CN111397440A - Meteorological sounding rocket launcher - Google Patents
Meteorological sounding rocket launcher Download PDFInfo
- Publication number
- CN111397440A CN111397440A CN202010328938.1A CN202010328938A CN111397440A CN 111397440 A CN111397440 A CN 111397440A CN 202010328938 A CN202010328938 A CN 202010328938A CN 111397440 A CN111397440 A CN 111397440A
- Authority
- CN
- China
- Prior art keywords
- plate
- support
- bolt
- nut
- washer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000005540 biological transmission Effects 0.000 claims description 4
- 230000001681 protective effect Effects 0.000 claims description 4
- 230000005855 radiation Effects 0.000 claims 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 abstract description 3
- 229910052744 lithium Inorganic materials 0.000 abstract description 3
- 101100234547 Caenorhabditis elegans rod-1 gene Proteins 0.000 description 6
- 238000001514 detection method Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 210000000481 breast Anatomy 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
The invention discloses a meteorological sounding rocket launcher which comprises a connecting rod, a shaft pin A, a shaft pin B, a first washer, a first nut, a second nut, a direction finder, a supporting seat and a traction chassis, wherein the meteorological sounding rocket launcher is stable in integral structure and suitable for operation under severe weather conditions; the launching angle adjusting mechanism adopts a link mechanism which is transmitted by a motor driving screw rod; the direction finder adopts four guide rails to combine with the middle ring A and the middle ring B to form a launching track, the launching caliber is 122 mm, the maximum angle of the high and low incidence angles is not less than 80 degrees, the height of the launching frame is not more than 3m in a transportation state, and the stability is high; the supporting part adopts a motor to drive a trapezoidal screw shaft to rotate, drives the connecting rod to move back and forth so as to achieve the purpose of adjusting the launching angle, and can be quickly switched into a manual mode; and a rocket operation automatic recording parameter instrument or a wireless launch controller can be used for controlling, a high-energy lithium battery is carried, and the problem of field power supply is solved.
Description
Technical Field
The invention relates to the field related to meteorological sounding, in particular to a meteorological sounding rocket launcher.
Background
The sounding rocket is a rocket for carrying out detection and scientific experiments in a near-earth space, structural components and parameters of each layer of atmosphere can be detected in the height direction by using the sounding rocket, and the sounding rocket is an effective detection tool in severe weather conditions at high altitude.
At present, under the severe weather condition, when the sounding rocket is launched, the overall stability is poor, the launching angle is easy to deviate, so that the subsequent sounding rocket cannot reach the preset detection height, the scattering of ballistic vertexes and falling points cannot be reduced, the launching angle is inconvenient to adjust, the field power supply is difficult, and the subsequent meteorological sounding work is influenced.
Disclosure of Invention
Therefore, in order to solve the above-mentioned defects, the invention provides a meteorological sounding rocket launcher.
The invention is realized in such a way that a meteorological sounding rocket launcher is constructed, the device comprises a connecting rod, a shaft pin A, a shaft pin B, a first washer, a first nut, a second nut, a direction finder, a supporting seat and a traction chassis, one end of the top of the connecting rod is connected to the middle of the bottom of the direction finder, one end of the bottom side of the connecting rod is connected with one end of the supporting seat through the shaft pin B and is fixed at the joint through the first washer, the first nut and the second nut, the bottom end of the direction finder is connected with the other end of the supporting seat through the shaft pin A, and the supporting seat is installed on the traction chassis.
Preferably, the orientator comprises a middle ring A, a middle ring B, a first bolt, a second washer, a third nut, a second bolt, a fourth nut, a third washer, a front baffle, a guide rail seat, a support, a third bolt, a fifth nut, a fourth washer, a support, a first bottom plate, a rear baffle A, a binding post, a wiring board and a fourth bolt, wherein the middle ring A and the middle ring B are symmetrically arranged at the upper end of the first bottom plate in front and rear, the front baffle is connected with the rear baffle through the guide rail and the guide rail seat, the bottom of the guide rail seat is provided with the first bottom plate, the front end of the first bottom plate is connected with the front baffle and is fixed through the second bolt, the fourth nut and the third washer, the rear end of the first bottom plate is connected with the rear baffle and is fixed through the first bolt, the second washer and the third nut, the bottom of the first bottom plate is provided with the support, and the, and the rear baffle plate is provided with a rear baffle plate A, and the bottom of the rear baffle plate is provided with a binding post, a wiring board and a fourth bolt.
Preferably, the support base comprises a support plate A, a sliding seat, a sliding rail, a support plate B, a bearing, a trapezoidal screw shaft, a screw shaft sleeve, a support plate C, a motor, a support plate D, a gear A, a first connecting key, a fifth gasket, a gear B, a second connecting key, a fifth bolt, a sixth nut, a sixth gasket, a sixth bolt and a base, the support plate A is arranged on the rear side of the base and fixed through the sixth bolt and connected to the support at the rear part of the bottom of the orienter, the sliding rail is arranged on the base and fixed with the front side of the support plate A through the sliding seat, the support plate B is arranged in the middle of the base, one end of the trapezoidal screw shaft is connected with the upper end of the support plate B through the bearing, the other end of the trapezoidal screw shaft is connected to the support plate D, the bottom of the support plate C is sleeved on the trapezoidal screw shaft through the screw shaft sleeve, and the output shaft of the machine is connected with a gear A, the gear A and the gear B are respectively arranged on the outer side of the bearing plate D and are connected with a first connecting key and a second connecting key, the gear A and the gear B are in meshing transmission, the gear B is connected with the end part of the trapezoidal screw rod shaft and is fixed by a fifth washer, and the bottom of the machine base is connected with a traction chassis and is fixed by a fifth bolt, a sixth nut and a sixth washer.
Preferably, the traction chassis comprises a rear support leg, a bolt, a seventh nut, a seventh bolt, a telescopic rod, a frame, a second bottom plate, a tire assembly, a shield, a front support leg assembly, a protective plate, a traction assembly and an eighth bolt, the rear support leg is arranged at the bottom of one end of the telescopic rod and fixed with the seventh bolt through the seventh nut, the other end of the telescopic rod is connected with the frame, the second bottom plate is arranged on the frame and fixedly connected with the bottom of the frame in the supporting seat, the tire assembly is arranged in the middle of the bottom of the frame, the shield is arranged on the outer side of the bottom of the frame, the front support leg assembly is arranged at the bottom of the front end of the frame and fixedly installed through the protective plate, the front end of the protective plate is connected with the traction assembly, and.
Preferably, four guide rails are arranged on the direction finder, and the guide rails are combined into a launching track by matching with the middle ring A and the middle ring B, the launching caliber of the launching track is 122 mm, and the maximum high and low launching angles are not less than 80 degrees.
Preferably, the middle rings A and B are respectively provided with two, the distance between the two middle rings A is 1000mm, and the distance between the two middle rings B is 3000 mm.
Preferably, the distance between the through holes in the middle of the bottom of the support and the through holes in the middle of the support on the rear side is 1000mm, and the distance between the through holes in the middle of the support on the rear side of the support and the rear baffle is 500 mm.
Preferably, the height between the through hole at the upper end of the bearing plate A and the support plate body at the bottom of the machine base is 740mm, the length of the support plate body at the bottom of the machine base is 800mm, and the distance between the two slide rails is 400 mm.
Preferably, the width of the second bottom plate is 900mm, and the sum of the length of the second bottom plate and the guard plate is 2780 mm.
Preferably, the height of the launcher is not more than 3m in the transportation state.
Preferably, the bracket can be connected with a rocket operation automatic recording parameter instrument or a wireless launching controller for control.
The invention has the following advantages: the invention provides a meteorological sounding rocket launcher through improvement, compared with the same type of equipment, the meteorological sounding rocket launcher has the following improvements:
the method has the advantages that: the meteorological sounding rocket launcher is stable in overall structure and suitable for operation under severe weather conditions; the launching angle adjusting mechanism adopts a link mechanism which is transmitted by a motor driving screw rod.
The method has the advantages that: the invention relates to a meteorological sounding rocket launcher, wherein a direction finder adopts a launching track formed by combining four guide rails, a middle ring A and a middle ring B, the launching caliber is 122 mm, the maximum high-low launching angle is not less than 80 degrees, the height of the launcher in a transportation state is not more than 3m, and the launcher is high in stability.
The method has the advantages that: according to the meteorological sounding rocket launcher, the supporting part adopts the motor to drive the trapezoidal screw shaft to rotate, the connecting rod is driven to move back and forth so as to achieve the purpose of adjusting the launching angle, and the mode can be quickly switched to a manual mode.
The advantages are that: according to the meteorological sounding rocket launcher, fifty-bell 600P double-row seat lengthened breast boards are selected as the loading platform for light clamping, and the launcher main body is installed on a truck longitudinal beam through bolts and steel plates, so that the stability is improved.
The advantages are that: the meteorological sounding rocket launcher can be controlled by using a rocket operation automatic recording parameter instrument or a wireless launch controller, carries a high-energy lithium battery, and solves the field power supply problem.
Drawings
FIG. 1 is a general view of a rocket launcher of the present invention;
FIG. 2 is a schematic view of the front view of the direction finder of the present invention;
FIG. 3 is a schematic top view of the orienter of the present invention;
FIG. 4 is a schematic view of the left side of the present invention;
FIG. 5 is a schematic view of the right side of the director of the present invention;
FIG. 6 is a front view of the support base of the present invention;
FIG. 7 is a schematic top view of the backup pad of the present invention;
FIG. 8 is a front view schematic of the traction chassis of the present invention;
fig. 9 is a schematic top view of the traction chassis of the present invention.
Wherein: the connecting rod-1, the shaft pin A-2, the shaft pin B-3, the first washer-4, the first nut-5, the second nut-6, the orientator-7, the supporting seat-8, the traction chassis-9, the middle ring A-71, the middle ring B-72, the first bolt-73, the second washer-74, the third nut-75, the second bolt-76, the fourth nut-77, the third washer-78, the front baffle-79, the guide rail-710, the guide rail seat-711, the supporting member-712, the third bolt-713, the fifth nut-714, the fourth washer-715, the support-716, the first bottom plate-717, the rear baffle-718, the rear baffle A-719, the wiring post-720, the wiring board-721, the fourth bolt-722, the rear baffle-718, the wiring post-719, the wiring board-722, the wiring board-720, A support plate A-81, a slide seat-82, a slide rail-83, a support plate B-84, a bearing-85, a trapezoidal screw shaft-86, a screw shaft sleeve-87, a support plate C-88, a motor-89, a support plate D-810, a gear A-811, a first connecting key-812, a fifth gasket-813, a gear B-814, a second connecting key-815, a fifth bolt-816, a sixth nut-817, a sixth gasket-818, a sixth bolt-819, a stand-820, a rear support-91, a bolt-92, a seventh nut-93, a seventh bolt-94, a telescopic rod-95, a stand-96, a second bottom plate-97, a tire assembly-98, a shield-99, a front support assembly-910, a shield-911, a front support assembly-95, A traction assembly-912 and an eighth bolt-913.
Detailed Description
The present invention will be described in detail below with reference to fig. 1 to 9, and the technical solutions in the embodiments of the present invention will be clearly and completely described, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The invention provides a meteorological sounding rocket launcher through improvement, which comprises a connecting rod 1, a shaft pin A2, a shaft pin B3, a first washer 4, a first nut 5, a second nut 6, a direction finder 7, a supporting seat 8 and a traction chassis 9, wherein one end of the top of the connecting rod 1 is connected to the middle of the bottom of the direction finder 7, one end of the bottom side is connected with one end of the supporting seat 8 through the shaft pin B3 and fixed at the connection position through the first washer 4, the first nut 5 and the second nut 6, the bottom end of the direction finder 7 is connected with the other end of the supporting seat 8 through the shaft pin A2, and the supporting seat 8 is installed on the traction chassis 9.
Further, the orientator 7 comprises a middle ring A71, a middle ring B72, a first bolt 73, a second washer 74, a third nut 75, a second bolt 76, a fourth nut 77, a third washer 78, a front baffle 79, a guide rail 710, a guide rail seat 711, a support 712, a third bolt 713, a fifth nut 714, a fourth washer 715, a support 716, a first bottom plate 717, a back baffle 718, a back baffle A719, a wiring terminal 720, a wiring board 721 and a fourth bolt 722, wherein the middle ring A71 and the middle ring B72 are symmetrically arranged at the upper end of the first bottom plate 717 front and back, the front baffle 79 is connected with the back baffle 718 through the guide rail 710 and the guide rail seat 711, the bottom of the guide rail seat 711 is provided with the first bottom plate 717, the front end of the first bottom plate 717 is connected with the front baffle 79 and fixed through the second bolt 76, the fourth nut 77 and the third washer 78, the back end is connected with the back baffle 718 and fixed through the first bolt 73, the second washer 74 and the third nut 75, the support 716 is arranged at the bottom of, the middle and the rear side of the bottom of the bracket 716 are respectively provided with a support 712, fixed by a third bolt 713, a fifth nut 714 and a fourth washer 715, respectively connected to the connecting link 1 and the support base 8, the rear baffle 718 is provided with a rear baffle a719, and the bottom is provided with a binding post 720, a wiring board 721 and a fourth bolt 722.
Further, the support base 8 includes a support plate a81, a slide carriage 82, a slide rail 83, a support plate B84, a bearing 85, a trapezoidal screw shaft 86, a screw shaft sleeve 87, a support plate C88, a motor 89, a support plate D810, a gear a811, a first connecting key 812, a fifth washer 813, a gear B814, a second connecting key 815, a fifth bolt 816, a sixth nut 817, a sixth washer 818, a sixth bolt 819, and a base 820, a support plate a81 is provided on the rear side of the base 820 and fixed by the sixth bolt 819 and connected to a support 712 at the bottom rear of the orienter 7, the base 820 is provided with the slide rail 83 and fixed to the front side of the support plate a81 by the slide carriage 82, the middle portion is provided with a support plate B84, one end of the trapezoidal screw shaft 86 is connected to the upper end of the support plate B84 by the bearing 85, the other end is connected to the D810, the bottom of the trapezoidal screw shaft C88 is sleeved on the trapezoidal screw shaft 86 by the screw shaft sleeve 87, the motor 89 is installed inside the support plate D810, the output shaft of the motor is connected with a gear A811, the gear A811 and a gear B814 are respectively arranged outside the support plate D810 and are connected with a first connecting key 812 and a second connecting key 815, the gear A811 and the gear B814 are in meshing transmission, the gear B814 is connected with the end part of the trapezoidal screw shaft 86 and is fixed by a fifth washer 813, and the bottom of the base 820 is connected with the traction chassis 9 and is fixed by a fifth bolt 816, a sixth nut 817 and a sixth washer 818.
Further, the traction chassis 9 includes a rear support leg 91, a latch 92, a seventh nut 93, a seventh bolt 94, an expansion link 95, a frame 96, a second bottom plate 97, a tire assembly 98, a shield 99, a front support leg assembly 910, a guard plate 911, a traction assembly 912, and an eighth bolt 913, the rear support leg 91 is disposed at the bottom of one end of the expansion link 95 and fixed to the seventh bolt 94 through the seventh nut 93, the other end of the expansion link 95 is connected to the frame 96, the second bottom plate 97 is disposed on the frame 96 and fixedly connected to the bottom of the base 820 in the support base 8, the tire assembly 98 is disposed at the middle of the bottom of the frame 96, the shield 99 is disposed at the outer side of the frame 96, the front support leg assembly 910 is disposed at the bottom of the front end of the frame 96 and fixed to the front support leg assembly 911 through the guard plate 911, the traction assembly 912 is connected to the front.
Furthermore, four guide rails 710 on the direction finder 7 are arranged, and are combined with the middle ring a71 and the middle ring B72 to form a launching track, the launching caliber of the launching track is 122 mm, the maximum high and low launching angles are not less than 80 degrees, and the combined launching track ensures the stability of the sounding rocket during launching.
Further, two middle rings A71 and two middle rings B72 are respectively arranged, the distance between the two middle rings A71 is 1000mm, and the distance between the two middle rings B72 is 3000 mm.
Further, the distance between the middle of the bottom of the support 716 and the through hole in the middle of the support 712 on the rear side is 1000mm, and the distance between the through hole in the middle of the support 712 on the rear side of the support 716 and the back plate 718 is 500 mm.
Furthermore, the height between the through hole at the upper end of the bearing plate A81 and the support plate body at the bottom of the machine base 820 is 740mm, the length of the support plate body at the bottom of the machine base 820 is 800mm, and the distance between the two slide rails 83 is 400 mm.
Further, the width of the second bottom plate 97 is 900mm, and the sum of the lengths of the second bottom plate 97 and the guard plate 911 is 2780 mm.
Furthermore, the height of the launcher is not more than 3m in a transport state, and the stability in transport is guaranteed.
The invention provides a meteorological sounding rocket launcher through improvement, and the working principle is as follows;
firstly, installing a launching frame at a proper position, and then adjusting the horizontal azimuth angle of the launching frame;
secondly, connecting a cable and switching on a power supply; the radio controller is used for adjusting the high and low shooting angles of the launcher, after the motor 89 works, the gear A811 and the gear B814 are meshed for transmission, the trapezoidal screw shaft 86 rotates, the bottom of the bearing plate C88 moves on the trapezoidal screw shaft 86 through the screw shaft sleeve 87, two ends of the bearing plate C88 slide on the slide rails 83 through the sliders, the bearing plate C8 drives the bottom of the connecting rod 1 to move, and meanwhile, the bearing 712 behind the bottom of the orientator 7 is positioned with the upper end of the bearing plate A81, so that the high and low shooting angles of the orientator 7 are adjusted;
thirdly, the arranged traction chassis 9 can be connected and installed on a truck longitudinal beam through a traction assembly 912 and fixed through bolts and steel plates, meanwhile, a second bottom plate 97 arranged at the bottom of the rack 96 can be used for assisting in moving and adjusting the position, and a telescopic rod 95 arranged at one side of the rack 96 is connected with a rear support leg 91 for assisting in supporting, can be stored when not used, and can be positioned and locked through a bolt 92;
fourthly, the set direction finder 7 adopts four guide rails 710 to be combined with the middle ring A71 and the middle ring B72 to form a launching track, the launching caliber is 122 mm, and detection and electric ignition launching can be implemented when the elevation angle rises to more than 55 degrees after the launching rack ignition system is switched on.
The meteorological sounding rocket launcher is provided through improvement, the overall structure is stable, and the meteorological sounding rocket launcher is suitable for operation under severe weather conditions; the launching angle adjusting mechanism adopts a connecting rod 1 mechanism which is transmitted by a screw rod driven by a motor 89; the direction finder 7 adopts four guide rails 710 to combine with the middle ring A71 and the middle ring B72 to form a launching track, the launching caliber is 122 mm, the maximum angle of the high and low incidence angles is not less than 80 degrees, the height of the launching cradle is not more than 3m in the transportation state, and the stability is high; the supporting part adopts a motor 89 to drive a trapezoidal screw shaft 86 to rotate, drives the connecting rod 1 to move back and forth so as to achieve the purpose of adjusting the launching angle, and can be quickly switched into a manual mode; the loading platform is lightly clamped by using a fifty-bell 600P double-row seat lengthened breast board, and the launcher main body is arranged on a truck longitudinal beam through bolts and steel plates, so that the stability is improved; the rocket operation automatic recording parameter instrument or the wireless launching controller can be used for controlling, a high-energy lithium battery is carried, and the problem of field power supply is solved.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described, and the standard parts used in the present invention are all available on the market, the special-shaped parts can be customized according to the description and the accompanying drawings, the specific connection mode of each part adopts the conventional means of bolt and rivet, welding and the like mature in the prior art, the machinery, parts and equipment adopt the conventional type in the prior art, and the circuit connection adopts the conventional connection mode in the prior art, and the details are not described herein.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. A meteorological sounding rocket launcher is characterized in that: the device comprises a connecting rod (1), a shaft pin A (2), a shaft pin B (3), a first gasket (4), a first nut (5), a second nut (6), an orientator (7), a supporting seat (8) and a traction chassis (9), wherein one end of the top of the connecting rod (1) is connected to the middle of the bottom of the orientator (7), one end of the bottom of the connecting rod is connected with one end of the supporting seat (8) through the shaft pin B (3), the connecting position of the bottom of the connecting rod is fixed through the first gasket (4), the first nut (5) and the second nut (6), the bottom end of the orientator (7) is connected with the other end of the supporting seat (8) through the shaft pin A (2), and the supporting seat (8) is installed on.
2. A weather sounding rocket launcher according to claim 1, characterized in that: the orientator (7) comprises a middle ring A (71), a middle ring B (72), a first bolt (73), a second washer (74), a third nut (75), a second bolt (76), a fourth nut (77), a third washer (78), a front baffle plate (79), a guide rail (710), a guide rail seat (711), a support (712), a third bolt (713), a fifth nut (714), a fourth washer (715), a support (716), a first bottom plate (717), a rear baffle plate (718), a rear baffle plate A (719), a binding post (720), a wiring board (721) and a fourth bolt (722), wherein the middle ring A (71) and the middle ring B (72) are symmetrically arranged at the upper end of the first bottom plate (717) in front and back, the front baffle plate (79) is connected with the rear baffle plate (718) through the guide rail (710) and the guide rail seat (711), the bottom of the guide rail seat (711) is provided with the first bottom plate (717), the front end of the first bottom plate (717) is connected with a front baffle (79) and fixed through a second bolt (76), a fourth nut (77) and a third washer (78), the rear end of the first bottom plate (717) is connected with a rear baffle (718) and fixed through a first bolt (73), a second washer (74) and a third nut (75), a support (716) is arranged at the bottom of the first bottom plate (717), a support (712) is arranged in the middle of the bottom of the support (716) and on the rear side of the bottom of the support, the support is fixed through a third bolt (713), a fifth nut (714) and a fourth washer (715) and connected with the connecting rod (1) and the support seat (8), a rear baffle A (719) is arranged on the rear baffle (718), and a binding post (720), a wiring board (721) and a fourth bolt (722) are arranged at the bottom of the rear baffle.
3. A weather sounding rocket launcher according to claim 1, characterized in that: the supporting seat (8) comprises a supporting plate A (81), a sliding seat (82), a sliding rail (83), a supporting plate B (84), a bearing (85), a trapezoidal screw shaft (86), a screw shaft sleeve (87), a supporting plate C (88), a motor (89), a supporting plate D (810), a gear A (811), a first connecting key (812), a fifth gasket (813), a gear B (814), a second connecting key (815), a fifth bolt (816), a sixth nut (817), a sixth gasket (818), a sixth bolt (819) and a machine base (820), the supporting plate A (81) is arranged on the rear side of the machine base (820) and fixed through the sixth bolt (819) and connected to a supporting piece (712) at the bottom rear part of the orientator (7), the sliding rail (83) is arranged on the machine base (820) and fixed with the front side of the supporting plate A (81) through the sliding seat (82), and the supporting plate B (84) is arranged in the middle part, one end of the trapezoidal screw shaft (86) is connected with the upper end of a support plate B (84) through a bearing (85), the other end of the trapezoidal screw shaft is connected with a support plate D (810), the bottom of the support plate C (88) is sleeved on the trapezoidal screw shaft (86) through a screw shaft sleeve (87), the upper end of the support plate D (810) is connected with a support (712) in the middle of the bottom of the orientator (7), the motor (89) is installed on the inner side of the support plate D (810), the output shaft of the motor is connected with a gear A (811), the gear A (811) and the gear B (814) are respectively arranged on the outer side of the support plate D (810) and are connected with a first connecting key (812) and a second connecting key (815), the gear A (811) and the gear B (814) are in meshing transmission, the gear B (814) is connected with the end of the trapezoidal screw shaft (86) and is fixed by a fifth washer (813), the bottom of, and is fixed by a fifth bolt (816), a sixth nut (817) and a sixth washer (818).
4. A weather sounding rocket launcher according to claim 1, characterized in that: the traction chassis (9) comprises rear support legs (91), a bolt (92), a seventh nut (93), a seventh bolt (94), a telescopic rod (95), a frame (96), a second bottom plate (97), a tire assembly (98), a shield (99), a front support leg assembly (910), a protective plate (911), a traction assembly (912) and an eighth bolt (913), wherein the rear support legs (91) are arranged at the bottom of one end of the telescopic rod (95) and fixed with the seventh bolt (94) through the seventh nut (93), the frame (96) is connected with the other end of the telescopic rod (95), the second bottom plate (97) is arranged on the frame (96) and fixedly connected with the bottom of a machine base (820) in the supporting seat (8), the tire assembly (98) is arranged in the middle of the bottom of the frame (96), the shield (99) is arranged on the outer side of the frame, the front support leg assembly (910) is arranged at the bottom of the front end of the frame (96) and is fixedly installed, the front end of the guard plate (911) is connected with a traction assembly (912), and the upper end of the rear supporting leg (91) is provided with an eighth bolt (913) and is fixed by a bolt (92).
5. A weather sounding rocket launcher according to claim 2, characterized in that: four guide rails (710) on the direction finder (7) are arranged and are combined into a launching track by matching with the middle ring A (71) and the middle ring B (72), the launching caliber of the launching track is 122 mm, and the maximum angle of the high and low radiation angles is not less than 80 degrees.
6. A weather sounding rocket launcher according to claim 2, characterized in that: the middle rings A (71) and the middle rings B (72) are respectively provided with two, the distance between the two middle rings A (71) is 1000mm, and the distance between the two middle rings B (72) is 3000 mm.
7. A weather sounding rocket launcher according to claim 2, characterized in that: the distance between the middle part of the bottom of the support (716) and the middle through hole of the support (712) on the rear side is 1000mm, and the distance between the middle through hole of the support (712) on the rear side of the support (716) and the rear baffle (718) is 500 mm.
8. A weather sounding rocket launcher according to claim 3, characterized in that: the height between the through hole at the upper end of the bearing plate A (81) and the support plate body at the bottom of the machine base (820) is 740mm, the length of the support plate body at the bottom of the machine base (820) is 800mm, and the distance between the two slide rails (83) is 400 mm.
9. A weather sounding rocket launcher according to claim 4, characterized in that: the width of the second bottom plate (97) is 900mm, and the sum of the lengths of the second bottom plate (97) and the guard plate (911) is 2780 mm.
10. A weather sounding rocket launcher according to claim 1, characterized in that: when the launcher is in a transportation state, the height is not more than 3 m.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010328938.1A CN111397440A (en) | 2020-04-23 | 2020-04-23 | Meteorological sounding rocket launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010328938.1A CN111397440A (en) | 2020-04-23 | 2020-04-23 | Meteorological sounding rocket launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111397440A true CN111397440A (en) | 2020-07-10 |
Family
ID=71437509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010328938.1A Pending CN111397440A (en) | 2020-04-23 | 2020-04-23 | Meteorological sounding rocket launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111397440A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113203318A (en) * | 2021-04-25 | 2021-08-03 | 北京机械设备研究所 | Portable three-leg launcher for forest fire-extinguishing cannon |
| CN113624070A (en) * | 2021-07-08 | 2021-11-09 | 陕西中天火箭技术股份有限公司 | Portable ground guidance rocket launcher with adjustable launch angle |
| CN114216366A (en) * | 2021-12-24 | 2022-03-22 | 鲁东大学 | Rocket launcher for ships |
| CN115615246A (en) * | 2022-10-15 | 2023-01-17 | 新余国科特种装备有限公司 | Launching device and launching method of rain-enhancement hail-suppression rocket projectile |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201016649Y (en) * | 2006-10-23 | 2008-02-06 | 新疆维吾尔自治区人工影响天气办公室 | Multifunctional artificial hail-proof rain-increasing rocket pod and emission controller thereof |
| CN202101605U (en) * | 2011-06-03 | 2012-01-04 | 江西钢丝厂 | Vehicle-mounted electric launching rack capable of moving horizontally and automatically |
| CN103528439A (en) * | 2013-10-12 | 2014-01-22 | 江西新余国科科技有限公司 | Precipitation Rain enhancement hail prevention rocket launcher |
| CN105584937A (en) * | 2016-03-03 | 2016-05-18 | 上汽大众汽车有限公司 | Tool turret hoisting tool |
| CN106197146A (en) * | 2016-08-12 | 2016-12-07 | 清华大学 | A kind of rocket model and the adjustable rocket launch platform of attitude |
| CN108398052A (en) * | 2018-05-18 | 2018-08-14 | 新余国科特种装备有限公司 | Afocal variable rocket launching finder |
| CN212179699U (en) * | 2020-04-23 | 2020-12-18 | 新余国科特种装备有限公司 | Meteorological sounding rocket launcher |
-
2020
- 2020-04-23 CN CN202010328938.1A patent/CN111397440A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201016649Y (en) * | 2006-10-23 | 2008-02-06 | 新疆维吾尔自治区人工影响天气办公室 | Multifunctional artificial hail-proof rain-increasing rocket pod and emission controller thereof |
| CN202101605U (en) * | 2011-06-03 | 2012-01-04 | 江西钢丝厂 | Vehicle-mounted electric launching rack capable of moving horizontally and automatically |
| CN103528439A (en) * | 2013-10-12 | 2014-01-22 | 江西新余国科科技有限公司 | Precipitation Rain enhancement hail prevention rocket launcher |
| CN105584937A (en) * | 2016-03-03 | 2016-05-18 | 上汽大众汽车有限公司 | Tool turret hoisting tool |
| CN106197146A (en) * | 2016-08-12 | 2016-12-07 | 清华大学 | A kind of rocket model and the adjustable rocket launch platform of attitude |
| CN108398052A (en) * | 2018-05-18 | 2018-08-14 | 新余国科特种装备有限公司 | Afocal variable rocket launching finder |
| CN212179699U (en) * | 2020-04-23 | 2020-12-18 | 新余国科特种装备有限公司 | Meteorological sounding rocket launcher |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113203318A (en) * | 2021-04-25 | 2021-08-03 | 北京机械设备研究所 | Portable three-leg launcher for forest fire-extinguishing cannon |
| CN113203318B (en) * | 2021-04-25 | 2022-08-12 | 北京机械设备研究所 | Portable three-leg launcher for forest fire-extinguishing cannon |
| CN113624070A (en) * | 2021-07-08 | 2021-11-09 | 陕西中天火箭技术股份有限公司 | Portable ground guidance rocket launcher with adjustable launch angle |
| CN114216366A (en) * | 2021-12-24 | 2022-03-22 | 鲁东大学 | Rocket launcher for ships |
| CN114216366B (en) * | 2021-12-24 | 2023-08-15 | 鲁东大学 | Rocket launching frame for ship |
| CN115615246A (en) * | 2022-10-15 | 2023-01-17 | 新余国科特种装备有限公司 | Launching device and launching method of rain-enhancement hail-suppression rocket projectile |
| CN115615246B (en) * | 2022-10-15 | 2024-06-11 | 新余国科特种装备有限公司 | Device and method for launching hail-proof rocket shell |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111397440A (en) | Meteorological sounding rocket launcher | |
| CN109720608B (en) | Vehicle-mounted movable hydraulic buffer landing platform for rocket recovery | |
| CN212179699U (en) | Meteorological sounding rocket launcher | |
| CN219037784U (en) | Aiming window protection plate and vehicle-mounted laser destruction device | |
| CN107176310B (en) | Unmanned aerial vehicle launching cradle | |
| CN202101605U (en) | Vehicle-mounted electric launching rack capable of moving horizontally and automatically | |
| CN108971832A (en) | A kind of automatic welding machinery hand | |
| US4014310A (en) | Transportable target throwing apparatus | |
| GB2342428B (en) | Self propelled gun | |
| CN207585327U (en) | A kind of strong electromagnetic pushes the device that body of moving removes rotary kiln outlet slagging | |
| CN202101606U (en) | Vehicular power-driven launcher with bomb storage | |
| CN111055984A (en) | Rocket launcher for ships | |
| CN211809594U (en) | Route inspection vehicle | |
| CN215725447U (en) | Large projectile body closing and retreating device | |
| JP2003336998A (en) | Vehicle mounted gun launching mechanism | |
| CN116442188A (en) | Explosion robot based on remote sensing technology | |
| CN212323675U (en) | Portable winter high-voltage power grid deicing device | |
| CN209891111U (en) | Automatic picking and placing equipment for traffic cones | |
| CN113819803A (en) | Large projectile body closing and retreating device | |
| CN219900707U (en) | Auxiliary feeding and discharging device of laser cutting machine | |
| CN221473960U (en) | Adjustable computer motherboard welding set | |
| CN221394097U (en) | Unmanned aerial vehicle takes photo by plane with camera is accomodate | |
| CN115446512B (en) | Material conveying trolley for tank welding | |
| CN206345020U (en) | Vehicle-mounted chassis lifting and moving device | |
| CN221138611U (en) | High-efficiency multifunctional self-propelled bullet hanging vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |