as claimed in claim 1, wherein the step S2 of calculating the friction sensitivity number of the explosion critical point of the formulation a comprises the following sub-steps:
s24 test for the stress increment delta P of the formula A at the explosion critical point, namely the explosion probability of 17 percentA-criticalAnd the velocity increment of the slurry Δ vA-critical;
S25 the degree of frictional sensitivity E at the explosion critical point of formulation A was calculated according to the following formulaA-critical,
5. The method for determining the risk of hybrid propellant torque as claimed in claim 1, wherein the step S2 of calculating the friction sensitivity number of the explosion critical point of the formulation B comprises the following sub-steps:
s26 test for the stress increment delta P of the formula B when the explosion critical point, namely the explosion probability is 17 percentB-criticalAnd the velocity increment of the slurry Δ vB-critical;
S27 the degree of frictional sensitivity E at the explosion critical point of formulation B was calculated according to the following formulaB-critical,
6. The method for determining the risk of hybrid torque of a composite propellant according to claim 1, wherein the step S3 includes the substeps of:
S31A coefficient k for correcting the degree of friction sensitivity of formulation A was calculated according to the following equation3,
S32 judging degree of friction sensitivity E of formula B mixed explosionB-criticalWhether or not the degree of frictional sensitivity E is less than or equal to the explosion critical point of the formula AA-criticalIf yes, go to step S33, otherwise, go to step S34;
s33 setting a correction coefficient k of the torque early warning valueEarly warning=k1k3While setting a torque safety value correction coefficient kSecurity=k2k3;
S34 setting a correction coefficient k of the torque early warning valueEarly warning=nk1k3While setting a torque safety value correction coefficient kSecurity=nk2k3,n>1。
7. The method for determining the risk of hybrid torque of the composite propellant according to claim 6, wherein n in the step S34 preferably takes a value of 1.5-2.
8. The method for determining the risk of hybrid torque of a composite propellant according to any one of claims 1 to 7, wherein the step S4 includes the substeps of:
s41 Using E obtained in the step S2B-criticalCalculating the torque threshold T for formulation B according toB-critical,
S42 using the TB-critical、kEarly warningAnd kSecurityRespectively calculating a hybrid torque early warning value T according to the following formulaHybrid early warningAnd a hybrid torque safety value THybrid security,
S43 judges the actual hybrid torque TActual mixing torqueWhether it is less than the safe value T of the mixed torqueHybrid securityIf yes, the mixing process is safe, if no, the mixing process is unsafe, and the actual mixing torque T is setActual mixing torqueGreater than the early warning value T of the mixed torqueHybrid early warningAnd stopping the machine.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910892377.5A CN110689640B (en) | 2019-09-20 | 2019-09-20 | Risk judgment method for composite propellant mixed torque |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910892377.5A CN110689640B (en) | 2019-09-20 | 2019-09-20 | Risk judgment method for composite propellant mixed torque |
Publications (2)
Publication Number | Publication Date |
---|---|
CN110689640A true CN110689640A (en) | 2020-01-14 |
CN110689640B CN110689640B (en) | 2020-12-08 |
Family
ID=69109894
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201910892377.5A Expired - Fee Related CN110689640B (en) | 2019-09-20 | 2019-09-20 | Risk judgment method for composite propellant mixed torque |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110689640B (en) |
Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090242037A1 (en) * | 2008-03-27 | 2009-10-01 | Drescher William T | Fuel delivery system for a torch |
US8444785B2 (en) * | 2007-01-05 | 2013-05-21 | Lockheed Martin Corporation | Solid composite propellants and methods of making propellants |
CN103454153A (en) * | 2013-09-12 | 2013-12-18 | 南京理工大学 | Test piece for determining I type fracture energy of compound propellant/coating layer bonding interface |
CN104492328A (en) * | 2014-12-19 | 2015-04-08 | 西安近代化学研究所 | Resonance mixing method for high-solid content adhesive system |
RU2014107220A (en) * | 2014-02-25 | 2015-08-27 | Николай Евгеньевич Староверов | ROCKET ENGINE STAROVEROVA-16 / OPTIONS / |
CN104912891A (en) * | 2015-04-15 | 2015-09-16 | 华中科技大学 | Safe connecting fixing device of vertical type mixing machine oar blade |
CN205414594U (en) * | 2016-02-02 | 2016-08-03 | 华中科技大学 | A numerical control equipment for plastic of solid rocket engine powder column |
CN206671159U (en) * | 2017-04-18 | 2017-11-24 | 浏阳花炮标准检验所 | A kind of pendulum type friction sensibility instrument |
CN108043305A (en) * | 2018-01-03 | 2018-05-18 | 湖北航鹏化学动力科技有限责任公司 | A kind of solid-propellant pulps without slurry mixing preparation method and system |
CN110104222A (en) * | 2019-04-25 | 2019-08-09 | 北京控制工程研究所 | A kind of modularization propulsion service system promoted based on mixed mode |
CN110156547A (en) * | 2019-07-03 | 2019-08-23 | 江西航天经纬化工有限公司 | A kind of high intensity low pressure index HTPB composite propellant and preparation method thereof |
CN110550607A (en) * | 2019-09-12 | 2019-12-10 | 湖北航天化学技术研究所 | alpha-AlH 3 flotation method and application thereof |
-
2019
- 2019-09-20 CN CN201910892377.5A patent/CN110689640B/en not_active Expired - Fee Related
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8444785B2 (en) * | 2007-01-05 | 2013-05-21 | Lockheed Martin Corporation | Solid composite propellants and methods of making propellants |
US20090242037A1 (en) * | 2008-03-27 | 2009-10-01 | Drescher William T | Fuel delivery system for a torch |
CN103454153A (en) * | 2013-09-12 | 2013-12-18 | 南京理工大学 | Test piece for determining I type fracture energy of compound propellant/coating layer bonding interface |
RU2014107220A (en) * | 2014-02-25 | 2015-08-27 | Николай Евгеньевич Староверов | ROCKET ENGINE STAROVEROVA-16 / OPTIONS / |
CN104492328A (en) * | 2014-12-19 | 2015-04-08 | 西安近代化学研究所 | Resonance mixing method for high-solid content adhesive system |
CN104912891A (en) * | 2015-04-15 | 2015-09-16 | 华中科技大学 | Safe connecting fixing device of vertical type mixing machine oar blade |
CN205414594U (en) * | 2016-02-02 | 2016-08-03 | 华中科技大学 | A numerical control equipment for plastic of solid rocket engine powder column |
CN206671159U (en) * | 2017-04-18 | 2017-11-24 | 浏阳花炮标准检验所 | A kind of pendulum type friction sensibility instrument |
CN108043305A (en) * | 2018-01-03 | 2018-05-18 | 湖北航鹏化学动力科技有限责任公司 | A kind of solid-propellant pulps without slurry mixing preparation method and system |
CN110104222A (en) * | 2019-04-25 | 2019-08-09 | 北京控制工程研究所 | A kind of modularization propulsion service system promoted based on mixed mode |
CN110156547A (en) * | 2019-07-03 | 2019-08-23 | 江西航天经纬化工有限公司 | A kind of high intensity low pressure index HTPB composite propellant and preparation method thereof |
CN110550607A (en) * | 2019-09-12 | 2019-12-10 | 湖北航天化学技术研究所 | alpha-AlH 3 flotation method and application thereof |
Non-Patent Citations (4)
Title |
---|
庞爱民: "《固体火箭推进剂理论与工程》", 30 June 2014, 北京 中国宇航出版社 * |
张力恒: "推进剂装药混合过程安全性研究", 《固体火箭技术》 * |
李锡文: "大型立式混合装备设计研究", 《西南大学学报》 * |
雷宁: "国外固体推进剂装药工艺安全性技术", 《飞航导弹》 * |
Also Published As
Publication number | Publication date |
---|---|
CN110689640B (en) | 2020-12-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Mintz et al. | Hydriding kinetics of powders | |
CN110689640B (en) | Risk judgment method for composite propellant mixed torque | |
Lin et al. | Effect of Aluminum Fiber Content on the Underwater Explosion Performance of RDX‐based Explosives | |
Salehi et al. | On the use of a powder rheometer to characterize the powder flowability at low consolidation with torque resistances | |
Pang et al. | Effects of dihydroxylammonium 5, 5′‐bistetrazole‐1, 1′‐diolate on the properties of htpb based composite solid propellant | |
Santhosh et al. | Rheokinetic characterization of polyurethane formation in a highly filled composite solid propellant | |
Kroezen et al. | Bubble size distribution and energy dissipation in foam mixers | |
Keshavarz et al. | A simple method for reliable estimation of the bubble energy in the underwater explosion | |
Furlan et al. | Centrifugal pump performance when handling highly non‐Newtonian clays and tailings slurries | |
Cheng et al. | A new type of functional chemical sensitizer MgH 2 for improving pressure desensitization resistance of emulsion explosives | |
Wu et al. | Experimental study of rheological properties of solid propellant slurry at low‐shear rate and numerical simulation | |
Mahanta Abhay et al. | Empirical modeling of chemoviscosity of hydroxy terminated polybutadiene based solid composite propellant slurry | |
Geckler et al. | Effervescent atomization of viscoelastic liquids: experiment and modeling | |
Yuan et al. | Influence of strain rate on mechanical properties of HTPE/PCL propellant applying to wide temperature range | |
Lade et al. | Effect of aluminium nanoparticles on rheology of AP based composite propellant: experimental study and mathematical modelling | |
Chauhan et al. | Studies on the processing of HTPB‐based fast‐burning propellant with trimodal oxidiser distribution and its rheological behaviour | |
Zhang et al. | Effect of particle size distribution on explosion intensity of aluminum powder | |
CN110108744A (en) | A kind of classification of explosives method based on thermal acceleration degradation | |
Restasari et al. | Particle packing models to determine time-dependent slip flow properties of highly filled polyurethane-based propellant | |
Wang et al. | Effect of the Volume Concentration of Binary Mixed Particles on the Flow and Wear Characteristics of Centrifugal Pumps | |
Tamura et al. | Normal Stress Effect in Dilute Polymer Solutions. I. Polystyrene in Dioctyl Phthalate | |
Baker et al. | Critical impact initiation energies for three HTPB propellants | |
CN109251118A (en) | A kind of anti high overload composite propellant and preparation method thereof | |
Wang et al. | Rheology of typical emulsifiers and effects on stability of emulsion explosives | |
Wang et al. | Numerical Study on Thermal Safety of Emulsion Matrix in Emulsifier |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201208 |
|
CF01 | Termination of patent right due to non-payment of annual fee |