Radar concealed mountain operation engineering method

Abstract

The invention relates to a radar hidden type mountain operation engineering method. A radar blindage auxiliary engineering system is used. The method comprises a non-wartime working step and a wartime step. In the non-wartime working step, the secondary radar is started; the main radar station is in a closed state; in the wartime step, the secondary radar is started, and the main radar station is intermittently started; the main radar station and the secondary radar form a radar matrix.

Description

Technical Field

[0001] The invention relates to a radar concealed mountain operation engineering method. Background Art

[0002] Radar antenna installation requires a base, and the existing technology generally uses a mobile radar vehicle or a fixed bracket for installation. However, in remote mountainous areas, radar installation is extremely inconvenient.

[0003] After the mountain is hollowed out, there will be problems such as collapse and deformation. How to keep the mountain stable becomes a technical problem that needs to be solved urgently. In addition, it is inconvenient to lift the equipment inside the mountain and it takes up a lot of space.

[0004] If a mobile radar vehicle is used, it is not suitable for mobile terrains such as mountainous areas, while a fixed bracket has poor scalability and is not convenient to carry and move. When the pot cover antenna needs to be replaced, its bracket needs to be replaced as well, which makes replacement inconvenient and affects efficiency. Especially in times of crisis, how to provide a quick and convenient installation base has become a technical problem that needs to be solved urgently.

[0005] In the prior art, the antenna occupies a large area and is inconvenient to transport or the antenna accessories need to be dismantled and installed on site, which is time-consuming and labor-intensive, especially during rescue time, which delays the opportunity and requires professional personnel to install, which is extremely inconvenient.

[0006] There are many mountainous areas in Northwest my country and Central Asia, and it is very inconvenient to use mobile radar vehicles, which are easy to be discovered. For this reason, fixed radars installed on the mountains are often used, and radars are arranged by excavating space in the mountains. This can not only interfere with high-altitude reconnaissance and detection, but also facilitate the placement of personnel and equipment. At the same time, it has good defensive capabilities.

[0007] There are many disadvantages of mountain shelter radar, such as signal interference, how to avoid being detected, how to reduce the occupation of the internal space of the mountain when it is retracted and hidden, and how to smoothly realize the exposure and retraction of the radar antenna has become a technical problem that needs to be solved urgently. Summary of the invention

[0008] The technical problem to be solved by the present invention is generally to provide a radar concealed mountain operation engineering method.

[0009] To solve the above problems, the technical solution adopted by the present invention is:

[0010] A radar concealed mountain operation engineering method, using a radar shelter auxiliary engineering system; the method includes non-wartime working steps and wartime steps;

[0011] In the non-wartime working procedure, the secondary radar is activated; the main radar station is closed;

[0012] In wartime procedures, the secondary radar is activated and the main radar station is activated intermittently; the main radar station and the secondary radar form a radar matrix.

[0013] As a further improvement of the above technical solution:

[0014] The power of the secondary radar is lower than that of the primary radar station;

[0015] The scanning range of the secondary radar is smaller than that of the primary radar station;

[0016] The scanning accuracy of the secondary radar is lower than that of the primary radar station.

[0017] First, the secondary radar is used to scan. When the scanning object needs to be located, the main radar station is started to perform a secondary scan and locate the scanning object to obtain the motion parameters, shape parameters and quantity of the scanning object.

[0018] When starting the main radar station operation, open the mountain gate and the auxiliary component sends the radar component out of the mountain gate; execute the radar base operation process.

[0019] When a scanning object is located close to the area where the main radar station is located, the scanning information of the same band is emitted by the simulated radar, and the radar component is converged into the mountain through the auxiliary component and the mountain gate is closed; the secondary radar is turned off.

[0020] When the radar antenna fails, the radar assembly will be retracted into the mountain; the radar antenna will be replaced by a crane suspended from the top beam;

[0021] Perform an installation method for a mountain radar antenna.

[0022] In order to provide a base that can facilitate work and convergence, a radar shelter auxiliary engineering system includes a frame assembly; an adjusting connecting rod part is arranged on the frame assembly; an adjusting swing part is arranged on the adjusting connecting rod part; and the adjusting connecting rod part is a four-bar mechanism. As a further improvement of the above technical solution: in order to realize radar installation, a radar assembly is arranged on the adjusting swing part. In order to form a stable mechanism for sending out radar and converging, the adjusting connecting rod part includes a main swing rod A and a secondary swing rod B, whose lower ends are respectively hingedly arranged on the frame assembly; a connecting rod C is hinged between the upper end of the main swing rod A and the upper end of the secondary swing rod B. In order to stabilize the mechanism, the main swing rods A are arranged in two parallel positions, the secondary swing rods B are arranged in two parallel positions, and the connecting rods C are arranged in two parallel positions; two connecting rods C are arranged between the two main swing rods A; and two connecting rods C are arranged between the two secondary swing rods B.

[0023] In order to realize the driving of the positive and negative parallelogram structure, a driven driving shaft and a swing gear shaft are respectively arranged on the frame assembly; the driven driving shaft and the active driving shaft are respectively connected to the corresponding motors through their corresponding clutches; the motor is on the frame assembly; the root of the driven driving shaft is key-connected with the auxiliary swing rod B; the root of the main swing rod A is key-connected with the active driving shaft; a swing gear shaft is hinged between the heads of the two main swing rods A; a plurality of intermediate wheel assemblies are arranged on the main swing rod A; a sliding gear A is arranged on the active driving shaft; the sliding gear A is transmission-connected with the swing gear shaft through a plurality of intermediate wheel assemblies; and the swing gear shaft is key-connected with the adjusting swing part.

[0024] In order to achieve synchronous swing of the radar antenna and adjustment of the scanning angle, a fork assembly is provided on the frame assembly. The fork assembly includes a first drive rod provided on the frame assembly and a second drive rod connected to the first drive rod in a direction-changing manner; a fork portion is provided at the end of the second drive rod, which is used to shift the sliding gear A to engage or disengage with the corresponding intermediate wheel assembly. The swing adjustment portion includes a swing frame assembly connected to the swing gear shaft; a longitudinal guide groove and a longitudinal drive rod are provided on the swing frame assembly.

[0025] In order to achieve further detection of the radar, the radar assembly is set in the longitudinal guide groove and connected to the longitudinal drive rod. The frame assembly is set in the mountain; when working, the radar assembly is located above the adjustment swing part; when converging, the radar assembly is located above or below the adjustment swing part. Through the improvement of the base, it is convenient to hide and work the radar, save limited mountain space, and facilitate installation, maintenance and work. Relative polar coordinates are formed through quadrilateral mechanisms and swing mechanisms to achieve accurate detection of the radar antenna.

[0026] In order to realize the extension and entry of the radar antenna into the mountain, a radar base operation process includes working steps; in the working steps, the mountain gate is opened, first, the adjusting connecting rod part is started to make a positive parallelogram motion to expose the head end of the main swing rod A out of the mountain gate; then, the adjusting connecting rod part is moved around to make an anti-parallelogram motion so that the main swing rod A continues to swing upward and extend to the set position.

[0027] As a further improvement of the above technical solution:

[0028] When performing a positive parallelogram motion, the driven drive shaft is connected to the motor, and the active drive shaft is connected to the motor; when performing an anti-parallelogram motion, the driven drive shaft is separated from the motor, and the active drive shaft is connected to the motor; first, after the active drive shaft drives the two main swing rods A to swing to a set angle, the fork portion is driven by the first drive rod and the second drive rod, so that the shifting sliding gear A is engaged with the corresponding intermediate gear assembly; secondly, while the head end of the main swing rod A is exposed at the mountain gate, the swing gear shaft drives the swing frame assembly to swing forward; thirdly, the radar assembly moves forward along the longitudinal guide groove through the longitudinal drive rod. After the working steps, there is a convergence step; the convergence step is opposite to the working steps. Among them, the working steps are assisted by the radar shelter auxiliary engineering system. When the radar assembly needs to be replaced, the radar assembly is separated from the longitudinal guide groove and the longitudinal drive rod for disassembly and assembly.

[0029] In order to improve the antenna, a concealed radar antenna component includes an antenna base; a swing arm component is hinged on the antenna base; a radar antenna part is arranged on the swing arm component; the swing arm component has an open state and a gathered state.

[0030] As a further improvement of the above technical solution:

[0031] As a split connection, the antenna base part is used to connect with the radar base; as a suitable antenna, the radar antenna part is a pot-lid type antenna; in order to facilitate the connection, a number of articulated connectors are distributed on the back of the radar antenna part; in order to meet the requirements of different sizes of radar antennas, the articulated connectors are adjustable along the side busbar direction.

[0032] The volume is reduced and a split structure is adopted, which further facilitates the transportation of accessories. The swing arm assembly includes a support seat portion arranged on the antenna base portion; an annular groove is arranged on the support seat portion; a pulling base and a plurality of guide bases are movable in the annular groove; a fixed support seat is fixedly arranged in the annular groove; a main rotating rod support group is hinged on the pulling base; a linkage hinged rod is hinged on the guide base, and its length can be adjusted; a fixed hinged support is hinged on the support seat portion; the main rotating rod support group and the linkage hinged rod The upper end of the fixed hinged support is hinged with the corresponding hinged connector; the linkage hinged rod at least includes a linkage hinged rod A and a linkage hinged support rod B; the driving base, the fixed support base and the guide base are connected through concentric annular guide rings A and / or annular guide rings B; guide holes matching the annular guide rings A and / or annular guide rings B are respectively provided on the driving base, the fixed support base and the guide base; the main rotating rod support group, the linkage hinged rod A, a plurality of linkage hinged support rods B and the fixed hinged support are arranged head to tail in sequence;

[0033] A first articulated rod A is articulated on the fixed articulated support through an articulated sleeve A; a second articulated rod B is articulated on the linked articulated rod A through an articulated sleeve B; the middle part of the second articulated rod B is articulated with the end of the first articulated rod A through an articulated seat A; a third articulated rod C is articulated on the linked articulated support rod B through an articulated sleeve C; the middle part of the third articulated rod C is articulated with the end of the second articulated rod B through an articulated seat B; between adjacent linked articulated support rods B, the middle part of the previous third articulated rod C is articulated with the end of the next third articulated rod C through an articulated seat C; between the linked articulated support rod B and the main rotating rod support group, an active connecting rod is articulated on the main rotating rod support group through an articulated sleeve D; a connecting articulated rod D is articulated on the linked articulated support rod B through an articulated sleeve B; the connecting articulated rod D and the active connecting rod are articulated through a connecting articulated seat D.

[0034] The articulated seat A, the articulated seat B and the articulated seat C have a rotation angle limit of movable articulation;

[0035] The maximum opening angles between the active connecting rod and the connecting hinge rod D, the connecting hinge rod D and the third hinge rod C, between adjacent third hinge rods C, between the third hinge rod C and the second hinge rod B, and between the second hinge rod B and the first hinge rod A are all acute angles and are arranged in a high and low staggered manner.

[0036] A hollow rotating seat is arranged at the center of the upper part of the supporting seat;

[0037] The rotating seat is connected to the main rotating rod support group through a rotating rod.

[0038] In order to facilitate the connection of the hinged rod, a central lifting rod is provided at the center of the rotating seat;

[0039] A lifting bracket is arranged at the upper end of the central lifting rod for supporting the lower part of the radar antenna.

[0040] In order to achieve Z-axis positioning, the annular groove is a T-slot.

[0041] In order to achieve three-point shaping, the first hinge rod A is provided with limit sleeves located on both sides of the hinge sleeve A;

[0042] Preferably, in order to increase the flexibility during opening and closing, the second hinged rod B is provided with limit sleeves located on both sides of the hinge sleeve B, thereby reducing the jamming phenomenon.

[0043] In order to facilitate installation, an antenna base is provided at the bottom of the radar antenna.

[0044] The lifting bracket is used to lift the antenna base;

[0045] A plurality of guide support members B are arranged on the support seat; the guide support members B move in a circular motion on the support seat.

[0046] In order to realize the installation and convenient transportation of the antenna, a method for installing a mountain radar antenna is provided, using the components of a concealed radar antenna;

[0047] The installation method includes the following steps:

[0048] First, open the swing arm assembly;

[0049] The radar antenna section is then mounted on the swing arm assembly.

[0050] As a further improvement of the above technical solution:

[0051] In order to reduce space and increase the opening angle, the antenna base is installed on the radar base during the first installation.

[0052] To suit the respective situation, when the radar antenna part is damaged, the radar antenna part is replaced on the swing arm assembly;

[0053] When transporting the concealed radar antenna assembly, the swing arm assembly is folded up.

[0054] In order to facilitate the connection, when the swing arm assembly is opened, the rotating seat is started, and the driving base of the main rotating arm support group is driven to rotate through the rotating rod, and under the guidance of the annular groove and the annular guide ring A and / or the annular guide ring B, the base and the guide base are driven to move forward along the arc; then, the connecting hinged rod D is driven to open in the forward movement through the active connecting rod, and the adjacent linked hinged support rods B are driven to move forward one by one in the arc; secondly, the adjacent third hinged rod C is driven forward and opened through the hinged seat C, and the second hinged rod B is driven forward and opened through the third hinged rod C, so that the linked hinged rod A and the linked hinged support rod B are opened;

[0055] The main rotating rod support group, the linkage hinged rod and the fixed hinged support member form a cone structure for supporting the radar antenna part;

[0056] When it is necessary to fold it, just rotate the rotating seat in the reverse direction.

[0057] When installing the radar antenna part; first, the lifting bracket is raised through the central lifting rod to support the antenna base; then, the position and angle of each articulated connection piece are adjusted to connect with the corresponding active connection rod, linkage articulated support rod B, linkage articulated rod A, and the upper end of the fixed articulated support piece; secondly, the central lifting rod is lowered by a set distance so that the articulated connection piece is stressed;

[0058] In order to realize the rotation of the radar and increase the scanning range, the rotation of the radar is realized by rotating the support seat.

[0059] In order to be suitable for combat situations, avoid being locked by reconnaissance aircraft, and protect the high-cost and high-precision main radar, a radar shelter auxiliary engineering system includes a main radar station and secondary radar stations arranged around the main radar station;

[0060] The main radar station includes an auxiliary component arranged in the mountain and a radar component arranged on the auxiliary component;

[0061] The secondary radar station is set up on the mountain around the radar assembly;

[0062] A secondary radar is provided at the secondary radar station;

[0063] To reduce the exposure of the primary radar, the secondary radar is activated when the radar assembly is operating.

[0064] As a further improvement of the above technical solution:

[0065] To facilitate internal construction, a frame structure located in the inner cavity of the mountain is provided on the auxiliary assembly;

[0066] The frame structure fits the space inside the mountain cavity;

[0067] A side beam is arranged on the frame structure, and a suspended top beam is arranged on the side beam;

[0068] A mountain gate is arranged on the frame structure;

[0069] The mountain gate includes the main gate in the middle and the side gates on both sides of the main gate;

[0070] When the main door and the side door are opened, they are used to send the radar components out of the mountain.

[0071] In order to reduce the impact on the mountain, a radar shelter auxiliary engineering system is set up in the frame structure;

[0072] The radar components are arranged on the radar shelter auxiliary engineering system.

[0073] The radar assembly includes an antenna base portion; a swing rod assembly is hinged on the antenna base portion;

[0074] A radar antenna portion is arranged on the swing arm assembly;

[0075] The swing arm assembly has an open state and a gathered state.

[0076] In order to confuse the enemy, the secondary radar simulates the appearance of the radar antenna section of the main radar station.

[0077] In non-wartime, the secondary radar is working; in wartime, the radar antenna department is working.

[0078] A crane is installed on the suspended top beam to assist in the disassembly and assembly of the radar antenna.

[0079] Simulated radars are set up around the secondary radar to confuse reconnaissance satellites.

[0080] The invention facilitates the rapid detection of the radar antenna out of the mountain gate, overcomes the respective disadvantages by using the ingenious combination of the positive and negative parallelogram mechanisms, reduces the dead points, and can be easily converged inside the mountain, making it convenient for the radar to adjust the detection distance and its tilt angle.

[0081] The present invention can provide a set of methods to achieve reasonable adjustment of the radar antenna, thereby meeting various working conditions and reducing the occupancy of various working conditions.

[0082] The present invention adopts a split antenna, which can effectively reduce the three-dimensional space in the transportation of the antenna, facilitate the installation and maintenance of the antenna, and has strong versatility.

[0083] The present invention realizes automatic opening of the main components, realizes the installation of the antenna, facilitates the installation and angle adjustment of the antenna, and reduces manual workload.

[0084] The present invention can effectively use the mountain as a cover to realize the confusion of camouflage radar and guide misjudgment. The secondary radar is used as the main working radar to protect the high-precision main radar, realize hierarchical response and avoid exposure. It reduces dependence on the mountain and avoids collapse. The internal equipment can be transported by crane.

[0085] The method of the present invention is flexible and meets various working conditions, thereby meeting all aspects of installation, debugging and work.

[0086] The beneficial effects are explained in conjunction with specific implementation methods. BRIEF DESCRIPTION OF THE DRAWINGS

[0087] Figure 1 It is a schematic diagram of the array principle of the radar antenna of the present invention.

[0088] Figure 2 It is a structural schematic diagram of the suspended top beam of the present invention.

[0089] Figure 3 It is a schematic structural diagram of the radar assembly of the present invention.

[0090] Figure 4 It is a schematic diagram of the use structure of the radar base of the present invention.

[0091] Figure 5 It is a schematic diagram of the structure of the adjusting connecting rod portion of the present invention.

[0092] Figure 6 It is a schematic diagram of the positive parallelogram motion of the adjusting connecting rod part of the present invention.

[0093] Figure 7It is a schematic diagram of the anti-parallelogram motion of the adjusting connecting rod part of the present invention.

[0094] Figure 8 It is a schematic diagram of the antiparallelogram motion adjustment of the radar assembly of the present invention.

[0095] Fig. 9 It is a structural schematic diagram of the main swing rod A of the present invention.

[0096] Fig.10 It is a schematic diagram of the structure of the driven drive shaft of the present invention.

[0097] Fig.11 It is a structural schematic diagram of the sliding gear A of the present invention.

[0098] Fig.12 It is a schematic diagram of the use structure of the longitudinal drive rod of the present invention.

[0099] Fig.13 It is a schematic diagram of the usage structure of the radar antenna of the present invention.

[0100] Fig.14 It is a schematic structural diagram of the radar antenna of the present invention.

[0101] Fig.15 It is a schematic structural diagram of the radar antenna accessory of the present invention.

[0102] Fig.16 It is a schematic diagram of the three-dimensional structure of the radar antenna auxiliary component of the present invention.

[0103] Among them: 1. Auxiliary components; 2. Radar components; 300. Secondary radar station; 301. Secondary radar; 302. Main radar station; 303. Frame structure; 304. Side beam; 305. Suspended top beam; 306. Side door; 307. Main door. 100, frame assembly; 101, adjusting connecting rod; 102, adjusting swing part; 103, main swing rod A; 104, auxiliary swing rod B; 105, connecting rod C; 106, driven drive shaft; 107, active drive shaft; 108, sliding gear A; 109, intermediate wheel assembly; 110, swing gear shaft; 111, swing frame assembly; 112, longitudinal guide groove; 113, longitudinal drive rod; 114, first drive rod; 115, second drive rod; 116, fork part; 200, radar antenna part; 201, swing rod assembly; 202, antenna base part; 203, support seat part; 204, annular groove; 205, hinged connector; 206, rotating seat; 207, lifting support 1. The support assembly of the main rotating rod is as follows: 208. The main rotating rod support group; 209. The fixed articulated support member; 210. The rotating rod member; 211. The guide base; 212. The pulling base; 213. The annular guide ring A; 214. The annular guide ring B; 215. The fixed support seat; 216. The guide support member B; 217. The linked articulated rod A; 218. The first articulated rod A; 219. The second articulated rod B; 220. The limiting sleeve; 221. The articulated seat A; 222. The articulated seat B; 223. The third articulated rod C; 224. The linked articulated support rod B; 225. The articulated seat C; 226. The active connecting rod; 227. The connecting articulated rod D; 228. The connecting articulated seat D; 229. The antenna base; 230. The central lifting rod. DETAILED DESCRIPTION

[0104] like Figure 1-16 As shown, the radar shelter auxiliary engineering system of this embodiment includes a frame assembly 100, the bottom of which is connected to the foundation, and the foundation part is a conventional method; an adjustment connecting rod part 101 is provided on the frame assembly 100 to achieve the swing of the radar; an adjustment swinging part 102 is provided on the adjustment connecting rod part 101 to achieve the radar protruding outward or receiving an edge inward;

[0105] The adjusting link part 101 is a four-link mechanism, which is simplified in the figure, and bearings and fasteners are omitted.

[0106] A radar assembly 2 is provided on the adjusting swing portion 102 for conducting reconnaissance scanning.

[0107] As a specific description, the adjusting link part 101 includes a main swing rod A103 and a secondary swing rod B104 whose lower ends are respectively hingedly mounted on the frame assembly 100; a connecting rod C105 is hingedly mounted between the upper ends of the main swing rod A103 and the upper ends of the secondary swing rod B104.

[0108] There are two main swing rods A103 arranged in parallel, two auxiliary swing rods B104 arranged in parallel, and two connecting rods C105 arranged in parallel.

[0109] Two connecting rods C105 are arranged between the two main swing rods A103;

[0110] Two connecting rods C105 are arranged between the two auxiliary swing rods B104; thereby achieving stable support.

[0111] In order to achieve the change of driving mode, a driven drive shaft 106 and a swing gear shaft 110 are respectively provided on the frame assembly 100; the driven drive shaft 106 and the active drive shaft 107 are respectively connected to the corresponding motors through their respective corresponding clutch transmissions; the motor is on the frame assembly 100; thereby achieving driving.

[0112] The root of the driven drive shaft 106 is key-connected to the auxiliary swing rod B104; the root of the main swing rod A103 is key-connected to the active drive shaft 107; the key is preferably a spline type. It should be noted that it can be a fixed key or a sliding key and a matching self-locking positioning component, using conventional parts such as clutches, brakes, positioning blocks or limit supports.

[0113] In order to realize the swing control, a swing gear shaft 110 is hinged between the heads of the two main swing rods A103;

[0114] In order to achieve power transmission, a plurality of intermediate wheel assemblies 109 are provided on the main swing rod A103; of course, a chain can be used instead.

[0115] The active drive shaft 107 is provided with a sliding gear A108 or other clutch control methods;

[0116] As a specific description, the sliding gear A108 is transmission-connected to the swing gear shaft 110 through a plurality of intermediate gear assemblies 109;

[0117] The swing gear shaft 110 is key-connected to the adjustment swing portion 102 .

[0118] As an example, but not limited to this structure, a fork assembly is provided on the frame assembly 100 .

[0119] The fork assembly includes a first driving rod 114 disposed on the frame assembly 100 and a second driving rod 115 connected to the first driving rod 114 in a direction-changing manner;

[0120] A shift fork portion 116 is provided at the end of the second driving rod 115 for shifting the sliding gear A 108 to engage with or disengage from the corresponding intermediate gear assembly 109 .

[0121] In order to realize the longitudinal movement of the radar, increase the detection distance, and form an ingenious combination of relative coordinates and polar coordinates, the adjustment swing part 102 includes a swing frame group 111 connected to the swing gear shaft 110; a longitudinal guide groove 112 and a longitudinal driving rod 113 are provided on the swing frame group 111.

[0122] The radar assembly 2 is disposed in the longitudinal guide groove 112 and connected to the longitudinal driving rod 113 .

[0123] The rack assembly 100 is arranged in the mountain;

[0124] When in operation, the radar assembly 2 is located above the adjustment swing portion 102;

[0125] When converged, the radar assembly 2 is located above or below the adjustment swing portion 102 .

[0126] like Figure 1 The radar base operation process of this embodiment includes working steps:

[0127] In the working steps, the mountain gate is opened. First, the adjusting link part 101 is started to make a positive parallelogram motion to expose the head end of the main swing rod A103 from the mountain gate; then, an anti-parallelogram motion is made around the adjusting link part 101, so that the main swing rod A103 continues to swing upward and protrude to the set position; thereby saving space and realizing the detection of the radar.

[0128] When performing a positive parallelogram motion, the driven drive shaft 106 is connected to the motor, and the active drive shaft 107 is connected to the motor;

[0129] When performing anti-parallelogram motion, the driven drive shaft 106 is separated from the motor, and the active drive shaft 107 is connected to the motor.

[0130] First, the active drive shaft 107 drives the two main swing rods A103 to swing to the set angle, and then drives the fork part 116 through the first drive rod 114 and the second drive rod 115, so that the sliding gear A108 is engaged with the corresponding intermediate wheel assembly 109; secondly, when the head end of the main swing rod A103 is exposed from the mountain gate, the swing gear shaft 110 drives the swing frame assembly 111 to swing forward; thirdly, the radar assembly 2 moves forward along the longitudinal guide groove 112 through the longitudinal drive rod 113, thereby realizing the ingenious movement of the radar.

[0131] After the working step, there is a convergence step; the convergence step is opposite to the working step, so as to collect the antenna to the edge of the mountain cavity.

[0132] The working steps are assisted by the radar shelter auxiliary engineering system.

[0133] When the radar assembly 2 needs to be replaced, the radar assembly 2 is separated from the longitudinal guide groove 112 and the longitudinal driving rod 113 for disassembly and assembly, thereby realizing a simple split modular setting.

[0134] like Figure 1 The components of the concealed radar antenna of this embodiment include an antenna base portion 202, which is used to be installed on a matching base; a swing arm component 201 is hinged on the antenna base portion 202;

[0135] A radar antenna unit 200 is provided on the swing arm assembly 201;

[0136] The swing arm assembly 201 has an open state and a gathered state. The open state is convenient for antenna installation, and the gathered state is convenient for transportation and replacement or storage when not in use.

[0137] The antenna base portion 202 is used to connect with the radar base;

[0138] The radar antenna part 200 is a pot-lid type antenna, which is not very convenient to match with radars of other structures;

[0139] A number of articulated connectors 205 are distributed on the back of the radar antenna section 200 to facilitate the connection of the articulated rods;

[0140] The hinged connection 205 is adjustable along the lateral busbar direction, and can be equipped with a limiting block, bolts and nuts or other limiting structures.

[0141] The swing arm assembly 201 includes a support base portion 203 disposed on an antenna base portion 202, which serves as a carrier, and which may have a built-in gear or motor to complete the rotation;

[0142] An annular groove 204 is provided on the support seat 203;

[0143] A pulling base 212 and a plurality of guide bases 211 are movable in the annular groove 204 to achieve the guiding operation;

[0144] A fixed support seat 215 is fixedly arranged in the annular groove 204 to achieve fixed support;

[0145] As a specific connection, for the convenience of description, the components are defined as follows: a main rotating rod support group 208 is hinged on the pulling base 212;

[0146] A linkage hinged rod is hinged on the guide base 211;

[0147] A fixed hinged support 209 is hinged on the support seat 203;

[0148] The upper ends of the main rotating rod support group 208, the linkage hinged rod and the fixed hinged support member 209 are hinged to the corresponding hinged connector 205;

[0149] The linkage hinged rod at least includes a plurality of linkage hinged rods A217 and linkage hinged support rods B224;

[0150] The pulling base 212, the fixed support base 215 and the guide base 211 are connected by concentric annular guide rings A213 and / or annular guide rings B214, thereby guiding them together to form a whole.

[0151] Guide holes matching the annular guide ring A213 and / or the annular guide ring B214 are respectively provided on the pulling base 212, the fixed support base 215 and the guide base 211, so as to facilitate the annular movement.

[0152] The main rotating rod support group 208, the linkage hinged rod A217, a plurality of linkage hinged support rods B224 and the fixed hinged support member 209 are arranged head to tail in sequence;

[0153] A first hinge rod A218 is hingedly connected to the fixed hinge support 209 via a hinge sleeve A;

[0154] A second hinged rod B219 is hingedly connected to the linkage hinged rod A217 via a hinge sleeve B;

[0155] The middle part of the second hinged rod B219 is hinged to the end of the first hinged rod A218 through a hinge seat A221;

[0156] A third hinged rod C223 is hingedly connected to the linkage hinged support rod B224 via a hinge sleeve C;

[0157] The middle part of the third hinged rod C223 is hinged to the end of the second hinged rod B219 through a hinged seat B222;

[0158] Between adjacent linked hinged support rods B224, the middle of the first third hinged rod C223 and the end of the second third hinged rod C223 are hinged via a hinge seat C225;

[0159] Between the linkage hinge support rod B224 and the main rotating rod support group 208,

[0160] An active connecting rod 226 is hingedly connected to the main rotating rod support group 208 via a hinge sleeve D;

[0161] A connecting hinge rod D227 is hingedly connected to the linkage hinge support rod B224 through a hinge sleeve B;

[0162] The connecting hinge rod D227 is hinged to the active connecting rod 226 via a connecting hinge seat D228.

[0163] The first hinge rod A218 is movably arranged on the hinge seat A221;

[0164] The hinge seat A221 is movably arranged on the second hinge rod B219;

[0165] The second hinge rod B219 is movably arranged on the hinge seat B222;

[0166] The hinge seat B222 is movably arranged on the third hinge rod C223;

[0167] The third hinge rod C223 is movably arranged on the corresponding hinge seat C225;

[0168] The hinge seat C225 is movably arranged on the corresponding third hinge rod C223;

[0169] The degree of articulation of its activities is adjusted according to the site.

[0170] The hinged seat A221, the hinged seat B222 and the hinged seat C225 have rotation angle limits to prevent the hinges from being opened too far and not being able to be fully opened;

[0171] The maximum opening angles of the active connecting rod 226 and the connecting hinge rod D227, the connecting hinge rod D227 and the third hinge rod C223, between adjacent third hinge rods C223, between the third hinge rod C223 and the second hinge rod B219, and between the second hinge rod B219 and the first hinge rod A218 are all acute angles and are staggered in height to avoid jamming or obstruction, making the opening and closing smoother.

[0172] As a rotation drive, a hollow rotating seat 206 is provided at the center of the upper part of the support seat 203;

[0173] The rotating seat 206 is connected to the main rotating rod support assembly 208 via a rotating rod 210 .

[0174] A central lifting rod 230 is provided at the center of the rotating base 206 to achieve lifting and lowering.

[0175] A lifting bracket 207 is provided at the upper end of the central lifting rod 230 for supporting the lower part of the radar antenna unit 200 .

[0176] The annular groove 204 is a T-shaped groove.

[0177] The first hinge rod A218 is provided with a limiting sleeve 220 located on both sides of the hinge sleeve A;

[0178] The second hinge rod B219 is provided with limiting sleeves 220 on both sides of the hinge sleeve B, thereby increasing flexibility and avoiding jamming.

[0179] An antenna base 229 is provided at the bottom of the radar antenna unit 200 to facilitate carrying and connection.

[0180] The lifting bracket 207 is used to lift the antenna base 229;

[0181] A plurality of guide support members B216 are provided on the support seat 203 ; the guide support members B216 move in a circular motion on the support seat 203 .

[0182] It adopts inner and outer ring guides to achieve more stable support and more reasonable force.

[0183] like Figure 1 As shown, the installation method for mountain radar antenna of this embodiment is based on the components of concealed radar antenna;

[0184] The installation method includes the following steps:

[0185] First, open the swing arm assembly 201;

[0186] Then, the radar antenna unit 200 is mounted on the swing arm assembly 201 .

[0187] During the first installation, the antenna base 202 is installed on the radar base. It can be installed quickly, simplifies the professionalism of the installation, is convenient for soldiers to operate, and is flexible and efficient.

[0188] When the radar antenna unit 200 is damaged, the radar antenna unit 200 is replaced on the swing arm assembly 201;

[0189] When transporting the components of the concealed radar antenna, the swing arm assembly 201 is folded to meet the requirements of different working conditions.

[0190] When the swing arm assembly 201 is opened, the rotating seat 206 is started, and the driving base 212 of the main rotating arm support group 208 is driven to rotate through the rotating rod 210, and under the guidance of the annular groove 204 and the annular guide ring A213 and / or the annular guide ring B214, the driving base 212 and the guide base 211 are driven to move forward along the arc; then, the connecting hinge rod D227 is driven to open in the forward movement through the active connecting rod 226, and the adjacent linked hinged support rod B224 is driven to move forward one by one in the arc; secondly, the adjacent third hinged rod C223 is driven forward and opened through the hinge seat C225, and the second hinged rod B219 is driven forward and opened through the third hinged rod C223, so that the linked hinged rod A217 and the linked hinged support rod B224 are opened;

[0191] The main rotating rod support group 208, the linkage hinged rod and the fixed hinged support 209 form a cone structure that supports the radar antenna part 200, thereby achieving support, providing counter-support through two rings, and reasonable force.

[0192] When it is necessary to fold it, the rotating seat 206 can be rotated in the reverse direction.

[0193] When installing the radar antenna unit 200, first, the lifting bracket 207 is raised through the central lifting rod 230 to support the antenna base 229; then, the position and angle of each articulated connector 205 are adjusted to connect with the corresponding active connecting rod 226, the linkage articulated support rod B224, the linkage articulated rod A217, and the upper end of the fixed articulated support 209; secondly, the central lifting rod 230 is lowered by a set distance so that the articulated connector 205 is subjected to force;

[0194] By supporting the rotation of the seat 203, the rotation of the radar is achieved as an extended protection.

[0195] like Figure 1 The radar shelter auxiliary engineering system of this embodiment is preferably built based on the above components, including a main radar station 302 and secondary radar stations 300 arranged around the main radar station 302; thereby realizing a radar matrix, thereby realizing a reasonable distribution of scanning.

[0196] As a basic structure, the main radar station 302 includes an auxiliary component 1 disposed in the mountain and a radar component 2 disposed on the auxiliary component 1;

[0197] The secondary radar station 300 is set up on the mountain around the radar assembly 2;

[0198] A secondary radar 301 is provided on the secondary radar station 300;

[0199] When the radar assembly 2 is in operation, the secondary radar 301 is activated.

[0200] A frame structure 303 located in the inner cavity of the mountain is provided on the auxiliary component 1;

[0201] The frame structure 303 is adapted to the space inside the mountain cavity;

[0202] A side beam 304 is arranged on the frame structure 303, and a suspended top beam 305 is arranged on the side beam 304, so as to realize bottom support without relying on the mountain, and at the same time, support the mountain to prevent collapse.

[0203] A mountain gate is provided on the frame structure 303;

[0204] The mountain gate includes a main gate 307 located in the middle and side gates 306 located on both sides of the main gate 307, so as to be adjusted according to the situation.

[0205] When the main door 307 and the side door 306 are opened, they are used to send the radar assembly 2 out of the mountain.

[0206] A radar shelter auxiliary engineering system is provided in the frame structure 303;

[0207] The radar component 2 is arranged on the radar shelter auxiliary engineering system.

[0208] As a whole protection, based on the whole of the above embodiment, the radar assembly 2 includes an antenna base portion 202; a swing arm assembly 201 is hinged on the antenna base portion 202;

[0209] A radar antenna unit 200 is provided on the swing arm assembly 201;

[0210] The swing arm assembly 201 has an open state and a closed state.

[0211] In order to interfere with enemy detection, the secondary radar 301 simulates the appearance of the radar antenna section 200 of the primary radar station 302 .

[0212] In order to protect the main radar and reduce its loss, in non-wartime state, the secondary radar 301 is in operation; in wartime state, the radar antenna unit 200 is in operation.

[0213] In order to facilitate engineering operations in the mountains, a crane is installed on the suspended top beam 305 to assist in disassembling and assembling the radar antenna unit 200 .

[0214] In order to serve as a false target as a substitute, a dummy radar is set around the secondary radar 301.

[0215] like Figure 1 The radar concealed mountain operation engineering method of this embodiment preferably uses the above-mentioned equipment and method steps, mainly using the radar shelter auxiliary engineering system; the method includes non-wartime working steps and wartime steps;

[0216] In the non-wartime working procedure, the secondary radar 301 is activated; the main radar station 302 is in a closed state;

[0217] As a protection of the operation method, in the wartime step, the secondary radar 301 is started and the main radar station 302 is started intermittently; the main radar station 302 and the secondary radar 301 form a radar matrix.

[0218] The power of the secondary radar 301 is lower than that of the primary radar station 302;

[0219] The scanning range of the secondary radar 301 is smaller than that of the primary radar station 302;

[0220] The scanning accuracy of the secondary radar 301 is lower than that of the primary radar station 302 .

[0221] First, scanning is performed through the secondary radar 301. When it is necessary to locate the scanned object, the main radar station 302 is started to perform a secondary scan and positioning on the scanned object to obtain the motion parameters, shape parameters and quantity of the scanned object.

[0222] When starting the operation of the main radar station 302, the mountain gate is opened, and the auxiliary component 1 sends the radar component 2 out of the mountain gate; and the above-mentioned radar base operation process is executed.

[0223] When a scanning object is located close to the area where the main radar station 302 is located, the scanning information of the same band is transmitted by simulating the radar, and the radar component 2 is converged into the mountain through the auxiliary component 1 and the mountain gate is closed; the secondary radar 301 is closed.

[0224] When the radar antenna unit 200 fails, the radar assembly 2 is retracted into the mountain; the radar antenna unit 200 is replaced by a crane suspended on the top beam 305;

[0225] Execute the above-mentioned installation method for mountain radar antenna.

[0226] The present invention realizes the radar antenna protruding out of the mountain gate or converging in the mountain without occupying as little space as possible through the auxiliary component 1. The radar component 2 is convenient for transportation and installation by improving the auxiliary support, and is also convenient for repairing or iteratively updating the antenna in the limited space inside the mountain. The secondary radar station 300 uses inferior old radars for daily work, or discards radars as substitutes, so as to avoid the real main radar being accurately located in wartime, thereby greatly reducing the power consumption and operation of the main radar, extending its life, and enhancing its concealment. The secondary radar 301 can be reasonably arranged on the nearby hills or areas, and the main radar station 302 is generally used only in wartime to attack by surprise. , to increase the confusion, the frame structure 303 is set in the inner cavity of the mountain, and is fixed to the mountain as a whole by anchor rods. It is equipped with an anti-leakage layer and an anti-insect layer to prevent damage to the plant root system and collapse. The accompanying drawings are only for illustrative purposes, not for limitation. There are also a large number of construction operations such as foundations in the mountains. It is a universal component and can be constructed according to the terrain. The side beams 304 are used to imitate the top of the mountain. The suspended top beams 305 are installed with manipulators, cranes, or wire wheels to complete the supporting operation and maintenance of the radar. The side doors 306 and the main door 307 are used as the mountain gates. Camouflage is set on the outside to achieve closing or opening, which is convenient for the protection and operation of the radar.

[0227] The present invention improves the accessories of the radar antenna part 200, which is convenient for quick disassembly and assembly, convenient for transportation, and reduces installation time. When the radar antenna is not in use, the swing arm assembly 201 can be collected and stored to reduce the space occupied. The antenna base part 202 is convenient for installation with the base, the support seat part 203 can be installed and adjusted, the annular groove 204 can achieve reversing guidance, the articulated connection part 205 can achieve articulated quick installation, the rotating seat 206 pulls the rotating rod part 210, which can realize rotational drive by a motor or gear, etc., the lifting bracket 207 can realize threaded clamping or plug-in, etc., the main rotating rod support group 208 can be pulled, and a multi-link is used to form a herringbone traction, and the fixed articulated support part 209 is used as a fixed support. It adopts a pulling base 212 and a guide base 211 to realize guide support, an annular guide ring A213 and an annular guide ring B214 to realize guide support, and a fixed support seat 215 is fixed by a top screw or a connecting piece. As a preferred embodiment, in order to realize better guidance, another annular groove is provided through the inner ring, and a guide support member B216 is placed to realize double guidance. The overall support is realized by the linkage of the articulated rod A217, the first articulated rod A218, the second articulated rod B219, the limit sleeve 220, the articulated seat A221, the articulated seat B222, the third articulated rod C223, the linkage articulated support rod B224, the articulated seat C225, the active connecting rod 226, the connecting articulated rod D227, and the connecting articulated seat D228, so as to facilitate better opening, and realize the support of the lifting support seat 207 and the antenna bottom support 229 by the central lifting rod 230. The present invention realizes the centralized collection of the connection and the opening when using it through the traction type connecting rod mechanism, which is convenient for transportation.

[0228] The present invention supports the whole through the frame assembly 100, and cleverly adjusts the connecting rod part 101 to cleverly design, and utilizes the smooth swing of the regular parallelogram in the mountain. When the radar component 2 is swung out, the anti-parallelogram is used to achieve the radar component 2 to reach the set position. Compared with a single regular parallelogram mechanism, it can achieve a smoother protrusion of the radar component 2 to avoid getting stuck. Compared with the anti-parallelogram mechanism, it can achieve the upward swing and contraction of the radar component 2 in the mountain, save space, and achieve a superposition effect. By coordinating and adjusting the swing part 102, polar coordinates are established to further increase the protrusion distance of the radar component 2.

[0229] As a specific structure, it realizes a connecting rod mechanism through a main swing rod A103, a secondary swing rod B104, and a connecting rod C105, realizes a positive parallelogram and an anti-parallelogram mechanism through a driven drive shaft 106 and an active drive shaft 107 to realize the detection and convergence of the radar, and in the convergence process, realizes that the inner cavity space of the mountain is occupied as little as possible, and the sliding gear A108 can be three gears or two gears, and the transmission is realized through the intermediate wheel assembly 109 and the chain, belt and gear. The swing gear shaft 110 realizes the swing of the swing frame group 111, and the radar movement adjustment is realized through the longitudinal guide groove 112 and the longitudinal drive rod 113. The fork part 116 is realized through the first drive rod 114 and the second drive rod 115, and the movement of the sliding gear A108 is realized to achieve clutch.

[0230] The present invention is fully described for a clearer disclosure, and the prior art is not listed one by one.

[0231] 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; although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or replace some of the technical features therein with equivalents; it is obvious for those skilled in the art to combine multiple technical solutions of the present invention. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention. The technical contents not described in detail in the present invention are all known technologies.

Claims

1. A radar concealed mountain operation engineering method, characterized in that: With the aid of radar shelter auxiliary engineering system; the method includes non-wartime work steps and wartime steps; In the non-wartime working procedure, the secondary radar (301) is activated; the main radar station (302) is in a closed state; In the wartime step, the secondary radar (301) is started, and the main radar station (302) is started intermittently; the main radar station (302) and the secondary radar (301) form a radar matrix.

2. The radar concealed mountain operation engineering method according to claim 1 is characterized by: The power of the secondary radar (301) is lower than that of the primary radar station (302); The scanning range of the secondary radar (301) is smaller than that of the primary radar station (302); The scanning accuracy of the secondary radar (301) is lower than that of the primary radar station (302).

3. The radar concealed mountain operation engineering method according to claim 2 is characterized by: First, scanning is performed through the secondary radar (301). When it is necessary to locate the scanned object, the main radar station (302) is started to perform a secondary scan and locate the scanned object to obtain the motion parameters, shape parameters and quantity of the scanned object.

4. The radar concealed mountain operation engineering method according to claim 3 is characterized by: When starting the operation of the main radar station (302), the mountain gate is opened, and the auxiliary component (1) sends the radar component (2) out of the mountain gate; and the radar base operation process is executed.

5. The radar concealed mountain operation engineering method according to claim 4 is characterized in that: When a scanning object is located close to the area where the main radar station (302) is located, the radar is simulated to transmit scanning information of the same band, and the radar component (2) is converged into the mountain through the auxiliary component (1) and the mountain gate is closed; the secondary radar (301) is closed.

6. The radar concealed mountain operation engineering method according to claim 5 is characterized by: When the radar antenna unit (200) fails, the radar assembly (2) is retracted into the mountain; the radar antenna unit (200) is replaced by a crane suspended on the top beam (305); Perform an installation method for a mountain radar antenna.

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