WO2023023993A1 - 一种便于调节的航空航天用雷达固定装置 - Google Patents
一种便于调节的航空航天用雷达固定装置 Download PDFInfo
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- WO2023023993A1 WO2023023993A1 PCT/CN2021/114615 CN2021114615W WO2023023993A1 WO 2023023993 A1 WO2023023993 A1 WO 2023023993A1 CN 2021114615 W CN2021114615 W CN 2021114615W WO 2023023993 A1 WO2023023993 A1 WO 2023023993A1
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- fixedly installed
- hole
- mounting
- aerospace
- rod
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- 238000009434 installation Methods 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 description 10
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
Definitions
- the invention relates to the technical field of radar, in particular to an easily adjustable aerospace radar fixing device.
- Radar means “radio detection and ranging", that is, using radio methods to find targets and determine their spatial positions. Therefore, radar is also called “radio positioning”. It is an electronic device that uses electromagnetic waves to detect targets. Radar emits electromagnetic waves to The target irradiates and receives its echo, thereby obtaining the distance from the target to the electromagnetic wave emission point, the distance change rate (radial velocity), azimuth, height and other information.
- radar In the prior art, multiple bolts are usually used to fix the radar. The fixing operation is cumbersome, and after fixing, it is not convenient to adjust the angle of the radar, and it is inconvenient to use. Therefore, we propose an easy-to-adjust aerospace radar Fixtures are used to solve the above problems.
- the purpose of the present invention is to solve the disadvantages that in the prior art, a plurality of bolts are usually used to fix the radar, and the fixing operation is cumbersome, and after fixing, it is not convenient to adjust the angle of the radar, and it is inconvenient to use.
- Regulated aerospace radar fixture
- an easily adjustable aerospace radar fixing device including a bottom plate, the top of the bottom plate is fixedly connected with the top of the support column, and the top of the support column is rotatably installed with a mounting seat , one side of the mounting seat is fixedly installed with an L-shaped plate, and one side of the L-shaped plate is provided with a chute.
- the bottom of the template is fixedly installed with a rotating disc
- the outer thread of the first threaded rod is installed with a sliding seat, which is slidably connected in the chute
- a motor is fixedly installed on one side of the sliding seat
- the output shaft of the motor is fixedly connected with a first
- a through hole is opened on one side of the mounting seat
- a worm and a rotating shaft are installed in the through hole and the bottom of the mounting seat respectively, and one end of the worm extends to the outside of the mounting seat and is fixedly installed with a second gear with one end of the rotating shaft.
- Each of the second gears is meshed with the first gear, and the other end of the rotating shaft and the outer side of the support column are respectively fixed with a first bevel gear and a second bevel gear, and the first bevel gear is meshed with the second bevel gear.
- one end of the L-shaped rod is fixedly installed on the top and bottom of the sliding seat, and the other ends of the two L-shaped rods are fixedly installed with limit racks, and the two limit racks are respectively movably meshed with the corresponding second gears.
- the bottom inner wall of the bottom of the through hole is rotatably installed with the bottom ends of two second threaded rods, and the outer sides of the two second threaded rods are fixedly installed with worm gears, and the worms are meshed with the two worm gears, and the top of the mounting seat is provided with two vertical holes, the tops of the two second threaded rods extend into the corresponding vertical holes and the moving sleeves are threadedly installed, the two moving sleeves are slidably connected in the corresponding vertical holes, and the tops of the two moving sleeves both extend to the mounting base
- a mounting hole is provided on the inner wall of the bottom of the chute, and the outer ring of the bearing is fixedly installed in the mounting hole, and the first threaded rod is fixedly socketed with the inner ring of the bearing, so that the first threaded rod can be rotated and installed.
- the top of the sliding seat is provided with a threaded hole, and the sliding seat is screwed on the outside of the first threaded rod through the threaded hole, so as to facilitate threaded installation of the sliding seat.
- a limit rod is fixedly installed on the bottom of the L-shaped plate, and the sliding seat is slidably connected to the outside of the limit rod, so as to limit the sliding seat to a certain extent.
- two fixing plates are fixedly installed in the through hole, and the worm is rotatably installed on the inside of the two fixing plates, so as to facilitate the rotatable installation of the worm.
- the outer side of the rotating shaft is rotatably mounted with a bushing, the top of the bushing is fixedly mounted with the bottom end of the fixing rod, and the top end of the fixing rod is fixedly mounted at the bottom of the mounting seat, so as to facilitate the rotating installation of the rotating shaft.
- a limiting groove is provided on the inner wall of one side of the vertical hole, and a limiting block is fixedly installed on one side of the moving sleeve, and the limiting block is slidably connected in the limiting groove, so as to limit the moving sleeve to a certain extent.
- the top of the mounting seat is provided with a plurality of positioning slots, and the bottom of the mounting plate is fixedly installed with a plurality of positioning rods, and the plurality of positioning rods are slidably connected in the corresponding positioning slots, so as to facilitate the positioning and placement of the mounting plate.
- the easily adjustable aerospace radar fixing device drives the first gear to rotate by starting the motor, so that it can be driven by the meshing transmission between the first gear and the second gear located above.
- the worm rotates, and then can drive the two second threaded rods to rotate through the meshing transmission between the worm and the two worm wheels, and then can drive the two moving sleeves to drive the two threaded rods through the meshing transmission between the moving sleeve and the second threaded rod.
- the said a kind of easy-to-adjust aerospace radar fixing device can drive the motor to move downward by rotating the rotating disc to drive the first threaded rod to rotate, and through the threaded connection between the sliding seat and the first threaded rod, so that The motor drives the first gear to separate from the upper second gear and meshes with the lower second gear, and at the same time, the lower limit rack can be moved downward to separate from the lower second gear, and can make The limit rack located at the top moves down to contact and mesh with the second gear located at the top, and then the motor can be started, and the rotating shaft can be driven to rotate through the meshing transmission of the first gear and the second gear located at the bottom, and then can Through the meshing transmission of the first bevel gear and the second bevel gear, and the
- Fig. 1 is a schematic structural view of a conveniently adjustable aerospace radar fixing device proposed by the present invention
- Fig. 2 is a structural schematic diagram of part A of a conveniently adjustable aerospace radar fixing device proposed by the present invention
- Fig. 3 is A schematic structural view of part B of a conveniently adjustable aerospace radar fixing device proposed by the present invention
- Fig. 4 is a structural schematic diagram of part C of a conveniently adjustable aerospace radar fixing device proposed by the present invention
- Fig. 5 is A structural schematic diagram of part D of an easily adjustable aerospace radar fixing device proposed by the present invention.
- an easily adjustable aerospace radar fixing device includes a bottom plate 1, the top of the bottom plate 1 is fixedly connected to the top of a support column 2, and the top of the support column 2 is rotatably installed with a mounting seat 3, and the mounting seat 3
- One side of the L-shaped plate 4 is fixedly installed, and one side of the L-shaped plate 4 is provided with a chute 5, and the top inner wall of the chute 5 is rotatably connected with the top end of the first threaded rod 6, and the bottom end of the first threaded rod 6
- the outer thread of the first threaded rod 6 is provided with a sliding seat 8, the sliding seat 8 is slidably connected in the chute 5, and one side of the sliding seat 8
- the two second gears 15 are movably meshed with the first gear 11.
- the first bevel gear 16 and the second bevel gear 17 are fixedly installed respectively, the first bevel gear 16 and the second bevel gear 17 are meshed, and the top and bottom of the slide seat 8 are fixedly equipped with L-shaped rods 18.
- One end, the other end of two L-shaped rods 18 are all fixedly installed limit racks 19, and two limit racks 19 are movably meshed with corresponding second gears 15 respectively.
- the bottom end of the second threaded rod 20, the outer sides of the two second threaded rods 20 are fixedly equipped with worm gears 21, the worm screw 13 is engaged with the two worm gears 21, and the top of the mounting seat 3 is provided with two vertical holes 22, two vertical holes 22 are provided on the top of the two second threaded rods 20.
- the top of the second threaded rod 20 extends into the corresponding vertical hole 22 and is threaded with a moving sleeve 23, and the two moving sleeves 23 are slidably connected in the corresponding vertical hole 22, and the tops of the two moving sleeves 23 all extend
- the bottom of the two top plates 24 is fixedly installed with a clamping rod 25
- the top of the mounting base 3 is movably installed with a mounting plate 26
- the top of the mounting plate 26 is fixedly installed with a radar body 27
- Both sides of the top of the mounting base 3 are provided with slots 28
- the two levers 25 are movably connected in the corresponding slots 28 .
- the bottom inner wall of the chute 5 is provided with a mounting hole, the outer ring of the bearing is fixedly installed in the mounting hole, and the first threaded rod 6 is fixedly socketed with the inner ring of the bearing, which is convenient for rotating and installing the first threaded rod 6 and the sliding seat 8.
- the top is provided with a threaded hole, and the sliding seat 8 is threadedly installed on the outside of the first threaded rod 6 through the threaded hole, which is convenient for threaded installation of the sliding seat 8.
- the bottom of the L-shaped plate 4 is fixedly installed with a limit rod 9, and the sliding seat 8 is slidably connected to the limit.
- the outer side of the position rod 9 plays a certain position-limiting effect on the sliding seat 8.
- Two fixing plates are fixedly installed in the through hole 12, and the worm 13 is rotatably installed on the inner side of the two fixing plates, which is convenient for rotating and installing the worm 13 and the rotating shaft 14.
- the outer side of the shaft sleeve is rotated and installed with a shaft sleeve, and the top of the shaft sleeve is fixedly installed with the bottom end of the fixed rod.
- Position groove, one side of the moving sleeve 23 is fixedly installed with a limit block, and the limit block is slidably connected in the limit groove, which plays a certain position-limiting effect on the moving sleeve 23.
- the top of the mounting seat 3 is provided with a plurality of positioning grooves
- the bottom of the mounting plate 26 is fixedly equipped with a plurality of positioning rods, and the plurality of positioning rods are slidably connected in the corresponding positioning grooves, so as to facilitate the positioning and placement of the mounting plate 26 .
- the radar body 27 when in use, can be placed on the top of the mounting base 3 through a plurality of positioning rods and a plurality of positioning grooves and the mounting plate 26, and then the motor 10 can be started to drive the first gear 11 to rotate, Thereby, the meshing transmission of the first gear 11 and the second gear 15 located above can drive the worm screw 13 to rotate, and then can drive the two second threaded rods through the meshing transmission of the worm screw 13 and the two worm wheels 21. 20 rotates, and then through the engagement transmission of the moving sleeve 23 and the second threaded rod 20, the two moving sleeves 23 drive the two top plates 24 to move downward, and then the top plate 24 drives the two clamping rods 25 to move downward.
- the engagement transmission between the first gear 11 and the second gear 15 located below can drive the rotating shaft 14 to rotate, and then can pass through the engagement transmission between the first bevel gear 16 and the second bevel gear 17, and the mounting seat 3 and the support column 2, the mounting base 3 can be driven to rotate, and then the angle of the radar body 27 can be adjusted.
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
一种便于调节的航空航天用雷达固定装置，包括底板(1)，底板(1)的顶部固定连接有支撑柱(2)的底端，支撑柱(2)的顶端转动安装有安装座(3)，安装座(3)的一侧固定安装有L型板(4)，L型板(4)的一侧开设有滑槽(5)，滑槽(5)的顶部内壁上转动连接有第一螺纹杆(6)的顶端，第一螺纹杆(6)的底端延伸至L型板(4)的下方并固定安装有转动盘(7)。装置结构设计合理，操作简单，便于对雷达本体进行固定，便于对雷达本体的角度进行调节使用，且只使用一个电机，降低了对能源的损耗，使用方便。
Description
本发明涉及雷达技术领域，尤其涉及一种便于调节的航空航天用雷达固定装置。
雷达意思为"无线电探测和测距"，即用无线电的方法发现目标并测定它们的空间位置，因此，雷达也被称为“无线电定位”，是利用电磁波探测目标的电子设备，雷达发射电磁波对目标进行照射并接收其回波，由此获得目标至电磁波发射点的距离、距离变化率(径向速度)、方位、高度等信息。然而，在现有技术中通常采用多个螺栓对雷达进行固定，固定操作繁琐，且固定后，不便于对雷达的角度进行调节，使用不便，因此我们提出了一种便于调节的航空航天用雷达固定装置用于解决上述问题。
本发明的目的是为了解决在现有技术中通常采用多个螺栓对雷达进行固定，固定操作繁琐，且固定后，不便于对雷达的角度进行调节，使用不便的缺点，而提出的一种便于调节的航空航天用雷达固定装置。
为了实现上述目的，本发明采用了如下技术方案：一种便于调节的航空航天用雷达固定装置，包括底板，所述底板的顶部固定连接有支撑柱的顶端，支撑柱的顶端转动安装有安装座，安装座的一侧固定安装有L型板，L型板的一侧开设有滑槽，滑槽的顶部内壁上转动连接有第一螺纹杆的顶端，第一螺纹杆的底端延伸至L型板的下方并固定安装有转动盘，第一螺纹杆的外侧螺纹安装有滑座，滑动连接在滑槽内，滑座的一侧固定安装有电机，电机的输出轴上固定连接有第一齿轮，安装座的一侧开设有通孔，通孔内与安装座的底部分别转动安装有蜗杆与转轴，蜗杆的一端延伸至安装座外并与转轴的一端均固定安装有第二齿轮，两个第二齿轮均与第一齿轮活动啮合，转轴的另一端与支撑柱的外侧分别固定安装有第一锥形齿轮与第二锥形齿轮，第一锥形齿轮与第二锥形齿轮相啮合，滑座的顶部与底部均固定安装有L型杆的一端，两个L型杆的另一端均固定安装有限位齿条，两个限位齿条分别与相对应的第二齿轮活动啮合，通孔的底部内壁上转动安装有两个第二螺纹杆的底端，两个第二螺纹杆的外侧均固定安装有蜗轮，蜗杆与两个蜗轮相啮合，安装座的顶部开设有两个竖孔，两个第二螺纹杆的顶端延伸至相对应的竖孔内并螺纹安装有移动套，两个移动套滑动连接在相对应的竖孔内，两个移动套的顶部均延伸至安装座的上方并固定安装有顶板，两个顶板的底部均固定安装有卡杆，安装座的顶部活动安装有安装板，安装板的顶部固定安装有雷达本体，安装座的顶部两侧均开设有卡槽，两个卡杆活动连接在相对应的卡槽内。
优选的，所述滑槽的底部内壁上开设有安装孔，安装孔内固定安装有轴承的外圈，第一螺纹杆与轴承的内圈固定套接，便于转动安装第一螺纹杆。优选的，所述滑座的顶部开设有螺纹孔，滑座通过螺纹孔螺纹安装在第一螺纹杆的外侧，便于螺纹安装滑座。优选的，所述L型板的底部固定安装有限位杆，滑座滑动连接在限位杆的外侧，对滑座起到一定的限位作用。优选的，所述通孔内固定安装有两个固定板，蜗杆转动安装在两个固定板的内侧，便于转动安装蜗杆。优选的，所述转轴的外侧转动安装有轴套，轴套的顶部固定安装有固定杆的底端，固定杆的顶端固定安装在安装座的底部，便于转动安装转轴。优选的，所述竖孔的一侧内壁上开设有限位槽，移动套的一侧固定安装有限位块，限位块滑动连接在限位槽内，对移动套起到一定的限位作用。优选的，所述安装座的顶部开设有多个定位槽，安装板的底部固定安装有多个定位杆，多个定位杆滑动连接在相对应的定位槽内，便于对安装板的定位放置。本发明中，所述的一种便于调节的航空航天用雷达固定装置，通过启动电机，带动第一齿轮转动，从而即可通过第一齿轮与位于上方的第二齿轮的啮合传动，即可带动蜗杆转动，进而可以通过蜗杆与两个蜗轮的啮合传动，即可带动两个第二螺纹杆转动，进而可以通过移动套与第二螺纹杆的啮合传动，即可使得两个移动套带动两个顶板向下移动，进而通过顶板带动两个卡杆向下移动，并滑进相对应的卡槽内，从而即可完成对雷达本体的固定，操作简单，便于对雷达本体的固定；本发明中，所述的一种便于调节的航空航天用雷达固定装置，通过转动转动盘带动第一螺纹杆转动，通过滑座与第一螺纹杆的螺纹连接，即可带动电机向下移动，从而即可使得电机带动第一齿轮与位于上方的第二齿轮分离并与位于下方的第二齿轮相啮合，同时可以通过位于下方的限位齿条向下移动与位于下方的第二齿轮分离，并且可以使得位于上方的限位齿条向下移动与位于上方的第二齿轮相接触啮合，随即即可启动电机，通过第一齿轮与位于下方的第二齿轮的啮合传动，即可带动转轴转动，进而可以通过第一锥形齿轮与第二锥形齿轮的啮合传动，以及安装座与支撑柱的转动连接，即可带动安装座转动，进而可以对雷达本体的角度进行调节，便于对雷达本体的角度进行调节；本发明结构设计合理，操作简单，便于对雷达本体进行固定，且便于对雷达本体的角度进行调节使用，且只使用一个电机，降低了对能源的损耗，使用方便。
图1为本发明提出的一种便于调节的航空航天用雷达固定装置的结构示意图；图2为本发明提出的一种便于调节的航空航天用雷达固定装置的A部分的结构示意图；图3为本发明提出的一种便于调节的航空航天用雷达固定装置的B部分的结构示意图；图4为本发明提出的一种便于调节的航空航天用雷达固定装置的C部分的结构示意图；图5为本发明提出的一种便于调节的航空航天用雷达固定装置的D部分的结构示意图。图中：1、底板；2、支撑柱；3、安装座；4、L型板；5、滑槽；6、第一螺纹杆；7、转动盘；8、滑座；9、限位杆；10、电机；11、第一齿轮；12、通孔；13、蜗杆；14、转轴；15、第二齿轮；16、第一锥形齿轮；17、第二锥形齿轮；18、L型杆；19、限位齿条；20、第二螺纹杆；21、蜗轮；22、竖孔；23、移动套；24、顶板；25、卡杆；26、安装板；27、雷达本体；28、卡槽。
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。参照图1-5，一种便于调节的航空航天用雷达固定装置，包括底板1，底板1的顶部固定连接有支撑柱2的顶端，支撑柱2的顶端转动安装有安装座3，安装座3的一侧固定安装有L型板4，L型板4的一侧开设有滑槽5，滑槽5的顶部内壁上转动连接有第一螺纹杆6的顶端，第一螺纹杆6的底端延伸至L型板4的下方并固定安装有转动盘7，第一螺纹杆6的外侧螺纹安装有滑座8，滑座8滑动连接在滑槽5内，滑座8的一侧固定安装有电机10，电机10的输出轴上固定连接有第一齿轮11，安装座3的一侧开设有通孔12，通孔12内与安装座3的底部分别转动安装有蜗杆13与转轴14，蜗杆13的一端延伸至安装座3外并与转轴14的一端均固定安装有第二齿轮15，两个第二齿轮15均与第一齿轮11活动啮合，转轴14的另一端与支撑柱2的外侧分别固定安装有第一锥形齿轮16与第二锥形齿轮17，第一锥形齿轮16与第二锥形齿轮17相啮合，滑座8的顶部与底部均固定安装有L型杆18的一端，两个L型杆18的另一端均固定安装有限位齿条19，两个限位齿条19分别与相对应的第二齿轮15活动啮合，通孔12的底部内壁上转动安装有两个第二螺纹杆20的底端，两个第二螺纹杆20的外侧均固定安装有蜗轮21，蜗杆13与两个蜗轮21相啮合，安装座3的顶部开设有两个竖孔22，两个第二螺纹杆20的顶端延伸至相对应的竖孔22内并螺纹安装有移动套23，两个移动套23滑动连接在相对应的竖孔22内，两个移动套23的顶部均延伸至安装座3的上方并固定安装有顶板24，两个顶板24的底部均固定安装有卡杆25，安装座3的顶部活动安装有安装板26，安装板26的顶部固定安装有雷达本体27，安装座3的顶部两侧均开设有卡槽28，两个卡杆25活动连接在相对应的卡槽28内。滑槽5的底部内壁上开设有安装孔，安装孔内固定安装有轴承的外圈，第一螺纹杆6与轴承的内圈固定套接，便于转动安装第一螺纹杆6，滑座8的顶部开设有螺纹孔，滑座8通过螺纹孔螺纹安装在第一螺纹杆6的外侧，便于螺纹安装滑座8，L型板4的底部固定安装有限位杆9，滑座8滑动连接在限位杆9的外侧，对滑座8起到一定的限位作用，通孔12内固定安装有两个固定板，蜗杆13转动安装在两个固定板的内侧，便于转动安装蜗杆13，转轴14的外侧转动安装有轴套，轴套的顶部固定安装有固定杆的底端，固定杆的顶端固定安装在安装座3的底部，便于转动安装转轴14，竖孔22的一侧内壁上开设有限位槽，移动套23的一侧固定安装有限位块，限位块滑动连接在限位槽内，对移动套23起到一定的限位作用，安装座3的顶部开设有多个定位槽，安装板26的底部固定安装有多个定位杆，多个定位杆滑动连接在相对应的定位槽内，便于对安装板26的定位放置。
本发明中，在使用时，可以通过多个定位杆与多个定位槽并且通过安装板26将雷达本体27放置在安装座3的顶部，然后即可启动电机10，带动第一齿轮11转动，从而即可通过第一齿轮11与位于上方的第二齿轮15的啮合传动，即可带动蜗杆13转动，进而可以通过蜗杆13与两个蜗轮21的啮合传动，即可带动两个第二螺纹杆20转动，进而可以通过移动套23与第二螺纹杆20的啮合传动，即可使得两个移动套23带动两个顶板24向下移动，进而通过顶板24带动两个卡杆25向下移动，并滑进相对应的卡槽28内，从而即可完成对雷达本体27的固定，并且可以通过转动转动盘7带动第一螺纹杆6转动，通过滑座8与第一螺纹杆6的螺纹连接，即可带动电机10向下移动，从而即可使得电机10带动第一齿轮11与位于上方的第二齿轮15分离并与位于下方的第二齿轮15相啮合，同时可以通过位于下方的限位齿条19向下移动与位于下方的第二齿轮15分离，并且可以使得位于上方的限位齿条19向下移动与位于上方的第二齿轮15相接触啮合，随即即可启动电机10，通过第一齿轮11与位于下方的第二齿轮15的啮合传动，即可带动转轴14转动，进而可以通过第一锥形齿轮16与第二锥形齿轮17的啮合传动，以及安装座3与支撑柱2的转动连接，即可带动安装座3转动，进而可以对雷达本体27的角度进行调节。
在此处键入工业实用性描述段落。
以上显示和描述了本发明的基本原理和主要特征和本发明的优点，对于本领域技术人员而言，显然本发明不限于上述示范性实施例的细节，而且在不背离本发明的精神或基本特征的情况下，能够以其他的具体形式实现本发明。因此，无论从哪一点来看，均应将实施例看作是示范性的，而且是非限制性的，本发明的范围由所附权利要求而不是上述说明限定，因此旨在将落在权利要求的等同要件的含义和范围内的所有变化囊括在本发明内。不应将权利要求中的任何附图标记视为限制所涉及的权利要求。此外，应当理解，虽然本说明书按照实施方式加以描述，但并非每个实施方式仅包含一个独立的技术方案，说明书的这种叙述方式仅仅是为清楚起见，本领域技术人员应当将说明书作为一个整体，各实施例中的技术方案也可以经适当组合，形成本领域技术人员可以理解的其他实施方式。
Claims (1)
- 一种便于调节的航空航天用雷达固定装置，包括底板（1），其特征在于，所述底板（1）的顶部固定连接有支撑柱（2）的顶端，支撑柱（2）的顶端转动安装有安装座（3），安装座（3）的一侧固定安装有L 型板（4），L 型板（4）的一侧开设有滑槽（5），滑槽（5）的顶部内壁上转动连接有第一螺纹杆（6）的顶端，第一螺纹杆（6）的底端延伸至L 型板（4）的下方并固定安装有转动盘（7），第一螺纹杆（6）的外侧螺纹安装有滑座（8），滑座（8）滑动连接在滑槽（5）内，滑座（8）的一侧固定安装有电机（10），电机（10）的输出轴上固定连接有第一齿轮（11），安装座（3）的一侧开设有通孔（12），通孔（12）内与安装座（3）的底部分别转动安装有蜗杆（13）与转轴（14），蜗杆（13）的一端延伸至安装座（3）外并与转轴（14）的一端均固定安装有第二齿轮（15），两个第二齿轮（15）均与第一齿轮（11）活动啮合，转轴（14）的另一端与支撑柱（2）的外侧分别固定安装有第一锥形齿轮（16）与第二锥形齿轮（17），第一锥形齿轮（16）与第二锥形齿轮（17）相啮合，滑座（8）的顶部与底部均固定安装有L 型杆（18）的一端，两个L 型杆（18）的另一端均固定安装有限位齿条（19），两个限位齿条（19）分别与相对应的第二齿轮（15）活动啮合，通孔（12）的底部内壁上转动安装有两个第二螺纹杆（20）的底端，两个第二螺纹杆（20）的外侧均固定安装有蜗轮（21），蜗杆（13）与两个蜗轮（21）相啮合，安装座（3）的顶部开设有两个竖孔（22），两个第二螺纹杆（20）的顶端延伸至相对应的竖孔（22）内并螺纹安装有移动套（23），两个移动套（23）滑动连权利要求书2接在相对应的竖孔（22）内，两个移动套（23）的顶部均延伸至安装座（3）的上方并固定安装有顶板（24），两个顶板（24）的底部均固定安装有卡杆（25），安装座（3）的顶部活动安装有安装板（26），安装板（26）的顶部固定安装有雷达本体（27），安装座（3）的顶部两侧均开设有卡槽（28），两个卡杆（25）活动连接在相对应的卡槽（28）内。2、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述滑槽（5）的底部内壁上开设有安装孔，安装孔内固定安装有轴承的外圈，第一螺纹杆（6）与轴承的内圈固定套接。3、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述滑座（8）的顶部开设有螺纹孔，滑座（8）通过螺纹孔螺纹安装在第一螺纹杆（6）的外侧。4、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述L 型板（4）的底部固定安装有限位杆（9），滑座（8）滑动连接在限位杆（9）的外侧。5、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述通孔（12）内固定安装有两个固定板，蜗杆（13）转动安装在两个固定板的内侧。6、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述转轴（14）的外侧转动安装有轴套，轴套的顶部固定安装有固定杆的底端，固定杆的顶端固定安装在安装座（3）权利要求书3的底部。7、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述竖孔（22）的一侧内壁上开设有限位槽，移动套（23）的一侧固定安装有限位块，限位块滑动连接在限位槽内。8、根据权利要求1 所述的一种便于调节的航空航天用雷达固定装置，其特征在于，所述安装座（3）的顶部开设有多个定位槽，安装板（26）的底部固定安装有多个定位杆，多个定位杆滑动连接在相对应的定位槽内。
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| CN117054973B (zh) * | 2023-10-11 | 2023-12-12 | 深圳市金众工程检验检测有限公司 | 测绘工程用无线定向雷达设备 |
| CN117054973A (zh) * | 2023-10-11 | 2023-11-14 | 深圳市金众工程检验检测有限公司 | 测绘工程用无线定向雷达设备 |
| CN117401173A (zh) * | 2023-12-15 | 2024-01-16 | 山西成功通用航空股份有限公司 | 一种气象雷达挂飞装置 |
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