Remote control full-automatic processing system of sample for testing composite solid propellant

By designing a remotely controlled fully automatic processing system for composite solid propellant test samples, the vacuum suction cup and drive mechanism is used to realize sample slices and sample preparation automation, solving the safety hazards of operators during traditional sample preparation, and realizing the sample preparation Fully automated and highly safe production of sample preparation.

CN119223701APending Publication Date: 2024-12-31SHANGHAI AEROSPACE CHEM ENG INST
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Patent Information

Application Number
CN202410689212.9
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-05-30
Publication Date
2024-12-31

AI Technical Summary

Technical Problem

In the mechanical properties and static combustion rate tests of composite solid propellants, operators need to operate them manually at close range during traditional sample preparation, which poses safety hazards such as combustion and explosion.

Method used

Design a sample remotely controlled fully automatic processing system for composite solid propellant tests, including slicing system, operation system and sample preparation system, and automate the sample slicing and sample preparation process through vacuum suction cups and drive mechanisms, operators and operations Area physical isolation, remote operation control system is used to remotely monitor and control the sample preparation process.

Benefits of technology

The full automation of the sample preparation process of composite solid propellant samples has been achieved, which eliminates the safety hazards caused by operator contact, greatly improves the safety and reliability of sample preparation, and can simultaneously produce dumbbell samples for mechanical performance testing and Strip type specimen for static combustion speed test.

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Abstract

The invention provides a remote control full-automatic processing system of a sample for testing a composite solid propellant, which comprises a slicing system for integrally cutting a square blank of the composite solid propellant into sheet-shaped intermediate blanks; the operation system is used for transferring the sheet-shaped intermediate blank material finished by the slicing system to the sample preparation system; the sample preparation system is used for performing sample preparation on the sheet-shaped intermediate blank material operated by the operation system; the remote operation control system is used for remotely controlling the slicing system, the operation system and the sample preparation system to complete preparation of dumbbell-shaped samples and strip-shaped samples; the remote operation control system is located in a control area, the control slicing system, the operation system and the sample preparation system are located in an operation area, and the operation area and the control area are physically isolated. Full-automatic operation is achieved in the whole machining process, operators and propellant sample preparation are physically isolated, potential safety hazards brought to the operators in the propellant sample preparation process are eliminated, and the intrinsic safety of sample preparation is greatly improved.
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Description

Technical Field

[0001] The invention belongs to the field of composite solid propellant sample production and processing, and in particular relates to a composite solid propellant mechanical property test and static burning rate test sample full-automatic remote control production and processing system. Background Art

[0002] As an energetic material, solid propellant not only provides energy for solid motors, but also has certain dangers. Due to the stimulation of external excitation sources such as heat, mechanical impact, friction and electrostatic field, solid propellant may cause combustion, explosion and other accidents. In particular, the development and application of new high-energy raw materials in recent years have made great progress in high-energy propellants. However, the increase in energy has brought about significant safety issues in the production, transportation, storage and use of solid propellants. During these processes, the propellants are subjected to combustion and explosion accidents caused by external stimuli such as accidental falls, impacts, and heat, which not only cause fatal damage to weapons and equipment, but also may cause a large number of casualties and huge economic losses.

[0003] When conducting mechanical properties and static burning rate tests on composite solid propellants, it is necessary to use composite solid propellant square billets as raw materials and process various forms of specimens (dumbbell-shaped specimens for mechanical properties testing and strip-shaped specimens for static burning rate testing).

[0004] The preparation process of propellant dumbbell specimens is shown in Figure 1 , including: (1) the square billet is divided into two sections; (2) one section is divided into four blocks along the casting direction; (3) each block is divided into several pieces with a thickness of 10 mm; (4) a dumbbell-shaped specimen is made.

[0005] The preparation process of burning rate test specimens is shown in Figure 2 , including: processing the composite solid propellant square billets into (4mm±0.5mm), (5mm±0.5mm) or (10mm±0.5mm) specimens one by one along the casting direction, and then laying the single specimen pieces flat and using a slicer to process them one by one into (4mm±0.5mm)×(4mm±0.5mm)×150mm, (5mm±0.5mm)×(5mm±0.5mm)×150mm, or (10mm±0.5mm)×(10mm±0.5mm)×150mm medicine strips.

[0006] The entire sample preparation process requires operators to use large guillotines, pneumatic slicers (strips), pneumatic tablet presses and other devices to complete the work manually at close range. During this process, the cutters will frequently cause friction, extrusion, collision and other stimulations to the composite solid propellant; and because the operator is in close contact with the propellant, there is a risk of the human body releasing static electricity to the propellant, especially in dry winter weather. The above potential factors may lead to accidents such as combustion and explosion of solid propellants, posing a major safety hazard.

[0007] Therefore, it is of great significance to establish a remote-controlled fully automatic processing system for composite solid propellant test specimens, realize fully automated operation of the composite solid propellant test specimen preparation process, physically isolate operators and propellant preparation, and ensure the safety and reliability of the composite solid propellant test specimen preparation process. Summary of the invention

[0008] In view of the current situation that the whole process of composite solid propellant sample preparation needs to be completed by operators manually working at close range, which poses a major safety hazard, the present invention aims to provide a remote-controlled fully-automatic processing system for composite solid propellant test samples, so as to realize fully-automatic operation of the composite solid propellant test sample preparation process, physically isolate operators and propellant sample preparation, and ensure the inherent safety of the composite solid propellant test sample preparation process.

[0009] The technical solution provided by the present invention is as follows:

[0010] A remote-controlled fully automatic processing system for composite solid propellant test specimens, comprising:

[0011] Slicing system, which cuts the composite solid propellant square billet into sheet-shaped intermediate billets;

[0012] The operation system transfers the sheet-shaped intermediate blanks completed by the slicing system to the sample preparation system;

[0013] The sample preparation system prepares samples of the sheet-shaped intermediate blanks operated by the operating system;

[0014] The sample preparation system includes a fifth drive mechanism, a dumbbell-shaped cutter, a sixth drive mechanism, a seventh drive mechanism, a dumbbell-shaped cutter holder, a blade, a blade holder, a second horizontal guide rail, a sample preparation plane, a second vertical guide rail, and a third vertical guide rail;

[0015] The dumbbell-shaped tool is fixed on the dumbbell-shaped tool holder, the dumbbell-shaped tool holder is embedded in the second vertical guide rail, the dumbbell-shaped tool moves up and down along the second vertical guide rail, the second vertical guide rail is fixed on the support surface of the support platform, the sixth drive mechanism is connected to the dumbbell-shaped tool holder, and serves as a power source for the dumbbell-shaped tool to move up and down; the blade is fixed on the blade holder, the blade holder is embedded in the third vertical guide rail, the blade moves up and down along the third vertical guide rail, the third vertical guide rail is fixed to the support surface of the support platform, and the seventh drive mechanism is connected to the blade holder. The first horizontal guide rail is connected to the frame and serves as a power source for the blade to move up and down; the second horizontal guide rail crosses the dumbbell-shaped tool and the blade and is fixed on the supporting surface; the sample preparation plane is connected to the second horizontal guide rail, on which the sheet-like intermediate blank is carried, and moves horizontally directly under the dumbbell-shaped tool and the blade; the fifth driving mechanism is connected to the sample preparation plane and serves as a power source for the horizontal movement of the sample preparation plane, driving the sheet-like intermediate blank on the sample preparation plane to move to the bottom of the dumbbell-shaped tool or the blade, and the dumbbell-shaped sample is prepared by the dumbbell-shaped tool, and the strip-shaped sample is prepared by the blade.

[0016] Furthermore, the sample preparation system also includes an eighth driving mechanism and a push plate arranged on the sample preparation plane. The eighth driving mechanism is connected to the push plate and serves as a power source for the horizontal movement of the suction cup baffle. When preparing samples, the push plate pushes the sheet-like intermediate blank to a fixed position on the sample preparation plane, so that the dumbbell-shaped tool or blade starts preparing samples at the fixed position on the sample preparation plane.

[0017] Furthermore, a positioning protrusion is provided on the sample making plane, and the push plate is opposite to the positioning protrusion. When making samples, the sheet-like intermediate blank is pushed to the positioning protrusion of the sample making plane, and the positioning protrusion of the sample making plane is used as a mark position for positioning the sheet-like intermediate blank. Alternatively, after the sheet-like intermediate blank is pushed to the positioning protrusion of the sample making plane, the sheet-like intermediate blank is continued to be pressed against, and the sample is fixed together with the positioning protrusion of the sample making plane.

[0018] Furthermore, the sample preparation system also includes a sample unloading mechanism, which includes a frame, a ninth driving mechanism and a unloading piece. The frame is arranged close to the sample preparation plane, the ninth driving mechanism is fixed on the frame, and the unloading piece is fixed on the ninth driving mechanism. The unloading piece moves horizontally under the drive of the ninth driving mechanism to deliver the sample prepared on the sample preparation plane into the sample collection box.

[0019] Furthermore, the slicing system includes a gate knife, a first vertical guide rail, a first driving mechanism, a support frame, a billet baffle, a second driving mechanism and a first horizontal guide rail; the support frame is fixed on the support surface of the support platform, and the first vertical guide rail is embedded in and fixed on one side of the support frame, facing the transfer system; the gate knife is connected to the first vertical guide rail, and moves vertically up and down along the first vertical guide rail to slice the composite solid propellant square billet; the driving mechanism is connected to the gate knife, serving as a power source for the movement of the gate knife; the first horizontal guide rail is fixed on the support surface, and the billet baffle is connected to the first horizontal guide rail, and moves along the first horizontal guide rail to push the composite solid propellant square billet toward the gate knife for stepping operation; the second driving mechanism is connected to the billet baffle, serving as a power source for the billet baffle; the area surrounded by the support frame, the billet baffle and the first horizontal guide rail is the propellant placement area.

[0020] Furthermore, the blank baffle is a suction cup baffle, and a plurality of vacuum suction cups are fixed on the plate body. One end of the vacuum suction cup is connected to the gas source through a gas pipeline, and a vacuum generator is installed on the gas pipeline. The other end passes through a prefabricated hole on the plate body and contacts with the composite solid propellant square blank to be cut, and the composite solid propellant square blank is fixed by adsorption through the negative pressure in the pipeline.

[0021] Furthermore, the operation system includes a first transfer guide rail, a third driving mechanism, a second transfer guide rail, a fourth driving mechanism, a transfer mechanism, a swinging mechanism and a transfer suction cup; the second transfer guide rail is embedded in the first transfer guide rail, the transfer mechanism is embedded in the second transfer guide rail, the swinging mechanism is fixed on the transfer mechanism, and the transfer suction cup is connected to the swinging mechanism, so as to realize the movement of the second transfer guide rail, the transfer mechanism, the swinging mechanism and the transfer suction cup as a whole along the first transfer guide rail, and the movement of the transfer mechanism, the swinging mechanism and the transfer suction cup as a whole along the second transfer guide rail; the fourth driving mechanism is fixed on the second transfer guide rail, serving as a power source for the overall movement of the transfer mechanism, the swinging mechanism and the transfer suction cup; the first transfer guide rail is fixed on the supporting surface, and the third driving mechanism is fixed on the first transfer rail, serving as a power source for the overall movement of the second transfer guide rail, the transfer mechanism, the swinging mechanism and the transfer suction cup; the swinging mechanism, as the power source of the transfer suction cup, drives the transfer suction cup to reciprocate in the horizontal-vertical direction, converts the vertical sheet-like intermediate blank completed by the slicing system into a horizontal state, and places it on the sample preparation plane.

[0022] Furthermore, the transfer suction cup includes an adapter plate and a plurality of vacuum suction cups fixed on the adapter plate; the adapter plate is connected to the swing mechanism; one end of the vacuum suction cup is connected to the gas source through a gas pipeline, and a vacuum generator is installed on the gas pipeline, and the other end passes through the plate body and contacts with the sheet-like intermediate blank formed after slicing, and the sheet-like intermediate blank is fixed by the negative pressure in the pipeline.

[0023] Furthermore, the fully automatic processing system also includes a remote operation control system for remotely controlling the slicing system, the operation system and the sample preparation system to complete the preparation of dumbbell-shaped specimens and strip-shaped specimens.

[0024] Furthermore, the remote operation control system is located in the control area, the control slicing system, the operation system and the sample preparation system are located in the operation area, and the operation area and the control area are physically isolated.

[0025] A remote-controlled fully-automatic processing system for composite solid propellant test specimens provided by the present invention has the following beneficial effects:

[0026] (1) The remote-controlled fully-automatic processing system for composite solid propellant test samples provided by the present invention is provided with two parts: an operation area and a control area. The operation area realizes the production and processing of samples; the control area is used to remotely control the operation area, input response sample preparation instructions to the operation area and monitor the workflow of the operation area; the operation area and the control area are remotely physically isolated and connected by optical fiber, thereby realizing remote-controlled fully-automatic processing of composite solid propellant test samples, eliminating the safety hazards brought to operators by the propellant sample preparation process, and greatly improving the inherent safety of sample preparation.

[0027] (2) The remote-controlled fully automatic processing system for composite solid propellant test specimens provided by the present invention can simultaneously realize the production and processing of dumbbell-shaped specimens for mechanical property testing and strip-shaped specimens for static burning rate testing through the design of the sample preparation system.

[0028] (3) The remote-controlled fully automatic processing system for composite solid propellant test specimens provided by the present invention controls a fully automatic pill cutter through a remote operation control system. It is only necessary to input information such as specimen size, size, and quantity into the operating system to realize the production and processing of specimens of different types and sizes. BRIEF DESCRIPTION OF THE DRAWINGS

[0029] Figure 1 The conventional preparation process for propellant dumbbell specimens;

[0030] Figure 2 It is the traditional preparation process of propellant strip specimen;

[0031] Figure 3 It is the overall schematic diagram of the fully automatic medicine cutting machine;

[0032] Figure 4 It is a structural diagram of the slicing system;

[0033] Figure 5 It is a structural diagram of the operating system;

[0034] Figure 6 This is a schematic diagram of the sample preparation system. DETAILED DESCRIPTION

[0035] The following detailed description of the present invention will make the features and advantages of the present invention more clear and explicit.

[0036] The word “exemplary” is used exclusively herein to mean “serving as an example, example, or illustration.” Any embodiment described herein as “exemplary” is not necessarily to be construed as preferred or advantageous over other embodiments.

[0037] The invention provides a remote-controlled fully-automatic processing system for composite solid propellant test samples, which comprises two parts: an operation area and a control area. The operation area can realize the production and processing of dumbbell-shaped samples for composite solid propellant mechanical property testing and strip-shaped samples of different sizes for static burning rate testing; the control area is used to remotely control the operation area, input corresponding sample preparation instructions to the operation area, and monitor the work flow of the operation area; the operation area and the control area are remotely physically isolated and connected through optical fiber, thereby realizing remote-controlled fully-automatic processing of composite solid propellant test samples, eliminating the potential safety hazards to operators in the propellant sample preparation process, and greatly improving the inherent safety of sample preparation.

[0038] like Figure 3 As shown, a composite solid propellant sample fully automatic cutting machine is placed on a supporting surface 5 of a supporting platform 4 (such as a supporting cabinet or the ground) in the working area, and mainly includes a slicing system 1, an operating system 2 and a sample preparation system 3.

[0039] like Figure 4 As shown, the slicing system 1 includes: a gate knife 6, a first vertical guide rail 7, a first driving mechanism 81 (such as a cylinder or an explosion-proof motor), a support frame 9, a billet baffle 10, a second driving mechanism 82 (such as a cylinder or an explosion-proof motor), a propellant placement area 11 (a propellant billet is placed at the position marked 11) and a first horizontal guide rail 12; the support frame 9 is fixed on the support surface 5, and the first vertical guide rail 7 is embedded and fixed on one side of the support frame 9, facing the transfer system 2; the gate knife 6 is connected to the first vertical guide rail 7 and can move vertically up and down along the first vertical guide rail 7 to cut the composite solid propellant billet. piece; a driving mechanism 81 (such as a cylinder or an explosion-proof motor) is fixed to the top of the support frame 9, connected to the gate knife 6, and serves as a power source for moving the gate knife 6; a first horizontal guide rail 12 is fixed on the support surface 5, and a billet baffle 10 is connected to the first horizontal guide rail 12, and can move along the first horizontal guide rail 12 to push the composite solid propellant square billet toward the gate knife for stepping operation; a second driving mechanism 82 (such as a cylinder or an explosion-proof motor) is connected to the billet baffle 10, and serves as a power source for the billet baffle 10; the area surrounded by the support frame 9, the billet baffle 10, and the first horizontal guide rail 12 is the propellant placement area 11.

[0040] Preferably, the blank baffle 10 is a suction cup baffle, and a plurality of vacuum suction cups such as a double-layer accordion-type industrial vacuum suction cup are fixed on the plate body. One end of the vacuum suction cup is connected to the gas source through a gas pipeline, and a vacuum generator is installed on the gas pipeline. The other end passes through a prefabricated hole on the plate body (the end is flush with the plate body or protrudes from the plate body, and preferably the end is flush with the plate body), contacts with the composite solid propellant square blank to be cut, and fixes the composite solid propellant square blank through negative pressure adsorption in the pipeline.

[0041] The main function of the slicing system 1 is to cut the composite solid propellant square billet into sheet-like intermediate billets. The thickness of the sheet-like intermediate billet is set by the operator in the control area through the program in the operating system. During operation, the composite solid propellant square billet is placed in the propellant placement area 11. The operator leaves the working area and operates the control system in the control area. After selecting the corresponding sample shape (dumbbell-shaped sample or strip-shaped sample), the size, quantity and other information of the required sample are entered in the corresponding window. After confirming the start, the second driving mechanism 82 (such as a cylinder or an explosion-proof motor) works, and the billet baffle 10 moves along the first horizontal guide rail 12 to the tail end of the composite solid propellant square billet. When the billet baffle 10 is a suction cup baffle, the billet baffle 10 generates suction on the one hand to fix the composite solid propellant square billet, and on the other hand to push The composite solid propellant square blank moves forward in steps according to the sample thickness set in the program; the gate knife 6 works synchronously to slice the composite solid propellant square blank; the gate knife 6 and the blank baffle 10 step in a complementary manner, that is, the blank baffle 10 moves forward one step according to the sample thickness set in the program and then stops, and at the same time the gate knife 6 moves downward to complete the slicing; the gate knife 6 is lifted and reset, and the blank baffle 10 continues to move forward one step according to the sample thickness set in the program, and then the cycle is continued until the number set in the program is completed; the accuracy of the composite solid propellant sheet intermediate blanks of different thickness sizes is ensured by the first horizontal guide rail 12 and the second drive mechanism 82.

[0042] like Figure 5As shown, the operation system includes: a first transfer guide rail 131, a third driving mechanism 83 (such as a cylinder or an explosion-proof motor), a second transfer guide rail 132, a fourth driving mechanism 84 (such as a cylinder or an explosion-proof motor), a transfer mechanism 14, a swinging mechanism 15 and a transfer suction cup 16; the second transfer guide rail 132 is embedded in the first transfer guide rail 131, the transfer mechanism 14 is embedded in the second transfer guide rail 132, the swinging mechanism 15 is fixed on the transfer mechanism 14, and the transfer suction cup 16 is connected to the swinging mechanism 15, so as to realize the overall movement of the second transfer guide rail 132+transfer mechanism 14+swinging mechanism 15+transfer suction cup 16 along the first transfer guide rail 131, and the transfer mechanism 14+swinging mechanism 15+transfer suction cup 16 The transport suction cup 16 moves along the second transfer rail 132 as a whole; the fourth drive mechanism 84 (such as a cylinder or an explosion-proof motor) is fixed on the second transfer rail 132, and serves as a power source for the transfer mechanism 14 + swing mechanism 15 + transfer suction cup 16 to move up and down in the second transfer rail 132 as a whole; the first transfer rail 131 is fixed on the support surface 5; the third drive mechanism 83 (such as a cylinder or an explosion-proof motor) is fixed on the first transfer rail 131, and serves as a power source for the second transfer rail 132 + transfer mechanism 14 + swing mechanism 15 + transfer suction cup 16 to move as a whole; the swing mechanism 15 serves as a power source for the transfer suction cup 16, driving the transfer suction cup 16 in the horizontal-vertical direction (0~90 ○ The vertical sheet-shaped intermediate blank completed by the slicing system is converted into a horizontal state and placed on the sample preparation plane 24.

[0043] The swing mechanism 15 is a rotary cylinder, an explosion-proof motor or other driving mechanism with a rotating shaft, etc., which can drive the transfer suction cup 16 to swing back and forth in the horizontal and vertical directions.

[0044] The transfer suction cup 16 includes an adapter plate and multiple vacuum suction cups fixed on the adapter plate, such as a double-layer accordion-type industrial vacuum suction cup; the adapter plate plays a role of transfer and bearing, and is connected to the swing mechanism 15; one end of the vacuum suction cup is connected to the gas source through a gas pipeline, and a vacuum generator is installed on the gas pipeline, and the other end passes through the plate body (the end is flush with the plate body or protrudes from the plate body), contacts with the sheet-like intermediate blank formed after slicing, and fixes the sheet-like intermediate blank through the negative pressure in the pipeline.

[0045] The function of the operation system 2 is to transfer the sheet-shaped intermediate blanks completed by the slicing system 1 to the sample preparation system 3 . When the blank baffle 10 moves along the first horizontal guide rail 12 and pushes the composite solid propellant square blank to the bottom of the gate knife 6, the third driving mechanism 83 (such as a cylinder or an explosion-proof motor) works synchronously, and the second transfer guide rail 132 moves along the first transfer guide rail 131, driving the transfer mechanism 14+swing mechanism 15+transfer suction cup 16 in a vertical state to move to the vicinity of the gate knife 6; the fourth driving mechanism 84 (such as a cylinder or an explosion-proof motor) works to adjust the height of the transfer mechanism 14+swing mechanism 15+transfer suction cup 16 in a vertical state so that the transfer suction cup 16 is in close contact with the outside of the composite solid propellant square blank, limiting the position of the composite solid propellant square blank; when the gate knife 6 completes the sample slicing, the transfer suction cup 16 works to generate suction to fix the sheet-like intermediate blank completed by the slicing system on the transfer suction cup 16; the swing mechanism 15 works to rotate the transfer suction cup 16 together with the sheet-like intermediate blank clockwise by 90 ○ third drive mechanism 83 (such as a cylinder or an explosion-proof motor) drives the second transfer rail 132 + transfer mechanism 14 + swing mechanism 15 + transfer suction cup 16 + sheet-like intermediate blank to move as a whole, so as to transfer the sheet-like intermediate blank to the sample preparation system 3.

[0046] The operation system may also include a mechanical arm device, which transfers the sheet-shaped intermediate blanks completed by the slicing system 1 to the sample preparation system 3 under the control of the remote operation control system in the control area. Of course, other structural arrangements may also be used, which will not be exhaustively listed here.

[0047] like Figure 6 As shown, the sample preparation system 3 includes: a fifth drive mechanism 85 (such as a cylinder or an explosion-proof motor), a sample unloading mechanism 17, a dumbbell-shaped tool 18, a sixth drive mechanism 86 (such as a cylinder or an explosion-proof motor), a seventh drive mechanism 87 (such as a cylinder or an explosion-proof motor), a vertical guide rail table 19, a dumbbell-shaped tool holder 201, a blade 21, a blade holder 202, an eighth drive mechanism 88 (such as a cylinder or an explosion-proof motor), a push plate 22, a second horizontal guide rail 231, a sample preparation plane 24, a third horizontal guide rail 232, a second vertical guide rail 251, a third vertical guide rail 252, and a sample collection box 26.

[0048] The dumbbell-shaped tool 18 is fixed on the dumbbell-shaped tool holder 201, and the dumbbell-shaped tool holder 201 is embedded in the second vertical guide rail 251, so that the dumbbell-shaped tool 18 can move up and down along the second vertical guide rail 251, and the second vertical guide rail 251 is fixed to the support surface 5. The sixth drive mechanism 86 (such as a cylinder or an explosion-proof motor) is fixed on the vertical guide rail table 19, which serves as a power source for the dumbbell-shaped tool 18 to move up and down; the blade 21 is fixed on the blade holder 202, and the blade holder 202 is embedded in the third vertical guide rail 252, so that the blade 21 can move up and down along the third vertical guide rail 252, and the third vertical guide rail 252 is fixed to the support surface 5. The seventh drive mechanism 87 (such as a cylinder or an explosion-proof motor) is fixed on the vertical guide rail table 19, which serves as a power source for the blade 21 to move up and down; dumbbell-shaped tool 18+dumbbell-shaped tool The tool holder 201+second vertical guide rail 251+sixth drive mechanism 86 as a whole and the blade 21+blade holder 202+third vertical guide rail 252+seventh drive mechanism 87 as a whole are parallel and fixed to each other; the second vertical guide rail 251 and the third vertical guide rail 252 each include two parallel guide posts, the second horizontal guide rail 231 is located on the inner side of the two guide posts of the second vertical guide rail 251 and the third vertical guide rail 252, crosses directly below the dumbbell-shaped tool 18 and the blade 21 and is fixed on the support surface 5; the sample preparation plane 24 is connected to the second horizontal guide rail 231, on which the sheet-like intermediate blank is carried, and lateral movement is achieved directly below the dumbbell-shaped tool 18 and the blade 21; the fifth drive mechanism 85 (such as a cylinder or an explosion-proof motor) is connected to the sample preparation plane 24, serving as a power source for the horizontal movement of the sample preparation plane 24.

[0049] The eighth driving mechanism 88 (such as a cylinder or an explosion-proof motor) is fixed on the sample preparation plane 24, connected to the push plate 22, and serves as a power source for the horizontal movement of the push plate 22; the push plate 22 is opposite to the positioning protrusion (located inside the plate or at the edge of the plate) on the sample preparation plane, and when preparing samples, the sheet-like intermediate blank is pushed to the positioning protrusion of the sample preparation plane, and the positioning protrusion of the sample preparation plane is used as a mark position for positioning the sheet-like intermediate blank, or after the sheet-like intermediate blank is pushed to the positioning protrusion of the sample preparation plane, it continues to press against the sheet-like intermediate blank, and fixes the sample together with the positioning protrusion of the sample preparation plane. Furthermore, a third horizontal guide rail 232 is also fixed on the sample preparation plane 24 to guide the movement of the push plate 22.

[0050] The sample unloading mechanism 17 includes a frame, a ninth driving mechanism (such as a cylinder or an explosion-proof motor) and a unloading piece. The frame is arranged close to the sample preparation plane 24, the ninth driving mechanism is fixed on the frame, and the unloading piece is fixed on the ninth driving mechanism. Driven by the ninth driving mechanism, horizontal movement (such as horizontal movement perpendicular to the direction of the second horizontal guide rail 231) is achieved to deliver the sample prepared on the sample preparation plane 24 (dumbbell-shaped sample for mechanical properties test and strip-shaped sample for static burning rate test) into the sample collection box 26.

[0051] The function of the sample preparation system 3 is to prepare the sheet-like intermediate blanks operated by the operation system 2 according to the size requirements set by the program. The operation system 2 operates the sheet-like intermediate blanks to the sample preparation plane 24, and the eighth drive mechanism 88 (such as a cylinder or an explosion-proof motor) works to drive the push plate 22 to move to the placement position of the sheet-like intermediate blanks and fix the sheet-like intermediate blanks. The fifth drive mechanism 85 (such as a cylinder or an explosion-proof motor) works to drive the sample preparation plane 24 as a whole to move along the second horizontal guide rail 231 and accurately position it below the dumbbell-shaped tool 18 or the blade 21. If the program sets a dumbbell-shaped sample, it moves to the bottom of the dumbbell-shaped tool 18; if the program sets a strip-shaped sample, it moves to the bottom of the blade 21. Taking the strip sample as an example, the second horizontal guide rail 231 moves precisely according to the sample size set by the program, and each time it moves, the blade 21 works downward once to complete the sample preparation; after completion, the second horizontal guide rail 231 continues to move the distance set by the program, and the blade 21 continues to work, and the process is repeated in sequence until the number of samples prepared reaches the number set by the program and then stops; after the sample preparation is completed, the fifth driving mechanism 85 drives the sample preparation plane 24 to move to the sample unloading mechanism 17, and the unloading part of the sample unloading mechanism 17 pushes the sample and waste together and puts them into the sample collection box 26 for temporary storage.

[0052] After the knife 6 in the slicing system 1 moves downward once to complete a slice, the knife 6 is reset, and the operating system 2 works at the same time, and the cut sheet-like intermediate blank is transferred to the sample preparation system 3 by the coordinated work of the transfer suction cup 16, the swing mechanism 15, and the transfer mechanism 14; then, the sample preparation system 3 starts to work and prepare samples; at the same time, the operating system 2 is reset, and the knife 6 in the slicing system 1 starts to work again, entering the next cycle, and the two systems work synchronously.

[0053] The first drive mechanism 81, the second drive mechanism 82, the third drive mechanism 83, the fourth drive mechanism 84, the fifth drive mechanism 85, the sixth drive mechanism 86, the seventh drive mechanism 87, the eighth drive mechanism 88 and the ninth drive mechanism can be cylinders or explosion-proof motors or other drive devices; when the cylinder is selected, the movement of the driven mechanism is driven by the extension and contraction of the piston rod; when the explosion-proof motor is selected, the rotation of the motor shaft is converted into the linear motion of the driven member through structural matching, such as the sixth drive mechanism 86 is an explosion-proof motor, the motor shaft (if it is equipped with a reducer, it is the output shaft of the reducer) is connected with a threaded rod, a threaded hole is provided on the dumbbell-shaped tool holder 201, the threaded rod cooperates with the threaded hole, and the explosion-proof motor runs to convert the rotation of the motor shaft into the linear motion of the dumbbell-shaped tool holder 201 along the second vertical guide rail 251. Of course, the above examples are only exemplary and are not limited to the above methods.

[0054] A remote operation control system is set up in the control area and matched with the full-automatic medicine cutter. It is used to remotely control the full-automatic medicine cutter and issue various operation instructions to the full-automatic medicine cutter, including sample preparation quantity, shape, size and other information, and monitor and observe the operation of the full-automatic medicine cutter. The working condition of the full-automatic medicine cutter is observed in real time. When the operation control system shows that the sample preparation is completed and the sample preparation operation is completed as observed in the monitoring video, the operator enters the operation area and takes out the sample collection box.

[0055] The present invention has been described in detail above in conjunction with specific implementations and exemplary examples, but these descriptions cannot be understood as limiting the present invention. Those skilled in the art understand that, without departing from the spirit and scope of the present invention, a variety of equivalent substitutions, modifications or improvements may be made to the technical solution of the present invention and its implementation methods, all of which fall within the scope of the present invention. The scope of protection of the present invention shall be subject to the attached claims.

[0056] The contents not described in detail in the specification of the present invention belong to the common knowledge of those skilled in the art.

Claims

1. A remote-controlled fully automatic processing system for composite solid propellant test specimens, characterized in that: include: Slicing system, which cuts the composite solid propellant square billet into sheet-shaped intermediate billets; The operation system transfers the sheet-shaped intermediate blanks completed by the slicing system to the sample preparation system; The sample preparation system prepares samples of the sheet-shaped intermediate blanks operated by the operating system; The sample preparation system comprises a fifth driving mechanism (85), a dumbbell-shaped cutter (18), a sixth driving mechanism (86), a seventh driving mechanism (87), a dumbbell-shaped cutter holder (201), a blade (21), a blade holder (202), a second horizontal guide rail (231), a sample preparation plane (24), a second vertical guide rail (251) and a third vertical guide rail (252); The dumbbell-shaped tool (18) is fixed on a dumbbell-shaped tool holder (201), the dumbbell-shaped tool holder (201) is embedded in a second vertical guide rail (251), and the dumbbell-shaped tool (18) moves up and down along the second vertical guide rail (251), the second vertical guide rail (251) is fixed on a support surface (5) of a support platform, and a sixth driving mechanism (86) is connected to the dumbbell-shaped tool holder (201) and serves as a power source for the dumbbell-shaped tool (18) to move up and down; the blade (21) is fixed on a blade holder (202), the blade holder (202) is embedded in a third vertical guide rail (252), and the blade (21) moves up and down along the third vertical guide rail (252), the third vertical guide rail (252) is fixed on the support surface (5) of the support platform; and a seventh driving mechanism (87) is connected to the blade holder (202) and serves as a power source for the blade (21) to move up and down; the second horizontal guide rail (231) crosses the dumbbell-shaped tool (18) and the blade (21) and is fixed on the support surface (5); the sample preparation plane (24) is connected to the second horizontal guide rail (231), on which the sheet-shaped intermediate blank is carried, and moves horizontally directly below the dumbbell-shaped tool (18) and the blade (21); the fifth driving mechanism (85) is connected to the sample preparation plane (24) and serves as a power source for the horizontal movement of the sample preparation plane (24), driving the sheet-shaped intermediate blank on the sample preparation plane (24) to move to the bottom of the dumbbell-shaped tool (18) or the blade (21), so that the dumbbell-shaped sample is prepared by the dumbbell-shaped tool (18), and the strip-shaped sample is prepared by the blade (21).

2. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 1 is characterized in that: The sample preparation system further comprises an eighth driving mechanism (88) and a push plate (22) arranged on the sample preparation plane (24); the eighth driving mechanism (88) is connected to the push plate (22) and serves as a power source for horizontal movement of the suction cup baffle (22); the push plate (22) pushes the sheet-shaped intermediate blank to a fixed position on the sample preparation plane during sample preparation, so that the dumbbell-shaped tool (18) or the blade (21) starts sample preparation at the fixed position on the sample preparation plane.

3. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 2, characterized in that: The sample preparation plane (24) is provided with a positioning protrusion, and the push plate (22) is opposite to the positioning protrusion. When preparing samples, the sheet-like intermediate blank is pushed to the positioning protrusion of the sample preparation plane, and the positioning protrusion of the sample preparation plane is used as a mark position for positioning the sheet-like intermediate blank. Alternatively, after the sheet-like intermediate blank is pushed to the positioning protrusion of the sample preparation plane, the sheet-like intermediate blank is continued to be pressed against the positioning protrusion of the sample preparation plane, and the sample is fixed together with the positioning protrusion of the sample preparation plane.

4. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 1, characterized in that: The sample preparation system further comprises a sample unloading mechanism (17), which comprises a frame, a ninth driving mechanism and a unloading member. The frame is arranged close to the sample preparation plane (24), the ninth driving mechanism is fixed on the frame, and the unloading member is fixed on the ninth driving mechanism. The unloading member moves horizontally under the drive of the ninth driving mechanism to deliver the sample prepared on the sample preparation plane (24) into the sample collection box.

5. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 1, characterized in that: The slicing system comprises a gate knife (6), a first vertical guide rail (7), a first driving mechanism (81), a support frame (9), a billet baffle (10), a second driving mechanism (82) and a first horizontal guide rail (12); the support frame (9) is fixed on a support surface (5) of a support platform, the first vertical guide rail (7) is embedded in and fixed on one side of the support frame (9) and faces the transfer system; the gate knife (6) is connected to the first vertical guide rail (7) and moves vertically up and down along the first vertical guide rail (7) to slice the composite solid propellant square billet; the driving mechanism ( 81) is connected to the gate knife (6) and serves as a power source for moving the gate knife (6); the first horizontal guide rail (12) is fixed on the support surface (5), the billet baffle (10) is connected to the first horizontal guide rail (12), moves along the first horizontal guide rail (12), and pushes the composite solid propellant square billet to move stepwise toward the gate knife; the second drive mechanism (82) is connected to the billet baffle (10) and serves as a power source for the billet baffle (10); the area surrounded by the support frame (9), the billet baffle (10) and the first horizontal guide rail (12) is the propellant placement area (11).

6. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 5, characterized in that: The blank baffle (10) is a suction cup baffle, and a plurality of vacuum suction cups are fixed on the plate body. One end of the vacuum suction cup is connected to a gas source through a gas pipeline, and a vacuum generator is installed on the gas pipeline. The other end of the vacuum suction cup passes through a prefabricated hole on the plate body and contacts with the composite solid propellant square blank to be cut, and fixes the composite solid propellant square blank by adsorbing it through the negative pressure in the pipeline.

7. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 1, characterized in that: The operation system comprises a first transfer guide rail (131), a third driving mechanism (83), a second transfer guide rail (132), a fourth driving mechanism (84), a transfer mechanism (14), a swing mechanism (15) and a transfer suction cup (16); the second transfer guide rail (132) is embedded in the first transfer guide rail (131), the transfer mechanism (14) is embedded in the second transfer guide rail (132), the swing mechanism (15) is fixed on the transfer mechanism (14), and the transfer suction cup (16) is connected to the swing mechanism (15), so that the second transfer guide rail (132), the transfer mechanism (14), the swing mechanism (15) and the transfer suction cup (16) can move along the first transfer guide rail (131) as a whole, and the transfer mechanism (14), the swing mechanism (15) and the transfer suction cup (16) can move along the first transfer guide rail (131) as a whole. The fourth driving mechanism (84) is fixed on the second transfer rail (132) and serves as a power source for the overall movement of the transfer mechanism (14), the swing mechanism (15) and the transfer suction cup (16); the first transfer rail (131) is fixed on the support surface (5); the third driving mechanism (83) is fixed on the first transfer rail (131) and serves as a power source for the overall movement of the second transfer rail (132), the transfer mechanism (14), the swing mechanism (15) and the transfer suction cup (16); the swing mechanism (15) serves as a power source for the transfer suction cup (16), driving the transfer suction cup (16) to reciprocate in the horizontal-vertical direction, converting the vertical sheet-shaped intermediate blank completed by the slicing system into a horizontal state, and placing it on the sample preparation plane (24).

8. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 7, characterized in that: The transfer suction cup (16) comprises an adapter plate and a plurality of vacuum suction cups fixed on the adapter plate; the adapter plate is connected to the swing mechanism (15); one end of the vacuum suction cup is connected to the gas source via a gas pipeline, and a vacuum generator is installed on the gas pipeline, and the other end passes through the plate body and contacts with the sheet-like intermediate blank formed after slicing, and the sheet-like intermediate blank is fixed by the negative pressure in the pipeline.

9. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 1, characterized in that: The fully automatic processing system also includes a remote operation control system for remotely controlling a slicing system, a running system and a sample preparation system to complete the preparation of dumbbell-shaped specimens and strip-shaped specimens.

10. The remote-controlled fully automatic processing system for composite solid propellant test specimens according to claim 9, characterized in that: The remote operation control system is located in the control area, the control slicing system, the operation system and the sample preparation system are located in the operation area, and the operation area and the control area are physically isolated.