CN110631419A - Portable detachable folding missile-rocket launching device - Google Patents
Portable detachable folding missile-rocket launching device Download PDFInfo
- Publication number
- CN110631419A CN110631419A CN201910777813.4A CN201910777813A CN110631419A CN 110631419 A CN110631419 A CN 110631419A CN 201910777813 A CN201910777813 A CN 201910777813A CN 110631419 A CN110631419 A CN 110631419A
- Authority
- CN
- China
- Prior art keywords
- shaped
- guide rail
- bolt
- missile
- plate
- 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.)
- Granted
Links
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
- F41F3/045—Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
-
- 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
- F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
The invention provides a portable detachable folding missile-rocket launching device, which comprises a missile/rocket, a missile body, a front direction finder, a rear direction finder and a tail wing, wherein the missile/rocket is provided with a missile body; the device comprises a sliding guide rail, a rectangular support aluminum plate, a B-shaped plate aluminum plate, a bolt, a clamping head, a T-shaped piece, a U-shaped connecting piece, a U-shaped arch door piece, a guide rail/support rod connector and a single-side trunnion bolt hole; the support leg comprises a support leg, a support leg hollow square rod and a support leg connecting piece; a leg fixing member; an L-shaped guide rail connecting rod; an angle adjusting support bar; the guide rail supports the slide rail; the device comprises a base, a base mounting plate and a single-side trunnion connecting piece; the invention can be disassembled into small parts, is convenient to carry and transport, is not limited by road and railway conditions, and greatly improves the flexibility and the maneuvering transfer speed; the launching device has a simple integral structure and lower requirements on operators, so that the individual combat capability of individual soldiers can be greatly improved.
Description
Technical Field
The invention belongs to the field of mechanical design, and mainly relates to a portable detachable folding missile-rocket launching device. The launching device can achieve the purpose of adjusting different launching angles by adjusting the angle between the supporting guide rail and the horizontal ground. The missile/rocket launching device can be disassembled and folded after use, the length of all the supports after disassembly does not exceed 1.2m, the missile/rocket launching device is simple in structure, convenient to install on site, carry by single soldier or multiple soldiers in mountainous areas, transport and maintain by automobiles or trains, greatly reduces the requirements on carrying, transporting and other conditions, and can be carried by personnel to reach the destination without being limited by the transporting conditions such as roads even in the jungle zones in mountainous areas. The portable detachable and foldable design greatly improves the maneuverability, the flexibility and the individual combat capability of the launching device, which has very important significance for combat and training.
Background
With the development of science and technology and the increasing speed of weapon renewal, the form of the battlefield is changing constantly. In order to improve the survivability of weapons and personnel, higher and higher requirements are put on the rapid response index of the weapon system. Therefore, the weapon launching is gradually transferred to roadbed (highway, railway, etc.), sea foundation and empty foundation from the original well foundation launching, which greatly improves the maneuverability and flexibility of weapon transferring and fighting, and further improves the battlefield viability. Weapons such as rockets and missiles have a great killing power, and in order to improve their combat efficiency, weapons such as light-weight portable missiles and rockets are favored. The launching conditions of the weapons such as the missile/rocket are directly related to the combat capability and the combat range of the soldiers. The invention aims to design a portable detachable folding missile-rocket launching device, which can be rapidly detached and folded after use, and is convenient to store, transport and carry. Because the sizes of the components of the launcher after disassembly and folding are all less than 1.2m, the launcher can be directly carried and transported by personnel in rugged mountain roads, steep slopes, even mountain areas and other zones which are inconvenient for vehicle transportation, the constraint on transportation conditions such as roads, railways and the like is eliminated, the transfer and transportation efficiency is greatly improved, the fighting fire points of weapons such as missiles/rockets and the like are rapidly dispersed to all regions, and the fighting capacity is improved.
The missile/rocket launching is mainly classified according to launching sites into roadbed launching, sea-based launching and air-based launching, wherein the roadbed launching comprises fixed launching and ground launching. The ground launching mainly comprises four modes of self-propelled type, traction type, railway type and portable type. The design of the patent belongs to a portable demountable missile/rocket launching device. The portable demountable missile/rocket launch version has gained wider use due to its greater maneuverability and flexibility. In addition, considering that the launching device needs to have good maneuverability and reliability, whether the structural design of the launching device is reasonable directly determines the power of the missile/rocket launching device and the convenience of carrying and transportation. The launching device is simple and reasonable in structure, convenient to detach and fold and carry after use, and can meet the launching requirements of missiles/rockets of various models through the standardized design of the orientator, so that the purpose of launching a plurality of missiles is achieved, and the using frequency and the weapon fighting capacity of the launching device are greatly improved due to good convenience and maneuverability.
Disclosure of Invention
Objects of the invention
The invention provides a portable detachable folding missile-rocket launching device, which aims to solve the problems of improving the portability, maneuverability and use frequency of the launching device. Can meet the requirements of missile/rocket launching of various types, can be disassembled and assembled conveniently, and is suitable for the operational use requirements of different launching angles and different launching directions. The number of the disassembled parts is small, the size of the disassembled parts is smaller than 1.2m, the requirement of convenience of direct carrying by personnel is met, the operational capacity of individual soldiers is greatly improved, the designed missile/rocket generating device has the advantages of simple structure, easiness in maintenance and low cost, and the requirement and the maintenance cost on operation and use personnel are reduced.
(II) technical scheme
The invention relates to a portable detachable folding missile-rocket launching device, which is characterized in that: the missile/rocket launcher comprises a missile/rocket (1), a missile body (10), a front direction finder (11), a rear direction finder (12), a tail wing (13), a sliding guide rail (2), a cuboid supporting aluminum plate (20), a Z-shaped plate aluminum plate (21), bolts (22), clamping heads (23), T-shaped pieces (24), U-shaped connecting pieces (25), U-shaped arch door pieces (26), guide rail/supporting rod connectors (27), single-side trunnion bolt holes (28), supporting legs (3), supporting leg hollow square rods (31), supporting leg connecting pieces (32), supporting leg fixing pieces (4), L-shaped guide rail connecting rods (5), angle adjusting supporting rods (6), guide rail supporting slide rails (7), a base (8), a base mounting plate (81) and single-side trunnion connecting pieces (82);
the mutual position relationship of the above components is: the missile/rocket is characterized in that an I-shaped front direction finder (11) and a rear direction finder (12) are respectively connected with the surface gravity center of a missile body (10) of the missile/rocket (1) and the surface of the front end of a tail wing (13) on the same axis; before launching, a front director (11) and a rear director (12) of the missile/rocket (1) are pushed into the sliding guide rail (2) along matching grooves in a sliding mode, and the missile/rocket (1) can freely slide along the guide rail sliding grooves through the front director (11) and the rear director (12); the main structure of the guide rail (2) is provided with two cuboid supporting aluminum plates (20) and a Z-shaped aluminum plate (21); each Z-shaped aluminum plate (21) is fastened with a corresponding rectangular support aluminum plate (20) through bolts, and the two parts are spliced side by side to form the basic shape of the guide rail (2); 2 rows of U-shaped arch door pieces (26) are respectively connected in parallel in the splicing position area of the U-shaped arch door pieces and the L-shaped guide rail connecting rods (5) are inserted along the notches of the U-shaped arch door pieces (26) to ensure that the U-shaped arch door pieces and the L-shaped guide rail connecting rods are accurately butted and form a seamless butted track; a T-shaped part (24) is connected to the central region of the back of the rectangular support aluminum plate (20) close to the front end, and the T-shaped part (24) is connected with the U-shaped connecting piece (25) through a bolt, so that the U-shaped connecting piece (25) can rotate but cannot move; a guide rail/support rod connector (27) is fixedly connected with the middle area of two rectangular support aluminum plates (20) close to the rear end, a clamping head (23) is arranged above the front surface of the tail part of the guide rail/support rod connector to prevent the guided missile/rocket (1) from withdrawing from the guide rail (2) when in static placement, and a pair of unilateral trunnion bolt holes (28) is arranged in the tail area of the back surface of the guide rail/rocket; the U-shaped connecting piece (25) in the central area of the front part of the guide rail (2) is connected with the supporting leg (3) to prevent the launcher from overturning during launching; the support legs (3) connect two support leg hollow square rods (31) through support leg connecting pieces (32), one ends of the support legs are connected with the U-shaped connecting pieces (25), and the other ends of the support legs are connected with support leg fixing pieces (4) for fixing the support legs (3) on the ground; a guide rail/support rod connector (27) on the back of the rear end of the guide rail (2) is connected with the angle adjusting support rod (6) and is used for supporting the guide rail (2) and adjusting the emission angle of the guide rail (2); the middle part of the guide rail supporting slide rail (7) is a hollow rectangular groove, one end of the angle adjusting support rod (6) is fastened and fixed with the guide rail supporting slide rail (7) through a bolt, and when the bolt is loosened, the angle adjusting support rod (6) can freely slide along a channel of the guide rail supporting slide rail (7) to adjust the hair-catching angle; the guide rail supporting slide rail (7) is fixedly connected to the base (8) through bolts, a plurality of bolt holes are uniformly distributed in parallel on the base mounting plate (81), and the unilateral trunnion connecting piece (82) is fixedly connected to the base mounting plate (81) through bolts;
the missile/rocket (1) consists of a missile body (10), a front director (11), a rear director (12) and a tail wing (13); their positional relationship to each other is: the front direction finder (11) and the rear direction finder (12) are connected or fastened on the same axis of the surface of the bullet body (10) by bolts, the front direction finder (11) is usually positioned near the gravity center, and the rear direction finder (12) is positioned in front of the tail wing (13) and close to the tail wing (13);
the bullet body (10) is generally a cylindrical shell, the front end of the bullet body is a conical structure, and the bullet body has small resistance in flight; the wall thickness and the connecting structure of the shell structure are related to the requirements and the specific design of the arrow body structure;
the front direction finder (11) and the rear direction finder (12) are I-shaped, and the front direction finder and the rear direction finder have the same structure and are respectively arranged at the middle part and the rear part of the same axis on the surface of the missile/rocket (1); the front and back direction finders (11, 12) are connected or hinged on the bullet body (10) by bolts, and the lower surfaces of the I-shaped front and back direction finders (11, 12) cling to the lower surfaces of the guide rail grooves to slide when the bullet is launched;
the structure of the tail wing (13) is a four-piece axisymmetric trapezoid structure, and the tail wing (13) is fixed at the tail part of the bullet body (10) in a clamping groove fixing mode;
the sliding guide rail (2) is composed of a rectangular support aluminum plate (20), a B-shaped plate aluminum plate (21), a bolt (22), a clamping head (23), a T-shaped piece (24), a U-shaped connecting piece (25), a U-shaped arch door piece (26), a guide rail/support rod connector (27) and a single-side trunnion bolt hole (28); their positional relationship to each other is: the main body structure of the sliding guide rail (2) is formed by splicing two cuboid supporting aluminum plates (20) with the same shape, 2Z-shaped aluminum plates (21) are symmetrically arranged on the two cuboid supporting aluminum plates (20) respectively, and bolt holes which are uniformly distributed are arranged at corresponding positions on the cuboid supporting aluminum plates (20) and the Z-shaped aluminum plates (21) and are fastened by bolts (22); the tail part of the sliding guide rail is provided with a clamping head (23) which is fastened on the sliding guide rail (2) through a bolt (22); seen from the back of the sliding guide rail (2), two rows of U-shaped arch door pieces (26) are connected to two sides of the splicing area, and are inserted side by side through two L-shaped guide rail connecting rods (5) to ensure the accurate butt joint of the two; the central area of the front semi-conductor rail of the sliding guide rail (2) is connected with a T-shaped part (24), the T-shaped part (24) is connected with 2U-shaped connecting pieces (25) through bolts, the moving freedom degree of the U-shaped connecting pieces (25) is eliminated, and the rotating freedom degree of the U-shaped connecting pieces (25) is reserved; the central area of the rear half guide rail is connected with a guide rail/supporting rod connector (27), and the end part of the sliding guide rail (2) is provided with a pair of unilateral trunnion bolt holes (28);
the cuboid supporting aluminum plate (20) is a rectangular aluminum plate, sinking bolt holes (the diameter is 10mm) are uniformly arranged on the rectangular aluminum plate, and an inner bolt is arranged on the rectangular aluminum plate;
the Z-shaped aluminum plate (21) is structurally characterized in that a flat plate is bent twice to form a Z shape, bolt through holes identical to those of the cuboid support aluminum plate (20) are formed in the Z-shaped aluminum plate (21), and the bolt through holes and the cuboid support aluminum plate can be hinged together through bolts (the diameter of the bolts is 10 mm);
the bolt (22) is a standard part (with a diameter of 10 mm);
the clamping head (23) is structurally a small rectangular iron sheet, two bolt holes (the diameter is 10mm) are respectively formed in two ends of the clamping head, and the middle of the clamping head is bent for four times, so that a small arch area is formed in the middle area and can be fastened with a Z-shaped plate aluminum plate (21) structure;
the T-shaped part (24) is formed by vertically connecting two small rectangular plates, and one surface of the T-shaped part is fastened on the back surface of a rectangular support aluminum plate (20) through connection or bolts; a round through hole (the diameter is 10mm) is arranged in the center of the rectangular plate vertical to the round through hole;
the U-shaped connecting piece (25) is formed by bending a small rectangular aluminum sheet, the shape of the U-shaped connecting piece is similar to a U shape, and the central areas of the bottom surface and the two side surfaces of the U-shaped connecting piece are respectively provided with a circular bolt through hole (the diameter is 10 mm);
the U-shaped arched door piece (26) is a U-shaped part with a notch formed by bending an aluminum strip twice, and two legs of the U-shaped arched door piece (26) are connected to a rectangular support aluminum plate (20); two connecting rows are distributed side by side;
the guide rail/support rod connector (27) is characterized in that a rectangular aluminum plate is used as a base, two lug plates are connected on the base side by side, and a bolt hole is oppositely arranged in the middle of each lug plate and is used for being hinged with the angle adjusting support rod (6);
the unilateral trunnion bolt hole (28) is a lower counter bore (the diameter is 10mm), is internally provided with threads, is positioned at the end part of the sliding guide rail (2), and is used for connecting a unilateral trunnion connecting piece (82);
the supporting legs (3) comprise supporting leg hollow square bars (31) and supporting leg connecting pieces (32); their mutual positional relationship is: 2 support leg hollow square rods (31) are fastened and connected through support leg connecting pieces (32) by bolts; one end of the supporting leg (3) is hinged with the U-shaped connecting piece (25) through a bolt, and the other end of the supporting leg is hinged with the supporting leg fixing piece (4) through a bolt;
the hollow square rod (31) of the supporting leg is a hollow cuboid square column (the length is 1.2m), and the cross section of the square column is in a shape like a Chinese character hui; two ends of the supporting leg hollow square rod (31) are provided with bolt through holes (the diameter is 10mm) in one direction;
the landing leg connecting piece (32) is also a hollow cuboid column, and the section is also in a shape of Chinese character hui; the size of the hollow section in the landing leg connecting piece (32) is equal to that of the section outside the landing leg hollow square rod (31); two parallel surfaces in one direction of the supporting leg connecting piece (32) are provided with 2 bolt holes (the diameter is 10mm) side by side;
the main structure of the supporting leg fixing part (4) is that 2 small flat plates with holes at the centers are vertically connected side by side on a square plate; the bottom surface square plate is provided with a square plate with four bolt holes, and the bolt holes are symmetrically and uniformly distributed; the central area on the bottom square plate is connected with two square plates with holes at a certain distance; when in use, the bottom square plate is fastened on the ground by using expansion bolts to penetrate through the bolt holes, and the square plate with the holes and the supporting legs (3) can be hinged by using common bolts;
the L-shaped guide rail connecting rod (5) is used for accurately connecting two cuboid supporting aluminum plates (20) which are arranged end to end in a connected mode; the L-shaped guide rail connecting rod (5) is formed by bending an iron bar with a rectangular cross section once, and the shape of the L-shaped guide rail connecting rod is similar to an L shape;
the angle adjusting support rod (6) is structurally a rectangular thick plate with a certain thickness, two ends of the thick plate are in arc transition, and a hollow cylinder taking the center of an arc as a circular point is arranged at each of the two ends; the hollow cylinder is hinged with the guide rail/support rod connector (27) through a shaft or a bolt, and the other end of the hollow cylinder is connected with the guide rail support sliding rail (7) through a bolt, so that the angle adjusting support rod (6) can move along the guide rail support sliding rail (7) to adjust the emission angle;
the periphery of the guide rail supporting slide rail (7) is a columnar cuboid, a hollowed small cuboid is arranged in the center of the cuboid and used for fixing a bolt rod, and bolt holes (the diameter is 10mm) are formed in two ends of the guide rail supporting slide rail (7); one end of the base can be used for being connected and fastened with the base (8); the guide rail supports the strip cuboid with the hollow center of the slide rail (7), so that the bolt rod has certain movement automation degree to achieve the purpose of adjusting the emission angle;
the base (8) consists of a base mounting plate (81) and a unilateral trunnion connecting piece (82); the unilateral trunnion connecting piece (82) is hinged and fastened on the base mounting plate (81) through a bolt; three unilateral trunnion connecting pieces (82) are hinged together through bolts, and the other two unilateral trunnion connecting pieces are fastened on unilateral trunnion bolt holes (28) through bolts;
the main body of the base mounting plate (81) is an aluminum plate (the thickness of the aluminum plate is 30 mm); the middle area of the aluminum plate is provided with a large hollow flame hole, the edge of the aluminum plate is also provided with a hole with the same size, and the aluminum plate is in a half-moon shape because the aluminum plate is positioned at the edge of the cuboid; a plurality of bolt holes are uniformly distributed on the base mounting plate, and protruded rectangular strips with holes are distributed on the peripheral side surface and appear in pairs;
the shape of the unilateral trunnion fixing seat (82) is similar to that of a whistle, a shaft hole is formed in the side surface area of the head of the whistle, and an installation bolt hole is formed in the mouth area of the whistle and used for installing the unilateral trunnion fixing seat (82) on the unilateral trunnion bolt hole (28) or a base installation plate (81);
the portable detachable folding missile/rocket launching device can be detached into small parts, is convenient to carry and transport, is not limited by road and railway conditions, and greatly improves the flexibility and the maneuvering transfer speed. The launching device has a simple integral structure and lower requirements on operators, so that the individual combat capability of individual soldiers can be greatly improved.
(III) the invention has the advantages that:
1. the invention discloses a portable detachable folding missile-rocket launching device, and belongs to the field of machining. The missile/rocket is provided with the same front and rear direction finders (11 and 12), so that the requirement that one launcher launches rockets and missiles of different models can be met, the use frequency of the launcher is improved, and the launching requirements of different angles and directions are met;
2. the portable detachable folding missile/rocket launching device is simple in structure and can be detached into small parts during transportation and storage. All the parts after disassembly are not larger than 1.2m in size, and are convenient to store, transport, carry and subsequently assemble. The small parts are convenient for individual soldiers to carry for operation, the transportation requirement is reduced, and the individual soldier operation capacity and range are greatly improved;
3. most parts of the portable detachable folding missile/rocket launching device are made of aluminum alloy, and the overall structure quality is reduced. The base mounting plate (81) is provided with a plurality of bolt holes and missile/rocket tail flame holes, so that the quality of the launcher is reduced, a larger degree of freedom is reserved for the installation and use of the launcher, and the requirements of different launching angles can be met;
4. the portable detachable folding missile/rocket launching device has the advantages of simple structure, low operation and use requirements, convenience in operation, low manufacturing cost, easiness in maintenance and environmental friendliness.
Drawings
FIG. 1 is an isometric view of a portable collapsible missile/rocket launcher of the present invention.
Figure 2 is an isometric illustration of a portable collapsible missile/rocket structure of the present invention.
FIG. 3 is a schematic axial side elevation view of a portable collapsible missile/rocket launcher sliding rail structure of the present invention.
FIG. 4 is a schematic axial side view of the back of the portable collapsible missile/rocket launcher sliding rail structure of the present invention.
FIG. 5 is a schematic view of the connection structure of the support legs of the portable collapsible missile/rocket launcher of the present invention.
FIG. 6 is a schematic view showing the structure of the base connection part of a portable collapsible missile/rocket launching device according to the invention.
FIG. 7 is a cross-sectional view of a portable collapsible missile/rocket launcher sliding guide of the present invention.
Figure 8 is an isometric view of a portable collapsible missile/rocket launcher cartridge of the present invention.
Figure 9 is an isometric view of a tee of a portable collapsible missile/rocket launcher of the present invention.
Figure 10 is an isometric view of a portable collapsible missile/rocket launcher U-shaped attachment of the present invention.
Figure 11 is an isometric view of a portable collapsible missile/rocket launcher rail/strut connector of the present invention.
Figure 12 is an isometric view of a portable collapsible missile/rocket launcher rail L-shaped rail attachment link of the present invention.
Figure 13 is an isometric view of a portable collapsible missile/rocket launcher angle adjustment support bar of the present invention.
Figure 14 is an isometric view of a portable collapsible missile/rocket launcher rail support skid of the present invention.
Figure 15 is an isometric view of a base portion of a portable collapsible missile/rocket launcher of the present invention.
In the figure:
1-missile/rocket, 10-missile body, 11-front direction finder, 12-rear direction finder and 13-empennage;
2-sliding guide rail, 20-cuboid supporting aluminum plate, 21-B-shaped aluminum plate, 22-bolt, 23-chuck, 24-T-shaped piece, 25-U-shaped connecting piece, 26-U-shaped arch door piece, 27-guide rail/supporting rod connector and 28-single-side trunnion bolt hole;
3-support leg, 31-support leg hollow square rod and 32-support leg connecting piece;
4-a leg mount;
5-L-shaped guide rail connecting rods;
6-angle adjusting support rods;
7-the guide rail supports the slide rail;
8-base, 81-base mounting plate, 82-unilateral trunnion connecting piece;
detailed description of the preferred embodiments
The present invention will be described in further detail with reference to the accompanying drawings.
The invention relates to a portable detachable folding missile/rocket launching device, which is shown in figure 1; the method is characterized in that: the missile/rocket launcher comprises a missile/rocket 1, a missile body 10, a front direction finder 11, a rear direction finder 12, a tail wing 13, a sliding guide rail 2, a cuboid supporting aluminum plate 20, a Z-shaped plate aluminum plate 21, a bolt 22, a clamping head 23, a T-shaped piece 24, a U-shaped connecting piece 25, a U-shaped arch door piece 26, a guide rail/support rod connector 27, a single-side trunnion bolt hole 28, a support leg 3, a support leg hollow square rod 31, a support leg connecting piece 32, a support leg fixing piece 4, an L-shaped guide rail connecting rod 5, an angle adjusting support rod 6, a guide rail supporting slide rail 7, a base 8, a base mounting plate 81 and a;
the mutual position relationship of the above components is: the surface of a missile body 10 at the gravity center of a missile/rocket 1 and the surface of the front end of a tail wing 13 are respectively connected with an I-shaped front direction finder 11 and a rear direction finder 12 on the same axis; before launching, a front director 11 and a rear director 12 of the missile/rocket 1 slide along a matching groove on a slide guide rail 2 and are pushed into a clamping head 23 on the guide rail 2, and the missile/rocket 1 can slide freely along a guide rail sliding groove through the front director (11) and the rear director (12); the guide rail 2 is mainly structurally provided with two cuboid support aluminum plates 20 and a Z-shaped plate aluminum plate 21; each B-shaped plate aluminum plate 21 is fastened with a corresponding rectangular support aluminum plate 20 through bolts, and the two parts are spliced side by side to form the basic shape of the guide rail 2; 2 rows of U-shaped arch pieces 26 are welded on the back area of the splicing position of the cuboid support aluminum plate 20 side by side respectively, 2L-shaped guide rail connecting rods 5 are inserted along the notches of the U-shaped arch pieces 26, accurate butt joint of the U-shaped arch pieces and the U-shaped arch pieces is guaranteed, and a seamless butt joint track is formed, so that the guide rails 2 are long enough when being launched, and each part is small in size and convenient to carry when being transported and stored; a T-shaped part 24 is connected to the central area of the back of the rectangular support aluminum plate 20 close to the front end, the T-shaped part 24 is connected with the U-shaped connecting piece 25 through bolts, the rotational freedom degree of the U-shaped connecting piece 25 is reserved, and the moving freedom degree is eliminated; a guide rail/support rod connector 27 is welded and fixed in the middle area close to the rear end cuboid support aluminum plate 20, and a pair of unilateral trunnion bolt holes 28 is arranged in the rear area of the back surface of the guide rail/support rod connector; the U-shaped connecting piece 25 in the central area of the front part of the guide rail 2 is connected with the supporting legs 3, so that the launcher is prevented from overturning due to the action of factors such as vibration or external wind and the like in the launching process; the two hollow square rods 31 of the support legs are connected by bolts through support leg connecting pieces 32 by the support legs 3, one ends of the support legs are connected with the U-shaped connecting pieces 25, the other ends of the support legs are connected with support leg fixing pieces 4, and the support leg fixing pieces 4 can be fastened on the ground through expansion bolts; a guide rail/support rod connector 27 on the back of the rear end of the guide rail 2 is connected with the angle adjusting support rod 6 and is used for supporting and adjusting the emission angle of the guide rail 2; the middle part of the guide rail supporting slide rail 7 is a hollow rectangular groove, and one end of the angle adjusting support rod 6 is fixedly fastened with the guide rail supporting slide rail 7 through a bolt; when the bolt is loosened, the angle adjusting support rod 6 can freely slide along the channel of the guide rail support slide rail 7 to adjust the hair angle; the guide rail supporting slide rail 7 is fixedly connected to the base 8 through bolts, a plurality of bolt holes are uniformly distributed in parallel on the base mounting plate 81, and the unilateral trunnion connecting piece 82 is fixedly connected to the upper base mounting plate 81 through bolts;
the missile/rocket 1 consists of a missile body 10, a front director 11, a rear director 12 and a tail wing 13; their positional relationship to each other is: a front direction finder 11 and a rear direction finder 12 are welded or bolted on the same axis on the surface of the bullet body 10, the front direction finder 11 is usually located near the center of gravity, and the rear direction finder 12 is located in front of the tail 13 and close to the tail 13; the design is beneficial to reducing the sinking amount of the head of the missile/rocket 1 in the sliding process so as to reduce the launching error and improve the precision of the missile/rocket;
the body 10 is generally cylindrical in configuration and the nose is conical in configuration to reduce drag of the air stream on the body 10 during flight. The diameter of the cylinder is 200mm, the thickness is 2mm, the cylinder is made of hard aluminum alloy, and the structure of the cylinder is shown in figure 2;
the front direction finder 11 and the rear direction finder 12 are I-shaped, made of stainless steel, and have the same structure and are respectively arranged at the middle part and the rear part of the same axis on the surface of the missile/rocket 1 and respectively close to the gravity center and the tail wing 13; the width of the upper surface of the I-shaped part is 15mm, and the thickness of the I-shaped part is 3 mm. The front and back direction finders (11, 12) are welded or hinged on the bullet body 10 by bolts, and the lower surfaces of the I-shaped front and back direction finders (11, 12) slide tightly against the lower surfaces of the guide rail grooves when the bullet is launched. The I-shaped design structure has small volume and weight, and the influence on the flow field of the missile body 10 can be ignored. The specific structures are shown as the marks 11 and 12 in fig. 2;
the structure of the tail wing 13 is a four-piece axisymmetric trapezoid structure, and the tail wing 13 is fixed at the tail part of the bullet body 10 in a clamping groove fixing mode. The upper side and the height of the trapezoid are both 120mm, and the inclined edge of the trapezoid of the tail wing 13 forms an angle of 120 degrees with the incoming flow direction. The tail wing 13 has less resistance during flight and can provide the required control moment;
the sliding guide rail 2 consists of a rectangular support aluminum plate 20, a Z-shaped aluminum plate 21, a bolt 22, a clamping head 23, a T-shaped piece 24, a U-shaped connecting piece 25, a U-shaped arch door piece 26, a guide rail/support rod connector 27 and a single-side trunnion bolt hole 28; their positional relationship to each other is: the main structure of the sliding guide rail 2 is formed by splicing two cuboid supporting aluminum plates 20 with the same shape, 2Z-shaped aluminum plates 21 are symmetrically arranged on the two cuboid supporting aluminum plates 20 respectively, bolt holes are uniformly distributed in corresponding positions on the cuboid supporting aluminum plates 20 and the Z-shaped aluminum plates 21 and are fastened by bolts 22, and a groove is formed in the middle of the symmetrically distributed Z-shaped aluminum plates 21 and can provide restraint and guidance for the sliding of the orientator; the tail part of the sliding guide rail is provided with a clamping head 23 which is fastened on the sliding guide rail 2 through a bolt 22, and the missile/rocket 1 which is placed on the launcher at a certain inclination angle can not be drawn out from the rear part of the sliding guide rail 2 when the missile/rocket is to be launched. Seen from the back of the sliding guide rail 2, two rows of U-shaped arch door pieces 26 are welded on two sides of the splicing area and are inserted side by side through two L-shaped guide rail connecting rods 5, so that the two are ensured to be accurately butted. The two rows of U-shaped arch door pieces 26 are beneficial to reducing the quality of the connecting rods and simultaneously improving the bending moment resistance coefficient of the connecting rods, and the rigidity and the connection accuracy of the L-shaped guide rail connecting rods 5 are improved. A T-shaped part 24 is welded in the central area of the front semi-conductor rail of the sliding guide rail 2, the T-shaped part 24 is connected with 2U-shaped connecting pieces 25 through bolts, the moving freedom degree of the U-shaped connecting pieces 25 is eliminated, and the rotating freedom degree of the U-shaped connecting pieces 25 is reserved. A rail/strut connector 27 is welded to the central region of the rear half rail, which provides a secure connection for angle adjustment. A pair of unilateral trunnion bolt holes 28 are formed in the end part of the sliding guide rail 2, so that the sliding guide rail 2 can be stably connected with the base 8;
the rectangular aluminum plate 20 is a rectangular aluminum plate with a width of 100mm and a length of 1.2 m. 6 rows of sunken bolt holes are uniformly arranged on the upper surface, the bolt holes are all M10 in size and are provided with internal bolts, and the specific structure is shown as the mark 20 in figures 3 and 4;
the structure of the Z-shaped aluminum plate 21 is that a flat plate is bent twice to form a Z shape, the Z-shaped aluminum plate 21 is provided with bolt through holes which are the same as those of the cuboid support aluminum plate 20, the two can be hinged together through bolts of M10, and the Z-shaped structure is shown as a mark 21 in figure 7;
the bolts 22 are all 10mm in diameter and are standard M10 hex bolts.
The chuck 23 is a small rectangular iron sheet with the length of 100mm, the width of 20mm and the thickness of 5mm, two ends of the chuck are respectively provided with a bolt hole with the diameter of 10mm, and the middle of the chuck is bent for four times, so that the middle area is provided with a small arch area which can be fastened with a Z-shaped plate aluminum plate 21 structure, and the axial side view of the specific structure is 8;
this T type spare 24 is formed by two small-size rectangular boards vertical welding, and one is the wide 80mm thick 5mm of long 100mm, and another has a circular through-hole side length that the diameter is 10mm for the centre to be the square board of 60 mm. The rectangular plate is fastened on the back of the rectangular support aluminum plate 20 by welding. A round through hole with the size of 10 is arranged in the center of a square plate vertical to the square plate and is used for being hinged with the U-shaped connecting piece 25, and the specific structure is seen in an axial side view 9;
the U-shaped connecting piece 25 is formed by bending a cuboid aluminum sheet with the length of 160mm, the width of 30mm and the thickness of 10mm, the shape is similar to a U, a round bolt through hole with the size of 10 is respectively arranged in the central areas of the bottom surface and the two side surfaces of the U-shaped connecting piece, and the axial side view 10 of the U-shaped connecting piece is shown among specific structures;
this U type arched door spare 26 is through bending twice the U shape part that has a breach with the aluminium strip of 95mm long wide 20mm, and the both legs of U type arched door spare 26 all weld on cuboid support aluminum plate 20. Two welded rows are distributed side by side, as indicated by reference 26 in fig. 4;
the guide rail/support rod connector 27 is characterized in that a rectangular aluminum plate with the length of 100mm and the width of 50mm is used as a base, two lugs are welded on the base at intervals of 50mm in parallel, a bolt hole with the diameter of 10mm is respectively arranged in the middle of each lug and is used for being hinged with an angle adjusting support rod 6, and the specific structure is shown in an axial side view 11;
the unilateral trunnion bolt hole 28 is a sunken hole with the diameter of 10, is internally threaded, is positioned at the end part of the sliding guide rail 2 by 70mm and is used for connecting a unilateral trunnion connecting piece 82;
the leg 3 comprises a leg hollow square bar 31 and a leg connector 32. Their mutual positional relationship is: the 2 leg hollow square bars 31 are fastened and connected by bolts through leg connectors 32. One end of the supporting leg 3 is hinged with the U-shaped connecting piece (25) through a bolt, and the other end of the supporting leg is hinged with the supporting leg fixing piece 4 through a bolt;
the hollow square bar 31 of the support leg is a hollow cuboid square column with the length of 1.2m, and the cross section of the square column is in a shape like a Chinese character 'hui'. The square of the outer frame of the section is changed into 20, and the side length of the square of the inner frame is 10 mm. Both ends of the leg hollow square bar 31 are provided with bolt through holes with a diameter of 10mm in one direction. The specific structure is shown as the mark 31 in FIG. 5;
the leg connecting member 32 is also a hollow rectangular column, and the cross section is also in a shape of a Chinese character 'hui'. The size of the hollow section of the inside of the leg connecting piece 32 is equal to that of the section of the outside of the leg hollow square rod 31. Two parallel sides in one direction of leg connecting piece 32 are opened side by side 2 bolt holes with the diameter of 10mm, and the specific structure is shown as reference number 31 in figure 5.
The main structure of the supporting leg fixing part 4 is that 2 small flat plates with holes at the centers are vertically welded on a square plate with the side length of 100mm side by side. Four bolt holes with the diameter of 10mm are formed in the bottom surface square plate, and the bolt holes are symmetrically and uniformly distributed. Two square plates with holes are welded in the central area of the bottom square plate at a certain distance; when the launcher is used, the expansion bolts penetrate through the bolt holes to fasten the bottom surface square plate on the ground, and the square plate with the holes and the supporting legs 3 can be hinged through common bolts, so that the problems that the launcher inclines due to lateral vibration or wind power in the launching process and the like are solved, and the specific structure is shown as a mark 4 in fig. 5;
l type guide rail connecting rod 5 is used for two blocks of accurate connection end to end cuboid support aluminum plate 20 of placing. The L-shaped guide rail connecting rod 5 is formed by bending an iron bar with a square section of 25mm at one time, the shape is similar to an L shape, and the specific structure is shown in figure 12;
the angle adjusting support rod 6 is a rectangular plate with the thickness of 20mm, the two ends of the thick plate are in arc transition, a hollow cylinder with the center of an arc is arranged at each of the two ends, and the diameter of the cylinder hole is 10 mm. The hollow cylinder is hinged with the guide rail/support rod connector 27 through a shaft or a bolt, the other end of the hollow cylinder is connected with the guide rail support sliding rail 7 through a bolt, the angle adjusting support rod 6 can move along the guide rail support sliding rail 7 to adjust the emission angle, and the specific structure is shown in a shaft side view 13;
the peripheral outline of the guide rail supporting slide rail 7 is a rectangular prism, and the outline is 800mm long and 30mm wide. The cuboid center has one to be used for fixed bolt pole by the small-size cuboid of fretwork, and the guide rail supports the both ends of slide rail 7 moreover and all has the bolt hole that the diameter is 10 mm. One end of which can be used for fastening in connection with the base 8. The guide rail supports the strip cuboid with the hollow center of the slide rail 7, so that the bolt rod has certain movement automation degree to achieve the purpose of adjusting the emission angle, and the specific structure is shown as an axial side view 14;
the base 8 is composed of a base mounting plate 81 and a single-side trunnion connecting piece 82. The single-sided trunnion connector 82 is hinged and fastened to the base mounting plate 81 by bolts. Three unilateral trunnion connectors 82 are hinged together through bolts, and the other two unilateral trunnion connectors are fastened on the unilateral trunnion bolt holes 28 through bolts; as shown in fig. 6 and 15;
the base mounting plate 81 is formed of an aluminum plate having a thickness of 30 mm. The middle area of the aluminum plate is provided with a hollow flame through hole with the radius of 30mm, the edge of the aluminum plate is also provided with a hole with the same size, and the hole is positioned at the edge of the cuboid, so the aluminum plate is half-moon-shaped; a plurality of bolt holes are uniformly distributed on the base mounting plate, protruded rectangular strips with holes are distributed on the peripheral side surfaces of the base mounting plate and appear in pairs, the bolt holes are formed in the rectangular strips with holes, the anti-overturning performance can be improved while the weight is reduced, and corresponding connecting rods can be connected to realize additional functions if other requirements exist, wherein the marks 81 in the specific structural shaft side view 15 are shown;
the shape of the unilateral trunnion fixing seat 82 is similar to that of a whistle, a shaft hole is formed in the side surface area of the head of the whistle, and an installation bolt hole is formed in the mouth area of the whistle and used for installing the unilateral trunnion fixing seat 82 on the unilateral trunnion bolt hole 28 or the base installation plate 81, wherein the specific structure is shown by a mark 82 in an axial side view 15;
according to the portable detachable folding missile/rocket 1 launching device, the front and rear direction finders (11 and 12) are mounted on the missile body 10 of the missile/rocket 1 and can freely slide along the sliding guide rails 2 on the direction finders (11 and 12), so that the launching direction of the missile/rocket 1 is ensured. By arranging the front and rear direction finders (11 and 12) as guide rail moving support sliding blocks, different types of missiles/rockets 1 can be launched by the same launching device, and the use frequency of the launching device is improved. The front guide rail and the rear guide rail are connected through the L-shaped guide rail connecting rod 5 to form an accurate long-strip-shaped track, the size of parts of the launching device is reduced, meanwhile, the length of the launching guide rail is still guaranteed, and the maneuverability and flexibility of the launching device are greatly improved. The structural design of the supporting legs 3 and the angle adjusting supporting rods 6 enables the launching device to launch missiles/rockets to different angles and improves the stability of the launching device. This emitter fastens each part through multiple small-size connecting piece and articulates, uses up to dismantle into small-size part and conveniently carries the transportation, compares with car or train transportation, has greatly reduced the restriction to the transportation condition, has greatly improved individual soldier's operational capability and operation scope.
Claims (10)
1. A portable detachable folding missile-rocket launching device is characterized in that: the missile/rocket launcher comprises a missile/rocket (1), a missile body (10), a front direction finder (11), a rear direction finder (12), a tail wing (13), a sliding guide rail (2), a cuboid supporting aluminum plate (20), a Z-shaped plate aluminum plate (21), bolts (22), clamping heads (23), T-shaped pieces (24), U-shaped connecting pieces (25), U-shaped arch door pieces (26), guide rail/supporting rod connectors (27), single-side trunnion bolt holes (28), supporting legs (3), supporting leg hollow square rods (31), supporting leg connecting pieces (32), supporting leg fixing pieces (4), L-shaped guide rail connecting rods (5), angle adjusting supporting rods (6), guide rail supporting slide rails (7), a base (8), a base mounting plate (81) and single-side trunnion connecting pieces (82);
the mutual position relationship of the above components is: the missile/rocket is characterized in that an I-shaped front direction finder (11) and a rear direction finder (12) are respectively connected with the surface gravity center of a missile body (10) of the missile/rocket (1) and the surface of the front end of a tail wing (13) on the same axis; before launching, a front director (11) and a rear director (12) of the missile/rocket (1) are pushed into the sliding guide rail (2) along matching grooves in a sliding mode, and the missile/rocket (1) can freely slide along the guide rail sliding grooves through the front director (11) and the rear director (12); the guide rail (2) is structurally provided with two cuboid support aluminum plates (20) and a Z-shaped aluminum plate (21); each Z-shaped aluminum plate (21) is fastened with a corresponding cuboid support aluminum plate (20) through bolts, and the two parts are spliced side by side to form the shape of the guide rail (2); 2 rows of U-shaped arch door pieces (26) are respectively connected in parallel in the splicing position area of the U-shaped arch door pieces and the L-shaped guide rail connecting rods (5) are inserted along the notches of the U-shaped arch door pieces (26) to ensure that the U-shaped arch door pieces and the L-shaped guide rail connecting rods are accurately butted and form a seamless butted track; a T-shaped piece (24) is connected to the central region of the back of the rectangular support aluminum plate (20) close to the front end, and the T-shaped piece (24) is connected with the U-shaped connecting piece (25) through a bolt, so that the U-shaped connecting piece (25) can rotate but cannot move; a guide rail/support rod connector (27) is fixedly connected with the middle area of the two cuboid support aluminum plates (20) close to the rear end, and a clamping head (23) is arranged above the front surface of the tail part of the guide rail/support rod connector and used for preventing the guided missile/rocket (1) from withdrawing from the guide rail (2) during static placement; the rear area of the back surface of the shell is provided with a pair of unilateral trunnion bolt holes (28); the U-shaped connecting piece (25) in the central area of the front part of the guide rail (2) is connected with the supporting leg (3) to prevent the launcher from overturning during launching; the supporting leg (3) connects two supporting leg hollow square rods (31) through a supporting leg connecting piece (32), one end of each supporting leg is connected with the U-shaped connecting piece (25), and the other end of each supporting leg is connected with a supporting leg fixing piece (4) and used for fixing the supporting leg (3) on the ground; a guide rail/support rod connector (27) on the back of the rear end of the guide rail (2) is connected with the angle adjusting support rod (6) and is used for supporting the guide rail (2) and adjusting the emission angle of the guide rail (2); the middle part of the guide rail supporting slide rail (7) is a hollow rectangular groove, one end of the angle adjusting support rod (6) is fastened and fixed with the guide rail supporting slide rail (7) through a bolt, and when the bolt is loosened, the angle adjusting support rod (6) can freely slide along the groove channel of the guide rail supporting slide rail (7) to adjust the hair-sending angle; the guide rail supporting slide rail (7) is fixedly connected to a base (8) through bolts, bolt holes are uniformly distributed in parallel on a base mounting plate (81), and a unilateral trunnion connecting piece (82) is fixedly connected to the base mounting plate (81) through bolts;
the missile/rocket (1) consists of a missile body (10), a front director (11), a rear director (12) and a tail wing (13); the front direction finder (11) and the rear direction finder (12) are connected and bolted on the same axis of the surface of the bullet body (10), the front direction finder (11) is usually positioned near the center of gravity, and the rear direction finder (12) is positioned in front of the tail wing (13) and close to the tail wing (13);
the bullet body (10) is generally a cylindrical shell, the front end of the bullet body is a conical structure, and the bullet body has small resistance in flight; the wall thickness of the shell structure and the connecting structure are related to the requirements and the specific design of the arrow body structure;
the front direction finder (11) and the rear direction finder (12) are I-shaped, and the front direction finder and the rear direction finder have the same structure and are respectively arranged at the middle part and the rear part of the same axis on the surface of the missile/rocket (1); the front and back direction finders (11, 12) are connected and hinged on the bullet body (10) by bolts, and the lower surfaces of the I-shaped front and back direction finders (11, 12) cling to the lower surfaces of the guide rail grooves to slide when the bullet is launched;
the structure of the tail wing (13) is a four-piece axisymmetric trapezoid structure, and the tail wing (13) is fixed at the tail part of the bullet body (10) in a clamping groove fixing mode;
the sliding guide rail (2) is composed of a rectangular support aluminum plate (20), a B-shaped plate aluminum plate (21), a bolt (22), a clamping head (23), a T-shaped piece (24), a U-shaped connecting piece (25), a U-shaped arch door piece (26), a guide rail/support rod connector (27) and a single-side trunnion bolt hole (28); their positional relationship to each other is: the main body structure of the sliding guide rail (2) is formed by splicing two cuboid supporting aluminum plates (20) with the same shape, 2Z-shaped aluminum plates (21) are symmetrically arranged on the two cuboid supporting aluminum plates (20) respectively, and bolt holes which are uniformly distributed are arranged at corresponding positions on the cuboid supporting aluminum plates (20) and the Z-shaped aluminum plates (21) and are fastened by bolts (22); the tail part of the sliding guide rail is provided with a clamping head (23) which is fastened on the sliding guide rail (2) through a bolt (22); seen from the back of the sliding guide rail (2), two rows of U-shaped arch door pieces (26) are connected to two sides of the splicing area, and are inserted side by side through two L-shaped guide rail connecting rods (5) to ensure the accurate butt joint of the two; the central area of the front semi-conductor rail of the sliding guide rail (2) is connected with a T-shaped part (24), the T-shaped part (24) is connected with 2U-shaped connecting pieces (25) through bolts, the moving freedom degree of the U-shaped connecting pieces (25) is eliminated, and the rotating freedom degree of the U-shaped connecting pieces (25) is reserved; the central area of the rear half guide rail is connected with a guide rail/supporting rod connector (27), and the end part of the sliding guide rail (2) is provided with a pair of unilateral trunnion bolt holes (28);
the cuboid supporting aluminum plate (20) is a rectangular aluminum plate, sink bolt holes are uniformly arranged on the rectangular aluminum plate, and an inner bolt is arranged on the rectangular aluminum plate;
the Z-shaped aluminum plate (21) is structurally characterized in that a flat plate is bent twice to form a Z shape, bolt through holes identical to those of the rectangular support aluminum plate (20) are formed in the Z-shaped aluminum plate (21), and the two can be hinged together through bolts;
the bolt (22) is a standard part;
the clamping head (23) is structurally a small rectangular iron sheet, bolt holes are formed in two ends of the small rectangular iron sheet respectively, and the middle of the small rectangular iron sheet is bent for four times, so that a small arch area is formed in the middle area and can be fastened with a Z-shaped plate aluminum plate (21) structure;
the T-shaped part (24) is formed by vertically connecting two small rectangular plates, and one surface of the T-shaped part is fastened on the back surface of a rectangular support aluminum plate (20) through connection and bolts; a circular through hole is arranged in the center of the rectangular plate vertical to the circular through hole;
the U-shaped connecting piece (25) is formed by bending a small rectangular aluminum sheet, the shape of the U-shaped connecting piece is similar to a U shape, and the central areas of the bottom surface and the two side surfaces of the U-shaped connecting piece are respectively provided with a circular bolt through hole;
the U-shaped arched door piece (26) is a U-shaped part with a notch formed by bending an aluminum strip twice, and two legs of the U-shaped arched door piece (26) are connected to a rectangular support aluminum plate (20); two connecting rows are distributed side by side;
the guide rail/support rod connector (27) is characterized in that a rectangular aluminum plate is used as a base, two lugs are connected on the base side by side, and a bolt hole is formed in the middle of each lug and used for being hinged with the angle adjusting support rod (6);
the unilateral trunnion bolt hole (28) is a sunken hole, is internally provided with threads, is positioned at the end part of the sliding guide rail (2) and is used for connecting a unilateral trunnion connecting piece (82);
the supporting legs (3) comprise supporting leg hollow square bars (31) and supporting leg connecting pieces (32); 2 support leg hollow square rods (31) are fastened and connected through support leg connecting pieces (32) by bolts; one end of the supporting leg (3) is hinged with the U-shaped connecting piece (25) through a bolt, and the other end of the supporting leg is hinged with the supporting leg fixing piece (4) through a bolt;
the hollow square rod (31) of the supporting leg is a hollow cuboid square column, and the cross section of the square column is in a shape like a Chinese character 'hui'; both ends of the hollow square rod (31) of the supporting leg are provided with bolt through holes in one direction;
the landing leg connecting piece (32) is also a hollow cuboid column, and the section is also in a shape of Chinese character hui; the size of the hollow section in the landing leg connecting piece (32) is equal to that of the section outside the landing leg hollow square rod (31); two parallel surfaces in one direction of the leg connecting piece (32) are provided with 2 bolt holes side by side;
the main structure of the supporting leg fixing part (4) is that 2 small flat plates with holes at the centers are vertically connected side by side on a square plate; the bottom surface square plate is provided with a square plate with four bolt holes, and the bolt holes are symmetrically and uniformly distributed; the central area on the bottom square plate is connected with two square plates with holes at a certain distance; when in use, the bottom square plate is fastened on the ground by using expansion bolts to penetrate through the bolt holes, and the square plate with the holes and the supporting legs (3) can be hinged by using common bolts;
the L-shaped guide rail connecting rod (5) is used for accurately connecting two cuboid supporting aluminum plates (20) which are arranged end to end in a connected mode; the L-shaped guide rail connecting rod (5) is formed by bending an iron bar with a rectangular cross section for one time, and is L-shaped;
the angle adjusting support rod (6) is structurally a rectangular thick plate with a preset thickness, two ends of the thick plate are in arc transition, and a hollow cylinder with an arc center as a circular point is arranged at each of the two ends; the hollow cylinder is hinged with the guide rail/support rod connector (27) through a shaft and a bolt, the other end of the hollow cylinder is connected with the guide rail support sliding rail (7) through the bolt, and the angle adjusting support rod (6) can move along the guide rail support sliding rail (7) to adjust the emission angle;
the periphery of the guide rail supporting slide rail (7) is a columnar cuboid, a hollowed small cuboid is arranged in the center of the cuboid and used for fixing a bolt rod, and bolt holes are formed in two ends of the guide rail supporting slide rail (7); one end of the base can be used for being connected and fastened with the base (8); the guide rail supports the strip cuboid with the hollow center of the slide rail (7) to ensure that the bolt rod has a preset movement automation degree so as to achieve the purpose of adjusting the emission angle;
the base (8) consists of a base mounting plate (81) and a unilateral trunnion connecting piece (82); the unilateral trunnion connecting piece (82) is hinged and fastened on the base mounting plate (81) through a bolt; three unilateral trunnion connecting pieces (82) are hinged together through bolts, and the other two unilateral trunnion connecting pieces are fastened on unilateral trunnion bolt holes (28) through bolts;
the main body of the base mounting plate (81) is an aluminum plate; the middle area of the aluminum plate is provided with a large hollow flame hole, the edge of the aluminum plate is also provided with a hole with the same size, and the aluminum plate is in a half-moon shape because the aluminum plate is positioned at the edge of the cuboid; bolt holes are uniformly distributed on the base mounting plate, and protruded rectangular strips with holes are distributed on the peripheral side surface and appear in pairs;
the shape of the unilateral trunnion fixing seat (82) is similar to that of a whistle, a shaft hole is formed in the side surface area of the head of the whistle, and an installation bolt hole is formed in the mouth area of the whistle and used for installing the unilateral trunnion fixing seat (82) on the unilateral trunnion bolt hole (28) and the base installation plate (81); the portable detachable folding missile/rocket launching device can be detached into small parts, is convenient to carry and transport, is not limited by road and railway conditions, and greatly improves the flexibility and the maneuvering transfer speed; the launching device has a simple integral structure and lower requirements on operators, so that the individual combat capability of individual soldiers can be greatly improved.
2. A portable collapsible missile-rocket launcher according to claim 1 in which: the front direction finder (11) and the rear direction finder (12) are I-shaped, and the material of the front direction finder and the rear direction finder is stainless steel.
3. A portable collapsible missile-rocket launcher according to claim 1 in which:
6 rows of sunken bolt holes are uniformly arranged on the cuboid support aluminum plate (20), and the bolt holes are all M10 in size and are provided with internal bolts.
4. A portable collapsible missile-rocket launcher according to claim 1 in which: the bolts (22) are standard parts, each having a diameter of 10 mm.
5. A portable collapsible missile-rocket launcher according to claim 1 in which: the T-shaped part (24) is a circular through hole in the center of the rectangular plate perpendicular to the T-shaped part, and the diameter of the through hole is 10 mm.
6. A portable collapsible missile-rocket launcher according to claim 1 in which:
the U-shaped connecting piece (25) is provided with a circular bolt through hole in the central area of the bottom surface and the two side surfaces respectively, and the diameter of the circular bolt through hole is 10 mm.
7. A portable collapsible missile-rocket launcher according to claim 1 in which: the unilateral trunnion bolt hole (28) is a sunken hole, is internally provided with threads, and has the diameter of 10 mm.
8. A portable collapsible missile-rocket launcher according to claim 1 in which:
the hollow square rod (31) of the landing leg is a hollow cuboid square column, and the length of the square column is 1.2 m; the cross section of the utility model is in a shape like a Chinese character hui; the two ends of the hollow square rod (31) of the supporting leg are provided with bolt through holes in one direction, and the diameter of each bolt through hole is 10 mm.
9. A portable collapsible missile-rocket launcher according to claim 1 in which: the two ends of the guide rail supporting slide rail (7) are respectively provided with a bolt hole, and the diameter of each bolt hole is 10 mm.
10. A portable collapsible missile-rocket launcher according to claim 1 in which: the main body of the base mounting plate (81) is an aluminum plate, and the thickness of the aluminum plate is 30 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910777813.4A CN110631419B (en) | 2019-08-22 | 2019-08-22 | Portable detachable folding missile-rocket launching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910777813.4A CN110631419B (en) | 2019-08-22 | 2019-08-22 | Portable detachable folding missile-rocket launching device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110631419A true CN110631419A (en) | 2019-12-31 |
| CN110631419B CN110631419B (en) | 2022-04-08 |
Family
ID=68970807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910777813.4A Active CN110631419B (en) | 2019-08-22 | 2019-08-22 | Portable detachable folding missile-rocket launching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110631419B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111854545A (en) * | 2020-06-04 | 2020-10-30 | 中国人民解放军国防科技大学 | Boosting gliding small-sized test rocket system |
| CN112548957A (en) * | 2020-11-05 | 2021-03-26 | 蓝箭航天技术有限公司 | Movable supporting device for assembling rocket engine |
| CN112696978A (en) * | 2020-12-24 | 2021-04-23 | 彩虹无人机科技有限公司 | Small missile ground launching height falling prevention method |
| CN113218247A (en) * | 2021-05-27 | 2021-08-06 | 北京星途探索科技有限公司 | Simple launching platform capable of adjusting launching inclination angle |
| CN114577062A (en) * | 2022-02-25 | 2022-06-03 | 西安航天发动机有限公司 | Truss type structure loading test platform |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020000174A1 (en) * | 2000-06-28 | 2002-01-03 | Seller Reginald Paul | Self-propelled rocket and collapsible rocket launch stand for use in providing the controlled occurence of an avalanche or a mud slide |
| RU2007116600A (en) * | 2007-05-02 | 2008-11-10 | Хаджи-Мурат Хасанович Байсиев (RU) | ROCKET LAUNCHER |
| CN201903289U (en) * | 2010-11-12 | 2011-07-20 | 中国路桥工程有限责任公司 | Rocket launcher |
| US20120060674A1 (en) * | 2008-09-12 | 2012-03-15 | Raytheon Company | Composite reinforced missile rail |
| 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 |
| RU2544037C1 (en) * | 2013-09-25 | 2015-03-10 | Открытое акционерное общество "Завод им. В.А. Дегтярева" | Launching facility |
| CN106043731A (en) * | 2016-06-22 | 2016-10-26 | 浙江大学 | Improved aircraft launching cradle |
| CN109780931A (en) * | 2019-01-28 | 2019-05-21 | 上海机电工程研究所 | It is a kind of based on MISSILE LAUNCHING with can angular transformation fixation device |
-
2019
- 2019-08-22 CN CN201910777813.4A patent/CN110631419B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020000174A1 (en) * | 2000-06-28 | 2002-01-03 | Seller Reginald Paul | Self-propelled rocket and collapsible rocket launch stand for use in providing the controlled occurence of an avalanche or a mud slide |
| RU2007116600A (en) * | 2007-05-02 | 2008-11-10 | Хаджи-Мурат Хасанович Байсиев (RU) | ROCKET LAUNCHER |
| US20120060674A1 (en) * | 2008-09-12 | 2012-03-15 | Raytheon Company | Composite reinforced missile rail |
| CN201903289U (en) * | 2010-11-12 | 2011-07-20 | 中国路桥工程有限责任公司 | Rocket launcher |
| RU2544037C1 (en) * | 2013-09-25 | 2015-03-10 | Открытое акционерное общество "Завод им. В.А. Дегтярева" | Launching facility |
| 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 |
| CN106043731A (en) * | 2016-06-22 | 2016-10-26 | 浙江大学 | Improved aircraft launching cradle |
| CN109780931A (en) * | 2019-01-28 | 2019-05-21 | 上海机电工程研究所 | It is a kind of based on MISSILE LAUNCHING with can angular transformation fixation device |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111854545A (en) * | 2020-06-04 | 2020-10-30 | 中国人民解放军国防科技大学 | Boosting gliding small-sized test rocket system |
| CN111854545B (en) * | 2020-06-04 | 2022-09-30 | 中国人民解放军国防科技大学 | Boosting gliding small-sized test rocket system |
| CN112548957A (en) * | 2020-11-05 | 2021-03-26 | 蓝箭航天技术有限公司 | Movable supporting device for assembling rocket engine |
| CN112696978A (en) * | 2020-12-24 | 2021-04-23 | 彩虹无人机科技有限公司 | Small missile ground launching height falling prevention method |
| CN113218247A (en) * | 2021-05-27 | 2021-08-06 | 北京星途探索科技有限公司 | Simple launching platform capable of adjusting launching inclination angle |
| CN114577062A (en) * | 2022-02-25 | 2022-06-03 | 西安航天发动机有限公司 | Truss type structure loading test platform |
| CN114577062B (en) * | 2022-02-25 | 2024-02-09 | 西安航天发动机有限公司 | Truss type structure loading test platform |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110631419B (en) | 2022-04-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110631419B (en) | Portable detachable folding missile-rocket launching device | |
| US6491303B1 (en) | Portable target | |
| ES2220884T3 (en) | DEVICE FOR MAKING MECHANICAL TESTS ON STRUCTURES (RAILWAYS, REGULABLE PIROTECHNICAL LAUNCHER, VIA FERREA). | |
| US20110037227A1 (en) | Portable projectile trap assembly | |
| US4505442A (en) | Transient surface contact vehicle | |
| RU2617162C1 (en) | Spacecraft, its payload module and service system module | |
| CN108349596A (en) | Payload distribution system | |
| CN210952524U (en) | Movable rocket launching cradle and rocket launching vehicle | |
| US6079310A (en) | Portable launcher | |
| ES2211664T3 (en) | REDUCED SIZE RADIOCONTROLLED FLYING DEVICE. | |
| KR101839130B1 (en) | Compressed air propulsion flying object. | |
| CA1125071A (en) | Rocket tube launcher with cast-in place tube support bulkhead | |
| CN113602386B (en) | Coal mine detection and rescue robot with glider and working method | |
| CN111854542A (en) | Active cruise return type liquid sounding rocket | |
| US3735985A (en) | Rocket propelled target | |
| US5299507A (en) | Ring guideway for rapid rail transit system | |
| Zaloga | German V-Weapon Sites 1943–45 | |
| CN205916345U (en) | Small -size fixed wing uavs launching cradle | |
| KR20040070337A (en) | Launcher platform | |
| RU2673447C1 (en) | Space vehicle | |
| RU2094337C1 (en) | Method for preparing launch pad for launching space rocket and ground equipment for performing launch | |
| CA1239137A (en) | Housing, especially for large equipment | |
| CN113606060B (en) | Movable fuel gas flow guide device and using method thereof | |
| CN109484612B (en) | A cantilever for oil moves unmanned aerial vehicle | |
| CN220450714U (en) | Portable movable indication board for highway |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |