Unattended vehicle-mounted photoelectric measurement equipment activity cabin capable of being automatically unfolded and folded
Patent Information
- Application Number
- CN202411264297.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-10
- Publication Date
- 2025-01-28
AI Technical Summary
The existing vehicle-mounted photoelectric measurement equipment needs to be manually opened and pushed to a fixed position when used in the field, and the movable compartment cannot be closed in time, resulting in electrical system short circuits, optical lenses falling into dust or corrosion, and mechanical component cards in sudden weather. Hysteresis or rust seriously affects service life and measurement tasks.
Designed a type of unmanned car -car photoelectric measurement equipment compartment that can be automatically carried out, and launched the withdrawal control system, the electric push -pull component of the activity compartment, the left -right door electric rotation component, and the door lock component through the activity capsule The automation of the cabin is unfolding and withdrawal.
The degree of automation has been improved, and it can quickly expand and withdraw the activity compartment in the absence of unattended situations, adapt to the emergency weather environment, protect the safety of optoelectronic measurement equipment, extend the service life, and improve the rapid response ability of the equipment.
Smart Images

Figure CN119370203A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to a vehicle-mounted photoelectric measurement cabin, in particular to an unattended vehicle-mounted photoelectric measurement equipment movable cabin which can be automatically unfolded and retracted. Background Art
[0002] Photoelectric measurement equipment is a measurement equipment that can quickly capture targets, accurately track targets, transmit real-time images, and replay images in modern shooting ranges. It is mainly used to record test parameters such as target motion trajectory data, flight attitude, and radiation characteristics, and is widely used in aviation, aerospace, and test shooting ranges. After the 1990s, photoelectric measurement equipment has mostly adopted a vehicle-mounted structure, that is, the vehicle body is used as a carrier and equipped with photoelectric instruments to carry out measurement work.
[0003] There are two ways to use vehicle-mounted photoelectric measurement equipment. The first way is vehicle-mounted ground measurement, that is, when performing a task, the photoelectric measurement equipment is loaded on a vehicle and transported to the measurement point. After unloading, it is installed on a pre-prepared foundation ring. After the task is completed, it is reloaded, and the equipment is transported on a vehicle, which improves the utilization rate of the equipment. However, the usage mode is still fixed on the foundation and has not gotten rid of the fixed point restriction. The other way is vehicle-mounted non-ground measurement, that is, the support platform is detached from elastic links such as tires through outrigger support and other methods. The instrument works directly on the support platform, and the equipment is leveled, positioned and oriented without landing before measurement is carried out. Its strong mobility can realize real-time capture, tracking and measurement at different times and places, rapid deployment and rapid withdrawal, eliminating the need for stationing points, and returning immediately after completing the task. It significantly improves the rapid response capability of photoelectric instruments and has become the most important method of use at present.
[0004] In certain specific measurement conditions, such as live recording of spacecraft launches, target characteristic measurements, and target event capture under high electromagnetic radiation, the measurement equipment may cause harm to the on-board operator. In this case, a remote unattended method is required to operate the optoelectronic measurement equipment. However, when the existing on-board measurement equipment, especially the mobile cabin, is used in the field, it needs to be manually opened and pushed and pulled to the designated position of the fixed cabin to be fixed, so that the equipment can be fully exposed to the external environment before the test task can be carried out. When encountering sudden weather environments such as sandstorms or rainy days, the unattended optoelectronic measurement equipment exposed to the environment is prone to electrical system short circuits, dust or corrosion of optical lenses, and mechanical component jamming or rusting due to the inability to close the mobile cabin in time, which seriously affects the service life of the equipment and even causes equipment failure. The losses in measurement tasks and economy are immeasurable. Therefore, it is urgent to carry out the optimization design of the mobile cabin under unattended working conditions in the field, so that when encountering sudden weather such as sandstorms, thunderstorms, etc., the withdrawal work can be completed quickly, thereby protecting the safety of the optoelectronic measurement equipment. Summary of the invention
[0005] The main purpose of the present invention is to solve the problem that the existing vehicle-mounted photoelectric measurement equipment needs to be manually opened and pushed and pulled to the designated position of the fixed cabin for fixing when used in the field, so that the equipment can only be carried out after it is fully exposed to the external environment, and the movable cabin cannot be closed in time when performing unattended tasks in the field. By providing an unattended vehicle-mounted photoelectric measurement equipment movable cabin that can be automatically deployed and retracted.
[0006] In order to achieve the above-mentioned invention object, the present invention provides the following technical solutions:
[0007] An unattended vehicle-mounted photoelectric measuring equipment movable cabin that can be automatically deployed and withdrawn comprises a movable cabin deployment and withdrawal control system, a movable cabin, a fixed cabin, a vehicle-mounted chassis and a photoelectric measuring device, wherein the fixed cabin is fixedly mounted on the vehicle-mounted chassis, the photoelectric measuring device is arranged on the vehicle-mounted chassis and is located between the fixed cabin and the movable cabin, and the movable cabin deployment and withdrawal control system is mounted on the vehicle-mounted chassis, and the special features thereof are:
[0008] The movable cabin is composed of a top wall, a left wall, a left cabin door, a right cabin door, and a right wall; wherein the left cabin door and the right cabin door are hinged on the left wall and the right wall respectively through an upper and a lower set of cabin door rotating hinges; movable cabin push-pull guide rail assemblies are respectively arranged between the left wall and the fixed cabin of the movable cabin, and between the right wall and the fixed cabin; a movable cabin electric push-pull assembly is arranged on the inner side of the left wall of the fixed cabin, and a movable cabin auxiliary guide assembly is arranged on the inner side of the right wall; left and right cabin door electric rotating assemblies are respectively installed between the left cabin door and the left wall of the movable cabin, and between the right cabin door and the right wall, and both of the left and right cabin door electric rotating assemblies are installed on the inner side of the cabin body; the movable cabin electric push-pull assembly and the left and right cabin door electric rotating assemblies are electrically controlled by a movable cabin deployment and retraction control system; the movable cabin deployment and retraction control system is controlled by a remote control console.
[0009] Furthermore, the two groups of movable cabin push-pull guide rail assemblies include guide rails, ball support frames, ball retainers and balls; wherein the two groups of guide rails are respectively installed on the inner sides of the left wall and the right wall, the two groups of ball retainers are respectively fixed in the grooves of the guide rails, and the two ball support frames are respectively fixed on the two outer walls of the fixed cabin; the two ball support frames are respectively arranged in the two groups of ball retainers, and the upper and lower walls of each ball support frame are respectively provided with an arc-shaped groove matching the size of the ball; the corresponding positions on the inner sides of the guide rails are also respectively provided with arc-shaped grooves of the same shape as the arc-shaped grooves on the ball support frames; a plurality of balls are respectively arranged on the ball retainers, and cooperate with the semicircular grooves arranged on the guide rails and the ball support frames, so that the movable cabin can slide back and forth.
[0010] Furthermore, each of the left and right door electric rotation components includes a revolving door motor, a revolving door reducer, a revolving door reducer mounting seat, a transmission connecting rod, a rotating hinge, a slide rail, a limit block, a photoelectric switch A, a transmission key, a spherical locking pin and a spherical rotating pin; wherein, the two revolving door reducer mounting seats are respectively mounted on the left wall and the right wall, and are L-shaped in structure, with their vertical parts correspondingly mounted on the left wall or the right wall, and their horizontal parts are fixedly connected to the revolving door reducer, the revolving door motor is fixedly connected to the revolving door reducer, and its output is connected to the input of the revolving door reducer; the revolving door motor is electrically controlled by the movable cabin deployment and retraction control system; the horizontal part of the revolving door reducer mounting seat is provided with a center hole, and the output shaft of the revolving door reducer passes through the center hole; a key slot is also provided on the output shaft of the revolving door reducer, and the transmission key is installed in the key slot; the output shaft of the revolving door reducer cooperates with the transmission connecting rod using the key slot and the transmission key to realize the dynamic output of the revolving door motor. The transmission connecting rod is a U-shaped structure, and its U-shaped mouth faces the corresponding left door or right door, and a center hole is provided at both ends, one end of which is sleeved on the output shaft of the revolving door reducer, and the other end is hinged with the rotary hinge through a pin shaft; the cross section of the slide rail is a T-shaped structure, and is fixed to the door by screws, and a T-shaped slide groove corresponding to it is designed on the base of the rotary hinge, and the slide rail cooperates with the T-shaped slide groove so that the rotary hinge can slide on the slide rail; limit stops are respectively installed at both ends of the slide rail, and a light shielding sheet is designed on the limit stop far from the left wall or the right wall, and a photoelectric switch A is installed on the upper end of the base of the rotary hinge, and a photoelectric switch gasket A is provided below the photoelectric switch A. When the left door or the right door is opened, the light shielding sheet on the limit stop blocks the photoelectric switch A, thereby realizing the closed limit of the left door or the right door.
[0011] Furthermore, a reducer transmission connecting rod pressure ring is also provided above the transmission connecting rod, and a screw is passed through the reducer transmission connecting rod pressure ring to fix the transmission connecting rod on the output shaft of the revolving door reducer to prevent it from moving up and down; the other end of the transmission connecting rod is hinged to the rotating hinge through a pin shaft, and the specific structure is as follows: two support ears are provided on the rotating hinge, and the two support ears are provided with corresponding center holes, the spherical locking pin is inserted from the lower center hole, and the spherical rotating pin is inserted from the upper center hole, the stud at the end of the spherical locking pin cooperates with the screw hole at the end of the spherical rotating pin to hinge the other end of the transmission connecting rod on the rotating hinge; the spherical locking pin, the spherical rotating pin and the other end of the transmission connecting rod are connected as a whole, so that the left door and the right door can rotate flexibly relative to the transmission connecting rod.
[0012] Furthermore, two anti-loosening locking springs are arranged between the spherical locking pin and the spherical rotating pin to prevent the connection between the spherical locking pin and the spherical rotating pin from loosening, causing the left door and the right door to get stuck during the opening or closing rotation process.
[0013] Furthermore, the movable cabin electric push-pull assembly includes a push-pull cabin motor, a push-pull cabin reducer, a push-pull cabin reducer mounting seat, a coupling, a transmission screw mounting seat, a photoelectric switch seat, a photoelectric switch B, a transmission screw, a transmission nut, an electric limit shading sheet, a laser ranging sensor support, a laser ranging sensor, a bearing outer pressure ring, an angular contact ball bearing group and a bearing inner pressure ring; wherein the push-pull cabin reducer mounting seat is installed on the inner side of the left wall of the fixed cabin, and the push-pull cabin reducer is installed on the push-pull cabin reducer mounting seat by screws after being connected to the push-pull cabin motor; the push-pull cabin motor is mounted by the movable cabin expansion The opening, retraction and collection control system is electrically controlled; the push-pull cabin reducer is fixedly connected to one end of the coupling, and the other end of the coupling is fixedly connected to one end of the transmission screw; the transmission screw mounting seat, the bearing outer pressure ring, the angular contact ball bearing group and the bearing inner pressure ring together constitute the support shaft system of the transmission screw, and the transmission screw is installed on the inner side of the left wall of the fixed cabin through the support shaft system; wherein, a shaft shoulder is designed on the transmission screw, and two angular contact ball bearing groups are installed on the transmission screw mounting seat in a back-to-back manner and abut against the shaft shoulder on the transmission screw; two shafts are respectively arranged on the outer sides of the two angular contact ball bearing groups. The outer pressure ring is used to axially compress and fix the angular contact ball bearing group; two groups of bearing inner pressure rings are also installed on the inner side of the angular contact ball bearing group, which can prevent the angular contact ball bearing group from loosening while pre-tightening it; the transmission nut is installed on the left wall and cooperates with the transmission screw to convert the rotational motion output by the push-pull cabin motor into the linear motion of the movable cabin; the transmission nut is also provided with two electric limit shading plates; photoelectric switches B are installed on the two transmission screw mounting seats through the photoelectric switch seat and the photoelectric switch gasket B arranged thereon; during the movement of the movable cabin, when the electric limit shading plate blocks the When the photoelectric switch B is on, the photoelectric switch B transmits the photoelectric signal to the push-pull cabin motor, thereby controlling the limit of the push-out and closing of the movable cabin; the laser ranging sensor is arranged on the left wall of the movable cabin through the laser ranging sensor support, and the laser ranging sensor is arranged above the transmission screw mounting seat; during the movement of the movable cabin, the laser ranging sensor emits a laser signal to the side wall of the transmission nut, and uses the side wall of the transmission nut to realize the reception of the laser signal echo, thereby determining the real-time movement position of the movable cabin, and the acquired position information can be used to determine the observation range that the photoelectric measuring equipment can achieve.
[0014] Furthermore, the auxiliary guide assembly of the movable cabin includes a bearing outer pressure ring, an angular contact ball bearing group, a bearing inner pressure ring, a guide rod, a guide piece and a guide mounting seat; wherein, the guide mounting seat, the bearing outer pressure ring, the angular contact ball bearing group and the bearing inner pressure ring together constitute the support shaft system of the guide rod, and the guide rod is installed on the inner side of the right wall of the fixed cabin; a shaft shoulder is designed on the transmission rod, and two angular contact ball bearing groups are installed on the guide mounting seat in a back-to-back manner and abut against the shaft shoulder on the guide rod; two bearing outer pressure rings are respectively arranged on the outer sides of the two angular contact ball bearing groups for axially pressing and fixing the angular contact ball bearing groups; two groups of bearing inner pressure rings are also installed on the inner side of the angular contact ball bearing group, which play a role in preventing loosening while pre-tightening the angular contact ball bearing group; the guide piece is installed on the right wall, and its inner wall cooperates with the guide rod; so that the movable cabin can be opened and closed stably.
[0015] Furthermore, door locking assemblies electrically controlled by the movable cabin deployment and retraction control system are installed at corresponding inner positions between the left cabin door and the top wall, between the right cabin door and the top wall, between the left cabin door and the fixed cabin, and between the right cabin door and the fixed cabin.
[0016] Further, the door locking assembly includes a brake mounting seat, a power-off lock brake stator, a brake spring, a power-off lock brake mover, a fixing pin and a fixing pin mounting seat; wherein, two brake mounting seats are mounted on the top wall, and the other two brake mounting seats are respectively mounted on the left door and the right door; four power-off lock brake stators are respectively mounted on four brake mounting seats by screws, and each of the power-off lock brake stators is electrically controlled by the mobile cabin deployment and retraction control system; each power-off lock brake stator is designed with 6 evenly distributed threaded holes, and a guide column is arranged at the center of the threaded hole; flanges with center holes are arranged at both ends of the brake spring, and the flange at the upper end of the brake spring is designed with external threads; four groups of fixing pin mounting seats are respectively mounted on the fixed cabin, the left door and the right door at positions corresponding to the brake mounting seats, and four groups of fixing pins are respectively mounted on the four groups of fixing pin mounting seats by screws; a center hole with a 45° chamfer is designed on the fixing pin, and a guide column with a 45° conical surface is designed on the power-off lock brake mover.
[0017] Furthermore, fixing pin mounting seats are respectively installed on the outer sides of the left wall and the right wall at positions corresponding to the power-loss lock brake movers on the opened left door and the right door, and fixing pins are installed on the seats by screws.
[0018] Furthermore, the six brake springs are installed on the outer side of the power-loss lock brake stator, which can improve the bending resistance of the power-loss lock brake rotor when it receives external force, and further enhance the reliability of the closing of the right door and the left door.
[0019] Compared with the prior art, the present invention has the following beneficial effects:
[0020] 1. High degree of automation: When the on-board photoelectric measurement equipment is powered on, the door locking assembly is first powered on to automatically release the closed state of the right and left doors. Secondly, the left and right door electric rotation assemblies use the power provided by the revolving door motor to realize the automatic opening of the right and left doors, and rely on the photoelectric signal to determine the final opening position, and then use the door locking assembly to fix the right and left doors in the open position, which can effectively prevent the right and left doors from shaking randomly due to wind load. Further, with the cooperation of the movable cabin auxiliary guide assembly and the movable cabin push-pull guide rail assembly, the movable cabin electric push-pull assembly uses the power provided by the push-pull cabin motor to realize the automatic opening of the square cabin, and relies on the photoelectric signal to determine the final opening position. It can be seen that the deployment action of the square cabin is all electrically operated, with a high degree of automation and no human participation. Similarly, the withdrawal action of the square cabin can be realized by electric control using the same logic. At the same time, the movable cabin electric push-pull assembly and the left and right door electric rotation assembly are designed with a travel limit structure relying on a photoelectric switch, which improves the safety of the automatic operation of the assembly.
[0021] 2. Strong adaptability to the working environment: In response to the unmanned equipment requirements mentioned by most shooting range users, the vehicle-mounted optoelectronic measurement equipment can automatically deploy and retract the activity cabin through remote control, which can conveniently realize the automatic deployment and retraction of the activity cabin. It can well cope with sudden weather conditions such as sandstorms or rainy days, and provide timely and effective protection for optoelectronic measurement equipment.
[0022] 3. Ability to work in rainy days without human supervision: The laser ranging sensor can obtain the position of the shelter in real time, and accurately calculate the deployment position of the optoelectronic measurement equipment in the shelter without rain according to the shape and position relationship between the shelter and the equipment. It can also calculate the azimuth and pitch angles that the shelter can observe in a semi-open state according to the acquired position information, thereby guiding the implementation of field observation tasks.
[0023] 4. Good performance: The push-pull guide rail assembly of the movable cabin achieves point-to-surface contact through the ball bearings to reduce the push-pull friction resistance of the movable cabin, effectively prevent the problem of jamming, and play a rough guiding role. At the same time, the auxiliary guide assembly of the movable cabin cooperates with the electric push-pull assembly of the movable cabin and the push-pull guide rail assembly of the movable cabin to play a precise guiding role, thereby ensuring the good performance of the push-pull of the square cabin. Furthermore, the left and right door electric rotation assemblies and the door locking assemblies cooperate to complete the opening, closing and locking functions of the left and right doors. The operating actions have a clear logical relationship, there are no risk points in the operation process, and the safety and reliability are high. BRIEF DESCRIPTION OF THE DRAWINGS
[0024] Figure 1 It is a schematic diagram of an embodiment of the present invention when the movable cabin is in a closed state;
[0025] Figure 2It is a schematic diagram of an embodiment of the present invention when the movable cabin is in an open state;
[0026] Figure 3 It is a schematic diagram of the three-dimensional structure of the movable cabin in an embodiment of the present invention;
[0027] Figure 4 This is a schematic diagram of the positions of the functional components of the mobile cabin in an embodiment of the present invention;
[0028] Figure 5 for Figure 4 A magnified view of a local position;
[0029] Figure 6 It is a schematic diagram of the assembly structure of the left and right door electric rotating components in an embodiment of the present invention;
[0030] Figure 7 for Figure 6 A cross-sectional view of the middle region A;
[0031] Figure 8 for Figure 6 A cross-sectional view of the middle region B;
[0032] Fig. 9 for Figure 6 A cross-sectional view of the middle region C;
[0033] Fig.10 It is a schematic diagram of the position of the electric push-pull assembly of the movable cabin in an embodiment of the present invention;
[0034] Fig.11 It is a schematic diagram of the assembly structure of the electric push-pull assembly of the movable cabin in an embodiment of the present invention;
[0035] Fig.12 for Fig.11 Cross-section of the middle region D;
[0036] Fig.13 for Fig.11 Schematic diagram of the structure of the middle area F;
[0037] Fig.14 for Fig.11 Schematic diagram of the structure of the middle region G;
[0038] Fig.15 This is a schematic diagram of the position of the auxiliary guide assembly of the movable cabin in an embodiment of the present invention;
[0039] Fig.16 for Fig.15 a cross-sectional view of the middle region E;
[0040] Fig.17 is a cross-sectional view of a door locking assembly in an embodiment of the present invention;
[0041] Fig.18It is a partial enlarged view of the position of the door when the movable cabin is in the open state in the embodiment of the present invention;
[0042] Fig.19 A schematic diagram of the working process of an embodiment of the present invention;
[0043] Fig. 20 Schematic diagram of a calculation model for observable azimuth and elevation angles according to an embodiment of the present invention.
[0044] Description of reference numerals:
[0045] 1- movable cabin; 2- fixed cabin; 3- vehicle chassis; 4- photoelectric measurement equipment; 5- top wall; 6- left wall; 7- left cabin door; 8- right cabin door; 9- right wall; 10- cabin door rotary hinge; 11- movable cabin push-pull guide rail assembly; 12- left and right cabin door electric rotary assembly; 13- cabin door locking assembly; 14- movable cabin electric push-pull assembly; 15- movable cabin auxiliary guide assembly; 16- guide rail; 17- ball support frame; 18- ball retainer; 19- ball; 20- revolving door motor; 21- revolving door reducer; 22- revolving door reducer mounting seat; 23- transmission connecting rod; 24- reducer transmission connecting rod pressure ring; 25- rotating hinge; 26- slide rail; 27- limit block; 28- photoelectric switch gasket A; 29- photoelectric switch A; 30- transmission key; 31- ball Surface locking pin; 32-spherical rotating pin; 33-anti-loosening locking spring; 34-brake mounting seat; 35-power-off lock brake stator; 36-brake spring; 37-power-off lock brake mover; 38-fixing pin; 39-fixing pin mounting seat; 40-push-pull cabin motor; 41-push-pull cabin reducer; 42-push-pull cabin motor reducer mounting seat; 43-coupling; 44-drive screw mounting seat; 45-photoelectric switch seat; 46-photoelectric switch gasket B; 47-photoelectric switch B; 48-drive screw; 49-drive nut; 50-electric limit shading sheet; 51-laser distance measuring sensor support; 52-laser distance measuring sensor; 53-bearing outer pressure ring; 54-angular contact ball bearing group; 55-bearing inner pressure ring; 56-guide rod; 57-guide piece; 58-guide mounting seat. DETAILED DESCRIPTION
[0046] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.
[0047] like Figure 1-3As shown, an unattended vehicle-mounted photoelectric measuring equipment movable cabin that can be automatically deployed and retracted includes a movable cabin deployment and retraction control system, a movable cabin 1, a fixed cabin 2, a vehicle-mounted chassis 3 and a photoelectric measuring device 4; the movable cabin deployment and retraction control system includes a cabin door locking assembly control module, a left and right cabin door electric rotation assembly control module and a movable cabin electric push-pull assembly control module, which are respectively used to control the cabin door locking assembly 13, the left and right cabin door electric rotation assembly 12 and the movable cabin electric push-pull assembly 14; the fixed cabin 2 The photoelectric measuring device 4 is fixedly mounted on the vehicle chassis 3, and is located between the fixed cabin 2 and the movable cabin 1. The movable cabin deployment and retraction control system is mounted on the vehicle chassis 3; the movable cabin 1 is composed of a top wall 5, a left wall 6, a left cabin door 7, a right cabin door 8, a right wall 9 and a cabin door rotary hinge 10; wherein the top wall 5, the left wall 6 and the right wall 9 are integral structures, and the left cabin door 7 and the right cabin door 8 are respectively hinged to the left wall 6 and the right wall 9 through two sets of cabin door rotary hinges 10 at the upper and lower ends; Figure 4 As shown, a movable cabin push-pull guide rail assembly 11 is respectively arranged between the left wall 6 and the fixed cabin 2, and between the right wall 9 and the fixed cabin 2; a movable cabin electric push-pull assembly 14 is arranged on the inner side of the left wall or the inner side of the right wall of the fixed cabin 2, and a movable cabin auxiliary guide assembly 15 is arranged on the inner side of the corresponding right wall or the inner side of the left wall; left and right cabin door electric rotation assemblies 12 are respectively installed between the left cabin door 7 and the left wall 6 of the movable cabin 1, and between the right cabin door 8 and the right wall 9, and both groups of left and right cabin door electric rotation assemblies 12 are installed on the inner side of the cabin body; the movable cabin electric push-pull assembly 14 and the left and right cabin door electric rotation assemblies 12 are electrically controlled by the movable cabin deployment and withdrawal control system; the movable cabin deployment and withdrawal control system is controlled by the remote control console; cabin door locking assemblies 13 are installed between the left cabin door 7 and the top wall 5, between the right cabin door 8 and the top wall 5, between the left cabin door 7 and the fixed cabin 2, and between the right cabin door 8 and the fixed cabin 2 of the movable cabin 1, and the cabin door locking assemblies 13 are installed on the inner side of the cabin body;
[0048] like Figure 5As shown, the movable cabin push-pull guide rail assembly 11 includes a guide rail 16, a ball support frame 17, a ball retainer 18 and a ball 19; two groups of guide rails 16 are respectively installed on the inner side of the left wall 6 and the right wall 9 by screws, two groups of ball retainers 18 are respectively fixed in the grooves of the guide rails 16, and two groups of ball support frames 17 are respectively installed on the two outer walls of the fixed cabin 2 by screws; two ball support frames 17 are respectively arranged in the two groups of ball retainers 18, and the upper and lower walls of each ball support frame 17 are respectively provided with an arc-shaped groove matching the size of the ball 19; the corresponding positions on the inner side of the guide rail 16 are also respectively provided with arc-shaped grooves of the same shape as the arc-shaped grooves on the ball support frame 17; a plurality of balls 19 are respectively arranged on the ball retainers 18, and cooperate with the semicircular grooves arranged on the guide rail 16 and the ball support frame 17, so that the movable cabin 1 can slide back and forth;
[0049] like Figure 6 As shown, the left and right door electric rotation components 12 include a revolving door motor 20, a revolving door reducer 21, a revolving door reducer mounting seat 22, a transmission connecting rod 23, a reducer transmission connecting rod pressure ring 24, a rotating hinge 25, a slide rail 26, a limit block 27, a photoelectric switch gasket A28, a photoelectric switch A29, a transmission key 30, a spherical locking pin 31, a spherical rotating pin 32 and an anti-loosening locking spring 33; wherein, the two revolving door reducer mounting seats 22 are respectively mounted on the left wall 6 and the right wall 9, and the structure is L-shaped, the vertical part thereof is correspondingly mounted on the left wall 6 or the right wall 9, and the horizontal part is fixedly connected to the revolving door reducer 21, the revolving door motor 20 is fixedly connected to the revolving door reducer 21, and its output is connected to the input of the revolving door reducer 21; the revolving door motor 20 is electrically controlled by the movable cabin deployment and retraction control system; as shown Figure 7 As shown, a central hole is provided on the horizontal part of the revolving door reducer mounting seat 22, and the output shaft of the revolving door reducer 21 passes through the central hole; a keyway is provided on the output shaft of the revolving door reducer 21, and the transmission key 30 is installed in the keyway; the transmission connecting rod 23 is a U-shaped structure, and its U-shaped mouth faces the corresponding left door 7 or right door 8, and central holes are provided at both ends, one end of which is sleeved on the output shaft of the revolving door reducer 21, and the other end is hinged to the rotating hinge 25 through a pin shaft; a reducer transmission connecting rod pressing ring 24 is also provided above the transmission connecting rod 23, and a screw is passed through the reducer transmission connecting rod pressing ring 24 to fix the transmission connecting rod 23 on the output shaft of the revolving door reducer 21 to prevent it from moving up and down;
[0050] like Figure 8The other end of the transmission connecting rod 23 is hinged to the rotating hinge 25 through a pin shaft, and the specific structure is as follows: the rotating hinge 25 is provided with two ears, and the two ears are provided with corresponding center holes, the spherical locking pin 31 is inserted from the lower center hole, and the spherical rotating pin 32 is inserted from the upper center hole, and the stud at the end of the spherical locking pin 31 cooperates with the screw hole at the end of the spherical rotating pin 32 to hinge the other end of the transmission connecting rod 23 on the rotating hinge 25; the spherical locking pin 31 and the spherical rotating pin 32 are connected to the rotating hinge 25. The rotation pin 32 and the other end of the transmission link 23 are connected as a whole, so that the left door 7 and the right door 8 can rotate flexibly relative to the transmission link 23; two anti-loosening locking springs 33 are also arranged between the spherical locking pin 31 and the spherical rotating pin 32, and their elastic force is used to pre-tighten and prevent the connection between the spherical locking pin 31 and the spherical rotating pin 32 from loosening, further improving the stability and rotation flexibility of this part, and preventing the left door 7 and the right door 8 from getting stuck during the opening or closing rotation process; Fig. 9 As shown, the cross section of the slide rail 26 is a T-shaped structure, and is fixed to the cabin door by screws. A T-shaped slide groove corresponding to the slide rail 26 is designed on the base of the rotary hinge 25. The slide rail 26 cooperates with the T-shaped slide groove so that the rotary hinge 25 can slide on the slide rail 26; limit stops 27 are respectively installed at both ends of the slide rail 26, and a light shielding sheet is arranged on the limit stop 27 which is far away from the left wall 6 or the right wall 9. A photoelectric switch A29 is installed on the upper end of the base of the rotary hinge 25. When the left cabin door 7 and the right cabin door 8 are closed, the light shielding sheet on the limit stop 27 shields the photoelectric switch A29. A photoelectric switch gasket A28 is arranged below the photoelectric switch A29. The photoelectric switch A29 transmits the photoelectric signal to the rotary door motor 20, thereby realizing the closing limit of the left cabin door 7 and the right cabin door 8;
[0051] like Fig.10 , Fig.11 As shown, the movable cabin electric push-pull assembly 14 includes a push-pull cabin motor 40, a push-pull cabin reducer 41, a push-pull cabin reducer mounting seat 42, a coupling 43, a transmission screw mounting seat 44, a photoelectric switch seat 45, a photoelectric switch gasket B 46, a photoelectric switch B 47, a transmission screw 48, a transmission nut 49, an electric limit shading sheet 50, a laser ranging sensor support 51, a laser ranging sensor 52, a bearing outer pressure ring 53, an angular contact ball bearing group 54 and a bearing inner pressure ring 55; wherein, as Fig.13 As shown, the push-pull cabin reducer mounting seat 42 is mounted on the inner side of the left wall of the fixed cabin 2, and the push-pull cabin reducer 41 is mounted on the push-pull cabin reducer mounting seat 42 by screws after being connected to the push-pull cabin motor 40; the push-pull cabin motor 40 is electrically controlled by the movable cabin deployment and retraction control system; the output end of the push-pull cabin reducer 41 is fixedly connected to one end of the coupling 43, and the other end of the coupling 43 is fixedly connected to one end of the transmission screw 48; Fig.12As shown, the transmission screw mounting seat 44, the bearing outer pressure ring 53, the angular contact ball bearing group 54 and the bearing inner pressure ring 55 together constitute the supporting shaft system of the transmission screw 48, and the transmission screw 48 is installed on the inner side of the left wall of the fixed cabin 2; wherein, a shaft shoulder is designed on the transmission screw 48, and two angular contact ball bearing groups 54 are installed on the transmission screw mounting seat 44 in a back-to-back manner and abut against the shaft shoulder on the transmission screw 48; two bearing outer pressure rings 53 are respectively arranged on the outer sides of the two angular contact ball bearing groups 54 for axially pressing and fixing the angular contact ball bearing groups 54; two groups of bearing inner pressure rings 55 are also installed on the inner side of the angular contact ball bearing group 54, which play a role in preventing loosening while pre-tightening the angular contact ball bearing group 54; as shown in FIG. Fig.14 As shown, the transmission nut 49 is installed on the left wall 6 and cooperates with the transmission screw 48 to convert the rotational motion output by the push-pull cabin motor 40 into the linear motion of the movable cabin 1; the transmission nut 49 is also provided with two electric limit shading sheets 50; the two transmission screw mounting seats 44 are both provided with photoelectric switches B 47 through the photoelectric switch seats 45 and the photoelectric switch gaskets B46 provided thereon; during the movement of the movable cabin 1, when the electric limit shading sheet 50 blocks the photoelectric switch B 47, the photoelectric switch B 47 transmits the photoelectric signal to the push-pull cabin motor 40, thereby controlling the limit of the push-out and closing of the movable cabin 1; the laser distance sensor 52 is arranged on the left wall 6 of the movable cabin 1 through the laser distance sensor support 51, and the laser distance sensor 52 is arranged above the transmission screw mounting seat 44; during the movement of the movable cabin 1, the laser distance sensor 52 emits a laser signal to the side wall of the transmission nut 49, and uses the side wall of the transmission nut 49 to realize the reception of the laser signal echo, thereby determining the real-time movement position of the movable cabin 1, and the acquired position information can be used to determine the observation range that the photoelectric measuring device 4 can achieve;
[0052] like Figure 15-16As shown, the auxiliary guide assembly 15 of the movable cabin includes a bearing outer pressure ring 53, an angular contact ball bearing group 54, a bearing inner pressure ring 55, a guide rod 56, a guide member 57 and a guide mounting seat 58, which are used to cooperate with the movable cabin electric push-pull assembly 14 and the movable cabin push-pull guide rail assembly 11 to realize the automatic opening and closing of the movable cabin 1; wherein, the guide mounting seat 58, the bearing outer pressure ring 53, the angular contact ball bearing group 54 and the bearing inner pressure ring 55 together constitute the support shaft system of the guide rod 56, and the guide rod 56 is installed on the inner side of the right wall of the fixed cabin 2; the conductive rod 56 is designed with a shaft shoulder , two angular contact ball bearing groups 54 are mounted on the guide mounting seat 58 in a back-to-back manner, and abut against the shaft shoulder on the guide rod 56; two bearing outer pressure rings 53 are respectively arranged on the outer sides of the two angular contact ball bearing groups 54, which are used to axially compress and fix the angular contact ball bearing groups 54; two groups of bearing inner pressure rings 55 are also installed on the inner side of the angular contact ball bearing group 54, which play a role in preventing loosening while pre-tightening the angular contact ball bearing group 54; the guide member 57 is installed on the right wall 9, and its inner wall cooperates with the guide rod 56; so that the movable cabin 1 can be stably opened and closed;
[0053] like Fig.17 As shown, the door locking assembly 13 includes a brake mounting seat 34, a power-off lock brake stator 35, a brake spring 36, a power-off lock brake mover 37, a fixing pin 38 and a fixing pin mounting seat 39; wherein, two brake mounting seats 34 are mounted on the top wall 5, and the other two brake mounting seats 34 are respectively mounted on the left door 7 and the right door 8; the four power-off lock brake stators 35 are respectively mounted on the four brake mounting seats 34, and each power-off lock brake stator 35 is designed with 6 evenly distributed threaded holes, and a guide column is arranged at the center of the threaded hole; each power-off lock brake stator 35 is electrically controlled by the movable cabin deployment and retraction control system; the brake spring Both ends of the spring 36 are provided with flanges with center holes, and the flange located at the upper end of the brake spring 36 is designed with external threads; four sets of fixed pin mounting seats 39 are respectively installed on the fixed cabin 2, the left cabin door 7 and the right cabin door 8 at positions corresponding to the brake mounting seats 34, and four sets of fixed pins 38 are respectively installed on the four sets of fixed pin mounting seats 39 by screws; the fixed pin 38 is designed with a center hole with a 45° chamfer, and the power-off lock brake mover 37 is designed with a guide column with a 45° cone surface; in the power-off state, the brake spring 36 uses elastic force to press the guide column of the power-off lock brake mover 37 into the center hole of the fixed pin 38, so that the left cabin door 7 and the right cabin door 8 can be reliably closed. The brake spring 36 is installed at the outer side of the power-off lock brake stator 35, which can improve the anti-bending ability of the power-off lock brake mover 37 when receiving external force, and further enhance the reliability of the closure of the left cabin door 7 and the right cabin door 8;
[0054] In addition, the positions of the power-off lock brake movers 37 on the left wall 6 and the right wall 9 corresponding to the opened left door 7 and the right door 8 are also respectively installed with fixing pin mounting seats 39, and the fixing pin 38 is installed on the fixing pin mounting seats 39 by screws; Fig.18 As shown, when the on-board photoelectric measuring equipment is to be powered on, the left door 7 and the right door 8 are automatically opened, and a suction force is generated between the power-off lock brake stator 35 and the power-off lock brake mover 37, and the brake spring 36 contracts along the guide column of the power-off lock brake stator 35, driving the power-off lock brake mover 37 to move, so that the matching relationship between the center hole of the fixing pin 38 and the guide column of the power-off lock brake mover 37 is released; Fig.18 As shown, when the left door 7 and the right door 8 are automatically opened 270° from the closed position to the predetermined position, the left and right door electric rotation components 12 stop moving after receiving the limit signal of the photoelectric switch 29. At this time, the power-off lock brake stator 35 and the power-off lock brake mover 37 installed on the inner side of the left door 7 and the right door 8 lose power, and the brake spring 36 pops out along the guide column of the power-off lock brake stator 35, driving the power-off lock brake mover 37 to move, so that the guide column of the power-off lock brake mover 37 and the center hole of the fixing pin 38 installed on the left wall 6 and the right wall 9 are in a matching relationship, thereby fixing the left door 7 and the right door 8 to the outer side of the right wall and the left wall of the cabin body.
[0055] When used in the field, the movable cabin 1, the fixed cabin 2 and the vehicle chassis 3 together form the vehicle-mounted structure of the photoelectric measuring device 4, that is, the vehicle body is used as a carrier to carry out the measurement work with the photoelectric instrument. Fig.19 As shown, the specific working process of opening the activity cabin 1 is as follows:
[0056] Step 1: The mobile cabin is deployed, the control system is powered on, the system is self-checked and each I / O port is initialized;
[0057] Step 2: The control system for deploying and retracting the movable cabin sends a command to the control module of the cabin door locking assembly to control the stator 35 of the power-off lock brake to pull the mover 37 of the power-off lock brake upward. At this time, the guide column on the mover 37 of the power-off lock brake is disengaged from the fixing pin 38, so that the left cabin door 7 and the right cabin door 8 are unlocked;
[0058] Step 3, the control system for deploying and withdrawing the movable cabin sends a command to the control module of the electric rotating assembly of the left and right doors to control the power supply of the rotating door motor 20 to realize the automatic opening of the left door 7 and the right door 8; when the light shielding sheet on the limit stopper 27 blocks the photoelectric switch A29, the photoelectric switch A29 sends a signal to the control module of the electric rotating assembly of the left and right doors to control the rotating door motor 20 to stop working;
[0059] Step 4: The control system for deploying and withdrawing the movable cabin sends a command to the cabin door locking assembly control module to control the power-off lock brake mover 37 to disengage from the power-off lock brake stator 35. At this time, the guide column on the power-off lock brake mover 37 falls into the fixing pin 38 provided at the corresponding position on the left wall 6 and the right wall 9, locking the left cabin door 7 and the right cabin door 8 in the 270° open position.
[0060] Step 5: The control system for unfolding and retracting the movable cabin sends a command to the control module of the movable cabin electric push-pull assembly to control the push-pull cabin motor 40 to be powered on, and the movable cabin auxiliary guide assembly 15 and the movable cabin push-pull guide rail assembly 11 cooperate to realize the automatic opening of the movable cabin 1; when the electric limit shading sheet 50 provided on the transmission nut 49 blocks the photoelectric switch B 47, the photoelectric switch B 47 sends a signal to the control module of the movable cabin electric push-pull assembly to drive the push-pull cabin motor 40 to stop working;
[0061] Step 6: The laser ranging sensor 52 feeds back the real-time position information of the movable cabin 1 to the movable cabin deployment and retraction control system, and the movable cabin deployment and retraction control system calculates the observation range in the open state.
[0062] The method of withdrawing the activity cabin 1 is the same as the above logic. Fig. 20 As shown in the calculation model, a Cartesian coordinate system is established with the intersection of the azimuth axis and the pitch axis of the photoelectric measurement equipment 4 as the origin O, and the vehicle length direction as the X-axis, the vehicle width direction as the Y-axis, and the vehicle height direction as the Z-axis; the optical load aperture carried by the photoelectric measurement equipment 4 is assumed to be D, and the distance between the optical axis of the optical load and the pitch center is assumed to be L.
[0063] If you want to obtain the azimuth angle and pitch angle that can be observed in the semi-open state of the mobile cabin 1, you need to know the coordinates (x, y, z) of the open outline of the mobile cabin 1 in the OXYZ coordinate system after the left cabin door 7 and the right cabin door 8 are opened. When the mobile cabin 1 is in a semi-open state, the Z-axis coordinate value z0 of the open outline of the mobile cabin 1 can be obtained by the laser ranging sensor 51. At the same time, the X-axis coordinate x0 and the X-axis coordinate y0 of the open outline of the mobile cabin 1 can be easily obtained according to the design model. Thus, the corresponding relationship between the observable azimuth angle α, the pitch angle β and the above parameters is established, as shown in the following formula:
[0064]
[0065] Since the distance x1 between the front end of the optical load and the origin O is fixed, the deployment position Δx of the movable cabin 1 when the movable cabin 1 is not initially deployed can be obtained according to the distance x2 between the movable cabin 1 and the origin O when the movable cabin 1 is not initially deployed. Assuming that the rain falls vertically, the following relationship can be obtained:
[0066] Δx=x2-x1
[0067] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention rather than to limit them. For ordinary professional and technical personnel in the field, the specific technical solutions recorded in the above embodiments can be modified, or some of the technical features therein can be replaced by equivalents, and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the scope of the technical solutions protected by the present invention.
Claims
1. An unattended vehicle-mounted photoelectric measuring equipment movable cabin that can be automatically deployed and retracted, comprising a movable cabin deployment and retraction control system, a movable cabin (1), a fixed cabin (2), a vehicle-mounted chassis (3) and a photoelectric measuring device (4), wherein the fixed cabin (2) is fixedly mounted on the vehicle-mounted chassis (3), the photoelectric measuring device (4) is arranged on the vehicle-mounted chassis (3) and is located between the fixed cabin (2) and the movable cabin (1), and the movable cabin deployment and retraction control system is arranged on the vehicle-mounted chassis (3), characterized in that: The movable cabin (1) is composed of a top wall (5), a left wall (6), a left cabin door (7), a right cabin door (8), and a right wall (9), and the top wall (5), the left wall (6), and the right wall (9) are all integral structures; the left cabin door (7) and the right cabin door (8) are respectively hinged on the left wall (6) and the right wall (9) through upper and lower sets of cabin door rotating hinges (10); A movable cabin push-pull guide rail assembly (11) is provided between the left wall (6) and the fixed cabin (2), and between the right wall (9) and the fixed cabin (2), respectively; a movable cabin electric push-pull assembly (14) is provided on the inner side of the left wall or the inner side of the right wall of the fixed cabin (2), and a movable cabin auxiliary guide assembly (15) is provided on the inner side of the right wall or the inner side of the left wall of the fixed cabin (2); Left and right door electric rotating assemblies (12) are respectively installed between the left door (7) and the left wall (6), and between the right door (8) and the right wall (9), and both of the left and right door electric rotating assemblies (12) are installed inside the cabin body of the movable cabin (1); The movable cabin electric push-pull assembly (14) and the left and right cabin door electric rotation assemblies (12) are all electrically controlled by a movable cabin deployment and retraction control system; the movable cabin deployment and retraction control system can be controlled by a remote control console.
2. The unattended vehicle-mounted photoelectric measurement equipment movable cabin that can be automatically deployed and retracted according to claim 1 is characterized in that: The two groups of movable cabin push-pull guide rail assemblies (11) each comprise a guide rail (16), a ball support frame (17), a ball retainer (18) and a ball (19); The two groups of guide rails (16) are respectively installed on the inner side of the left wall (6) and the right wall (9); the two groups of ball retainers (18) are respectively fixed in the grooves of the guide rails (16); and the two ball support frames (17) are respectively fixed on the two outer side walls of the fixed cabin (2); the two ball support frames (17) are respectively arranged in the two groups of ball retainers (18); the upper and lower walls of each ball support frame (17) are respectively provided with an arc-shaped groove matching the size of the ball (19); the corresponding positions on the inner side of the guide rails (16) are also respectively provided with an arc-shaped groove having the same shape as the arc-shaped groove on the ball support frame (17); a plurality of balls (19) are respectively arranged on the ball retainers (18) and cooperate with the semicircular grooves arranged on the guide rails (16) and the ball support frame (17), so that the movable cabin (1) can slide forward and backward.
3. The unattended vehicle-mounted photoelectric measurement equipment movable cabin that can be automatically deployed and retracted according to claim 1 is characterized in that: Each of the left and right door electric rotating assemblies (12) comprises a rotating door motor (20), a rotating door reducer (21), a rotating door reducer mounting seat (22), a transmission connecting rod (23), a rotating hinge (25), a slide rail (26), a limit stopper (27), a photoelectric switch A (29), a transmission key (30), a spherical locking pin (31) and a spherical rotating pin (32); The two revolving door reducer mounting seats (22) are respectively mounted on the left wall (6) and the right wall (9), and are L-shaped in structure. The vertical portion is correspondingly mounted on the left wall (6) or the right wall (9), and the horizontal portion is fixedly connected to the revolving door reducer (21). The revolving door motor (20) is fixedly connected to the revolving door reducer (21), and the output of the revolving door reducer is connected to the input of the revolving door reducer (21). The revolving door motor (20) is electrically controlled by the movable cabin deployment and retraction control system. The revolving door reducer mounting seats The horizontal part of (22) is provided with a central hole, and the output shaft of the revolving door reducer (21) passes through the central hole; the output shaft of the revolving door reducer (21) is provided with a keyway, and the transmission key (30) is installed in the keyway; the transmission connecting rod (23) is a U-shaped structure, and its U-shaped mouth faces the corresponding left door (7) or right door (8), and the two ends are respectively provided with central holes, one end of which is sleeved on the output shaft of the revolving door reducer (21), and the other end is hinged to the rotating hinge (25) through a pin shaft; The cross section of the slide rail (26) is T-shaped and is fixed to the door by screws. A T-shaped slide groove corresponding to the slide rail (26) is designed on the base of the rotary hinge (25). The slide rail (26) cooperates with the T-shaped slide groove so that the rotary hinge (25) can slide on the slide rail (26). Limit blocks (27) are respectively installed at both ends of the slide rail (26). A light shielding sheet is arranged on the limit block (27) which is far away from the left wall (6) or the right wall (9). A photoelectric switch A (29) is installed on the upper end of the base of the rotary hinge (25). When the left door (7) and the right door (8) are closed, the light shielding sheet on the limit block (27) shields the photoelectric switch A (29). A photoelectric switch gasket A (28) is arranged below the photoelectric switch A (29). The photoelectric switch A (29) transmits a photoelectric signal to the rotary door motor (20), thereby realizing the closing limit of the left door (7) and the right door (8).
4. The unattended vehicle-mounted photoelectric measurement equipment movable cabin that can be automatically deployed and retracted according to claim 3 is characterized in that: A reducer drive connecting rod pressing ring (24) is also provided above the drive connecting rod (23). A screw is passed through the reducer drive connecting rod pressing ring (24) to fix the drive connecting rod (23) on the output shaft of the revolving door reducer (21) to prevent it from moving up and down. The other end of the transmission connecting rod (23) is hinged to the rotating hinge (25) through a pin shaft, and the specific structure is as follows: the rotating hinge (25) is provided with two support ears, and the two support ears are provided with corresponding center holes, the spherical locking pin (31) is inserted from the lower center hole, and the spherical rotating pin (32) is inserted from the upper center hole, and the stud at the end of the spherical locking pin (31) is matched with the screw hole at the end of the spherical rotating pin (32) to hinge the other end of the transmission connecting rod (23) on the rotating hinge (25); the spherical locking pin (31), the spherical rotating pin (32) and the other end of the transmission connecting rod (23) are connected as a whole, so that the left door (7) and the right door (8) can be flexibly rotated relative to the transmission connecting rod (23).
5. The unattended vehicle-mounted photoelectric measurement equipment movable cabin that can be automatically deployed and retracted according to claim 4 is characterized in that: Two anti-loosening locking springs (33) are also arranged between the spherical locking pin (31) and the spherical rotating pin (32) to prevent the connection between the spherical locking pin (31) and the spherical rotating pin (32) from loosening, thereby causing the left door (7) and the right door (8) to become stuck during the opening or closing rotation process.
6. The unattended vehicle-mounted photoelectric measurement equipment movable cabin capable of automatically deploying and retracting according to claim 1, characterized in that: The movable cabin electric push-pull assembly (14) comprises a push-pull cabin motor (40), a push-pull cabin reducer (41), a push-pull cabin reducer mounting seat (42), a coupling (43), a transmission screw mounting seat (44), a photoelectric switch seat (45), a photoelectric switch B (47), a transmission screw (48), a transmission nut (49), an electric limit light shielding sheet (50), a laser distance sensor support (51), a laser distance sensor (52), a bearing outer pressure ring (53), an angular contact ball bearing group (54) and a bearing inner pressure ring (55); The push-pull cabin reducer mounting seat (42) is mounted on the inner side of the left wall of the fixed cabin (2); the push-pull cabin reducer (41) is mounted on the push-pull cabin reducer mounting seat (42) by means of screws after being connected to the push-pull cabin motor (40); the push-pull cabin motor (40) is electrically controlled by the movable cabin deployment and retraction control system; the output end of the push-pull cabin reducer (41) is fixedly connected to one end of the coupling (43), and the other end of the coupling (43) is fixedly connected to one end of the transmission screw (48); the transmission screw mounting seat (44), the bearing outer pressure ring (53), the angular contact ball bearing group (54) and the bearing inner pressure ring (55) together constitute The supporting shaft system of the transmission screw (48) is provided, and the transmission screw (48) is installed on the inner side of the left wall of the fixed cabin (2); wherein the transmission screw (48) is designed with a shaft shoulder, and two angular contact ball bearing groups (54) are installed on the transmission screw mounting seat (44) in a back-to-back manner and abut against the shaft shoulder on the transmission screw (48); two bearing outer pressure rings (53) are respectively arranged on the outer sides of the two angular contact ball bearing groups (54) for axially pressing and fixing the angular contact ball bearing groups (54); two groups of bearing inner pressure rings (55) are also arranged on the inner side of the angular contact ball bearing groups (54) for pre-tightening the angular contact ball bearing groups (54) The transmission nut (49) is mounted on the left wall (6) and cooperates with the transmission lead screw (48) to convert the rotational motion output by the push-pull cabin motor (40) into the linear motion of the movable cabin (1); the transmission nut (49) is also provided with two electric limit shading sheets (50); the two transmission lead screw mounting seats (44) are both provided with photoelectric switches B (47) through photoelectric switch seats (45) and photoelectric switch gaskets B (46) arranged thereon; during the movement of the movable cabin (1), when the electric limit shading sheet (50) blocks the photoelectric switch B (47), the photoelectric switch B (47) transmits a photoelectric signal to the push-pull cabin motor (4 0), thereby controlling the limit of the push-out and closing of the movable cabin (1); the laser distance sensor (52) is arranged on the left wall (6) of the movable cabin (1) through the laser distance sensor support (51), and the laser distance sensor (52) is arranged above the transmission screw mounting seat (44); during the movement of the movable cabin (1), the laser distance sensor (52) emits a laser signal to the side wall of the transmission nut (49), and uses the side wall of the transmission nut (49) to realize the reception of the laser signal echo, thereby determining the real-time movement position of the movable cabin (1), and the acquired position information can be used to determine the observation range that can be achieved by the photoelectric measurement device (4).
7. The unattended vehicle-mounted photoelectric measurement equipment movable cabin capable of automatically deploying and retracting according to claim 1, characterized in that: The movable cabin auxiliary guide assembly (15) comprises a bearing outer pressure ring (53), an angular contact ball bearing group (54), a bearing inner pressure ring (55), a guide rod (56), a guide member (57) and a guide mounting seat (58); The guide mounting seat (58), the bearing outer pressure ring (53), the angular contact ball bearing group (54) and the bearing inner pressure ring (55) together form a supporting shaft system of the guide rod (56), and the guide rod (56) is installed on the inner side of the right wall of the fixed cabin (2); the transmission rod (56) is designed with a shaft shoulder, and the two angular contact ball bearing groups (54) are installed on the guide mounting seat (58) in a back-to-back manner and abut against the shaft shoulder on the guide rod (56); the two angular contact Two bearing outer pressure rings (53) are respectively arranged on the outer side of the ball bearing group (54) for axially pressing and fixing the angular contact ball bearing group (54); two groups of bearing inner pressure rings (55) are also arranged on the inner side of the angular contact ball bearing group (54) for pre-tightening the angular contact ball bearing group (54) and preventing it from loosening; a guide member (57) is installed on the right wall (9), and its inner wall cooperates with the guide rod (56); so that the movable cabin (1) can be stably opened and closed.
8. The unattended vehicle-mounted photoelectric measurement equipment movable cabin that can be automatically deployed and retracted according to claim 1 is characterized in that: Door locking assemblies (13) electrically controlled by the movable cabin deployment and retraction control system are installed at corresponding inner positions between the left cabin door (7) and the top wall (5), between the right cabin door (8) and the top wall (5), between the left cabin door (7) and the fixed cabin (2), and between the right cabin door (8) and the fixed cabin (2).
9. The unattended vehicle-mounted photoelectric measurement equipment movable cabin capable of automatically deploying and retracting according to claim 8, characterized in that: The door locking assembly (13) comprises a brake mounting seat (34), a power-off lock brake stator (35), a brake spring (36), a power-off lock brake mover (37), a fixing pin (38) and a fixing pin mounting seat (39); Two brake mounting seats (34) are mounted on the top wall (5), and the other two brake mounting seats (34) are respectively mounted on the left cabin door (7) and the right cabin door (8); the four power-off lock brake stators (35) are respectively mounted on the four brake mounting seats (34), and each power-off lock brake stator (35) is designed with 6 evenly distributed threaded holes, and a guide column is arranged at the center of the threaded hole; each power-off lock brake stator (35) is electrically controlled by the mobile cabin deployment and retraction control system; the brake spring (36 ) are provided with flanges with center holes at both ends, and the flange located at the upper end of the brake spring (36) is designed with external threads; four groups of fixing pin mounting seats (39) are respectively installed at positions corresponding to the brake mounting seats (34) on the fixed cabin (2), the left cabin door (7) and the right cabin door (8), and four groups of fixing pins (38) are respectively installed on the four groups of fixing pin mounting seats (39) by screws; the fixing pins (38) are designed with a center hole with a 45° chamfer, and the power-off lock brake mover (37) is designed with a guide column with a 45° cone surface.
10. The unattended vehicle-mounted photoelectric measurement equipment movable cabin capable of automatically unfolding and retracting according to claim 9, characterized in that: A fixing pin mounting seat (39) is respectively installed on the outer side of the left wall (6) and the right wall (9) at positions corresponding to the power-off lock brake movers (37) on the left door (7) and the right door (8) after opening, and a fixing pin (38) is installed on the seat by screws.