CN114030616A - Anti-interference method and device for marching after air-drop war chariot landing - Google Patents
Anti-interference method and device for marching after air-drop war chariot landing Download PDFInfo
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- CN114030616A CN114030616A CN202111472387.7A CN202111472387A CN114030616A CN 114030616 A CN114030616 A CN 114030616A CN 202111472387 A CN202111472387 A CN 202111472387A CN 114030616 A CN114030616 A CN 114030616A
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- 238000000034 method Methods 0.000 title claims abstract description 25
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 66
- 239000010959 steel Substances 0.000 claims abstract description 66
- 229920000271 Kevlar® Polymers 0.000 claims abstract description 59
- 239000004761 kevlar Substances 0.000 claims abstract description 59
- 239000007853 buffer solution Substances 0.000 claims abstract description 57
- 239000002184 metal Substances 0.000 claims description 39
- 229920000742 Cotton Polymers 0.000 claims description 17
- 230000000712 assembly Effects 0.000 claims description 6
- 238000000429 assembly Methods 0.000 claims description 6
- 241001272720 Medialuna californiensis Species 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000013016 damping Methods 0.000 description 5
- 238000004904 shortening Methods 0.000 description 4
- 238000003825 pressing Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007429 general method Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/14—Absorbing landing shocks
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Abstract
The application provides a method and a device for preventing interference of marching after landing of an air-drop war chariot, which belong to the technical field of airborne landing air-drop, when the war chariot slowly moves forwards, a preset position of a rear wheel moves backwards, a Kevlar belt pulls a disengagement steel cable, and a stopper rotates when the disengagement steel cable moves backwards, so that a front beam is disengaged from a chassis of the war chariot, and the front end of a buffer system falls off and lands; when the war chariot moves forward, the rear beam and the war chariot chassis move relatively to slide out of the sliding groove, the buffer system is released from the war chariot chassis, and in the releasing process, the pulling stroke of the releasing steel cable backwards at the preset position of the rear wheel is not more than 10 cm. The invention avoids the damage to the wheel axle (or the track), eliminates the interference factor of the battle vehicle marching, shortens the preparation time for fighting, and is suitable for all vehicle types which are arranged in air-drop troops and take a cargo-free air-drop system as an air-drop carrier.
Description
Technical Field
The application belongs to the technical field of airborne and airdrop, and particularly relates to a marching anti-interference method and device after an airdrop war chariot is landed.
Background
With the development of various large-scale and high-performance transport aircraft, the air freight airdrop has increasingly prominent status and effect in modern war, and the fighting hit mode of reloading airdrop is also more emphasized. The built war chariot air-drop battle has important significance for suppressing enemy firepower and beaching and attacking forcibly, and also reflects the informatization and three-dimensional battle level of the army to a certain extent. The existing relatively mature war chariot air-drop modes mainly comprise a cargo bed air-drop mode and a cargo bed-free air-drop mode, the cargo bed air-drop mode is complex in binding and mooring the war chariot, the war chariot is difficult to escape after landing, time-consuming and labor-consuming, and the war chariot is extremely unfavorable for timely putting into combat to play the fighting efficiency; the cargo-free air-drop system has fewer interfaces with a chassis of the war chariot, can realize quick installation with the war chariot, can realize quick automatic release of the buffer system and the war chariot after the war chariot is air-dropped and landed, and immediately put into operation, thereby greatly shortening the conversion time from the air-drop landing to the time of playing the operation efficiency.
In the related art, when a combat vehicle is airdropped by using a cargo space-free airdrop system, a general method is to mount a buffer system on a chassis of the combat vehicle, and after the combat vehicle lands, the buffer system is released by pulling a release cable tied in the rear wheels (or behind tracks) in advance through forward movement of the combat vehicle, but the release cable tied in the rear wheels (or behind tracks) cannot be manually released, and once the two release cables with the length of nearly 4 meters are rolled into wheel axles (or tracks), the power system of the combat vehicle can be damaged and cannot move forward.
Disclosure of Invention
In order to solve the problem that the release steel cable causes interference to a wheel axle (or a track) after a buffer system releases the release steel cable when a war chariot in the related technology lands, the invention provides a method and a device for preventing interference to the march after the landing of the air-drop war chariot, which are used for solving the problem that the release steel cable of the buffer system tied on the rear wheel (or below the track) of the war chariot smoothly separates from the war chariot when the air-drop war chariot without a cargo platform lands at present, thereby avoiding the damage to the wheel axle (or the track) and eliminating the interference factors of the march of the war chariot, and the technical scheme is as follows:
in one aspect, a marching anti-interference method after an air-drop war vehicle lands is provided, and the method comprises the following steps:
forming two tamper assemblies, each tamper assembly comprising: the release steel rope 4, the Kevlar belt 6, the pin pulling belt 7, the rubber rope 9 and the connecting piece are connected, and one ends of the release steel rope 4, the pin pulling belt 7 and the rubber rope 9 are connected with the connecting piece; the folded end of the Kevlar belt 6 is connected with a connecting piece,
installing a buffer system 1 below an air-drop war chariot;
installing a connecting ring 14 at the front part of the chariot on a front beam 11 of the buffer system 1, and locking the connecting ring 14;
the ends of two releasing steel ropes 4 are respectively connected to two stoppers 2 at the middle part of a front beam 11 of a buffer system 1, the other ends of two rubber ropes 9 are respectively tied at 1/4 of two longitudinal beams 13 in the middle of the buffer system 1, a pin pulling belt 7 is tied on a rear beam 12 of the buffer system 1 at the corresponding side, two Kevlar belts 6 are respectively tied and tied at preset positions of rear wheels at the corresponding side, and the Kevlar belts 6, the releasing steel ropes 4 and the rubber ropes 9 have no loosening allowance;
the damping system 1 is disengaged from the chassis of the war chariot after the war chariot airdrops and lands, when the war chariot slowly moves forwards, the preset position of the rear wheel moves backwards, the Kevlar belt 6 pulls the disengaging steel cable 4, the disengaging steel cable 4 rotates the stopper 2 when moving backwards, and then the front beam 11 is disengaged from the chassis of the war chariot, and the front end of the damping system 1 falls off and lands; when the war chariot continues to move forwards, the rear beam 12 and the war chariot chassis generate relative motion to slide out of the sliding groove, the buffer system 1 is released from the war chariot chassis, and in the releasing process, the backward pulling stroke of the releasing steel cable 4 is not more than 10cm by the preset position of the rear wheel;
in the next forward movement of the chariot, the mooring point position of the Kevlar belt 6 at the preset position starts to move upwards or forwards, the pin pulling belt 7 is straightened and pulls the pin 8, the pin 8 is pulled out from the folded end of the Kevlar belt 6, the Kevlar belt 6 slides out from the metal ring 5, the releasing steel rope 4 is separated from the Kevlar belt 6, the rubber rope 9 quickly pulls the releasing steel rope 4 close to the wheels or the crawler belt to the center of the buffer system 1, and the releasing steel rope 4 is separated from the chariot.
Optionally, the connector comprises: the metal ring 5, the bolt 8 and the cotton rope 10, the forming process of each group of anti-interference components comprises:
one end of a releasing steel rope 4 is pressed and connected with a metal ring 5 in a pressing mode, a rubber rope 9 is sleeved on the metal ring 5, a Kevlar belt 6 is folded from the middle position in half, the folded end penetrates through the metal ring 5 at the end of the releasing steel rope 4 from bottom to top, a plug pin 8 connected with a pin pulling belt 7 is inserted into the folded end of the Kevlar belt 6 from back to front, and the plug pin 8 and the metal ring 5 are tied and secured through a cotton rope 10.
Optionally, the preset position is a lower track below or behind the hub.
Optionally, the installing the buffer system 1 under the air-drop war chariot comprises:
the convex part in the middle of the back beam 12 of the buffer system 1 is arranged in the groove at the tail part of the chariot.
Optionally, the mounting of the connecting ring 14 at the front of the chariot 1 on the front beam 11 and the locking of the connecting ring 14 comprises:
the connecting ring 14 at the front part of the war chariot is arranged in a groove at the middle part of the front beam 11 of the buffer system 1, the connecting ring 14 is locked by the stopper 2 on the front beam 11, and half-moon-shaped matching is adopted between the stopper 2 and the connecting ring 14.
In a second aspect, a marching anti-interference device after an air-drop war chariot is landed is provided, which comprises: two tamper assemblies, each tamper assembly comprising: the release steel rope 4, the Kevlar belt 6, the pin pulling belt 7, the rubber rope 9 and the connecting piece are connected, and one ends of the release steel rope 4, the pin pulling belt 7 and the rubber rope 9 are connected with the connecting piece; the folded end of the Kevlar belt 6 is connected with a connecting piece;
the end of the releasing steel cable 4 is connected with a stopper 2 at the middle part of a front beam 11 of the buffer system 1,
the other end of the rubber rope 9 is tied to 1/4 of the middle longitudinal beam 13 of the buffer system 1,
the pin pulling belt 7 is tied on the back beam 12 of the buffer system 1 on the corresponding side,
the Kevlar belt 6 is tied and tied at a preset position of the corresponding side rear wheel.
Optionally, the connector comprises: a metal ring 5, a bolt 8 and a cotton rope 10,
one end of the releasing steel cable 4 is pressed with a metal ring 5,
a rubber rope 9 is sleeved on the metal ring 5,
the doubling-over end of the Kevlar belt 6 doubled over from the middle is connected with the metal ring 5,
the pin pulling belt 7 is connected with a pin 8,
a bolt 8 is inserted into the doubling-up end of the Kevlar belt 6,
the cotton string 10 is used to tie the bolt 8 to the metal ring 5 for security.
Optionally, the weight of the cotton string 10 is 5kg to 11 kg.
The invention solves the problem that the buffer system tied on the rear wheels (or tracks) of the war chariot releases the steel cable from smoothly separating from the war chariot after the prior air-drop war chariot using the cargo-free air-drop system lands, thereby avoiding the damage to the wheel axle (or tracks) of the wheels, eliminating the interference factors of the war chariot marching, shortening the preparation time for fighting, and being suitable for all vehicle types which are arranged in a train and take the air-drop system without the cargo-free platform as the air-drop carrier.
Drawings
FIG. 1 is a partial detailed schematic view of the present invention;
FIG. 2 is a schematic view of the rear end of the bumper system of the present invention connected to a combat tank;
FIG. 3 is a schematic view of the front end of the bumper system of the present invention connected to a combat tank;
FIG. 4 is a schematic view of the overall connection of the present invention;
FIG. 5 is a schematic illustration of the disengagement of the steel cord of the present invention.
The device comprises a buffer system 1, a stopper 2, a bolt 3, a steel cable 4, a metal ring 5, a Kevlar rope 6, a pin pulling belt 7, a pin 8, a rubber rope 9, a cotton rope 10-5, a front beam 11, a rear beam 12, a longitudinal beam 13 and a connecting ring 14.
Detailed Description
The present application will now be described in further detail with reference to specific embodiments and the accompanying drawings.
The invention provides a marching anti-interference method after an air-drop war chariot lands, which solves the problem that a buffer system tied to the rear wheel (or the rear part of a crawler belt) of the war chariot is easy to damage a wheel axle (or the crawler belt) by a steel cable after the air-drop war chariot lands by using a cargo-free platform air-drop system at present, so that the steel cable is smoothly separated from the war chariot, thereby avoiding the damage to the wheel axle (or the crawler belt), eliminating the interference factors of the war chariot marching, shortening the preparation time for fighting, and being suitable for all vehicle types which are arranged in a train and take an air-drop army and take the cargo-free platform air-drop system as an air-drop carrier.
Referring to fig. 1, there is shown a structure diagram of a marching anti-interference device after landing of an air-drop war chariot, including: two tamper assemblies, each tamper assembly comprising: the release steel rope 4, the Kevlar belt 6, the pin pulling belt 7, the rubber rope 9 and the connecting piece are connected, and one ends of the release steel rope 4, the pin pulling belt 7 and the rubber rope 9 are connected with the connecting piece; the folded end of the Kevlar belt 6 is connected with a connecting piece;
as shown in fig. 4, the end of the release wire 4 is connected to the stopper 2 at the middle portion of the front beam 11 of the cushion system 1,
the other end of the rubber rope 9 is tied to 1/4 of the middle longitudinal beam 13 of the buffer system 1,
the pin pulling belt 7 is tied on the back beam 12 of the buffer system 1 on the corresponding side,
the Kevlar belt 6 is tied and tied at a preset position of the corresponding side rear wheel. The preset position is a lower crawler below or behind the hub.
Wherein, the connecting piece includes: a metal ring 5, a bolt 8 and a cotton rope 10,
one end of the releasing steel cable 4 is pressed with a metal ring 5,
a rubber rope 9 is sleeved on the metal ring 5,
the doubling-over end of the Kevlar belt 6 doubled over from the middle is connected with the metal ring 5,
the pin pulling belt 7 is connected with a pin 8,
a bolt 8 is inserted into the doubling-up end of the Kevlar belt 6,
the cotton string 10 is used to tie the bolt 8 to the metal ring 5 for security.
Wherein, the weight of the cotton rope 10 can be 5 kg-11 kg.
The invention also provides a marching anti-interference method after the air-drop war chariot is landed, referring to fig. 1 to 5, the method comprises the following steps:
1) forming two tamper assemblies, each tamper assembly comprising: the release steel rope 4, the Kevlar belt 6, the pin pulling belt 7, the rubber rope 9 and the connecting piece are connected, and one ends of the release steel rope 4, the pin pulling belt 7 and the rubber rope 9 are connected with the connecting piece; the 6 fifty percent discount ends of kaffra cord area are connected with the connecting piece, the connecting piece includes: the metal ring 5, the bolt 8 and the cotton rope 10, the forming process of each group of anti-interference components comprises: one end of a releasing steel rope 4 is pressed and connected with a metal ring 5 in a pressing mode, a rubber rope 9 is sleeved on the metal ring 5, a Kevlar belt 6 is folded from the middle position in half, the folded end penetrates through the metal ring 5 at the end of the releasing steel rope 4 from bottom to top, a plug pin 8 connected with a pin pulling belt 7 is inserted into the folded end of the Kevlar belt 6 from back to front, and the plug pin 8 and the metal ring 5 are tied and secured through a cotton rope 10.
2) Installing a buffer system 1 below an air-drop war chariot; installing the bumper system 1 below an air-drop chariot, comprising: the convex part in the middle of the back beam 12 of the buffer system 1 is arranged in the groove at the tail part of the chariot.
3) Installing a connecting ring 14 at the front part of the chariot on a front beam 11 of the buffer system 1, and locking the connecting ring 14; installing the connecting ring 14 at the front part of the war chariot on the front beam 11 of the buffer system 1 and locking the connecting ring 14, comprising: the connecting ring 14 at the front part of the war chariot is arranged in a groove at the middle part of the front beam 11 of the buffer system 1, the connecting ring 14 is locked by the stopper 2 on the front beam 11, and half-moon-shaped matching is adopted between the stopper 2 and the connecting ring 14.
4) The ends of two releasing steel ropes 4 are respectively connected to two stoppers 2 at the middle part of a front beam 11 of a buffer system 1, the other ends of two rubber ropes 9 are respectively tied at 1/4 of two longitudinal beams 13 at the middle part of the buffer system 1, a pin pulling belt 7 is tied on a rear beam 12 of the buffer system 1 at the corresponding side, two Kevlar belts 6 are respectively tied and tied at preset positions of rear wheels at the corresponding side, and the preset positions are lower tracks below or behind hubs. The Kevlar belt 6, the release steel cable 4 and the rubber rope 9 have no slack allowance;
the damping system 1 is disengaged from the chassis of the war chariot after the war chariot airdrops and lands, when the war chariot slowly moves forwards, the preset position of the rear wheel moves backwards, the Kevlar belt 6 pulls the disengaging steel cable 4, the disengaging steel cable 4 rotates the stopper 2 when moving backwards, and then the front beam 11 is disengaged from the chassis of the war chariot, and the front end of the damping system 1 falls off and lands; when the war chariot continues to move forwards, the rear beam 12 and the war chariot chassis generate relative motion to slide out of the sliding groove, the buffer system 1 is released from the war chariot chassis, and in the releasing process, the backward pulling stroke of the releasing steel cable 4 is not more than 10cm by the preset position of the rear wheel;
in the next forward movement of the chariot, the mooring point position of the Kevlar belt 6 at the preset position starts to move upwards or forwards, the pin pulling belt 7 is straightened and pulls the pin 8, the pin 8 is pulled out from the folded end of the Kevlar belt 6, the Kevlar belt 6 slides out from the metal ring 5, the releasing steel rope 4 is separated from the Kevlar belt 6, the rubber rope 9 quickly pulls the releasing steel rope 4 close to the wheels or the crawler belt to the center of the buffer system 1, and the releasing steel rope 4 is separated from the chariot.
Specifically, the marching anti-interference method after the air-drop war chariot is landed comprises the following steps:
step 110, as shown in fig. 1, one end of the steel releasing rope 4 is pressed and connected with a metal ring 5, and a rubber rope 9 is sleeved on the metal ring 5. The Kevlar belt 6 is folded in half from the middle position, the folded end passes through the metal ring 5 at the end of the release steel cable 4 from bottom to top, the bolt 8 connected with the pin pulling belt 7 is inserted into the folded end of the Kevlar belt 6 from back to front, and the bolt 8 and the metal ring 5 are tied and secured by a 5kg cotton rope 10. Two groups were prepared in the same manner.
And step 120, installing the buffer system 1 below the air-drop war chariot. As shown in fig. 2, the male member of the middle of the rear beam 12 of the bumper system 1 is mounted in a recess in the rear of the vehicle.
Step 130, as shown in fig. 3, the connecting ring 14 at the front part of the chariot is installed in the groove at the middle part of the front beam 11 of the damping system 1, and the connecting ring 14 is locked by the stopper 2 on the front beam 11, and the stopper 2 and the connecting ring 14 adopt half-moon-shaped matching.
In step 140, as shown in fig. 4, the ends of the two release wires 4 are connected to the two stoppers 2 at the middle portion of the front beam 11 by bolts 3. The other ends of the two rubber ropes 9 are respectively tied at 1/4 of the two longitudinal beams 13 in the middle of the buffer system 1, the pin pulling belts 7 are tied at the rear beams 12 at the corresponding sides, the Kevlar belts 6 are respectively tied and tied below the hubs (or the lower tracks at the rear) of the rear wheels at the corresponding sides, and the Kevlar belts 6, the releasing steel ropes 4 and the rubber ropes 9 have no loosening allowance.
As shown in fig. 5, after the war chariot is dropped and landed, the buffer system 1 is disengaged from the chassis, when the war chariot slowly moves forward, the lower part of the hub of the rear wheel (or the lower crawler belt at the rear) moves backward, the disengaging steel cable 4 is pulled through the Kevlar belt 6, the stopper 2 rotates when the disengaging steel cable 4 moves backward, the front beam 11 is disengaged from the chassis of the war chariot, and the front end of the buffer system 1 falls off and lands; when the war chariot continues to move forward, the rear beam 12 and the war chariot chassis move relatively to slide out of the sliding groove, the buffer system 1 is released from the war chariot chassis, and in the releasing process, the backward pulling stroke of the releasing steel cable 4 below the hub (or the lower crawler belt below the rear) of the rear wheel is not more than 10 cm.
In the next forward travel of the war chariot, the mooring point position of the Kevlar belt 6 on the wheel (or the track) starts to move upwards (or forwards), the pin pulling belt 7 is straightened and pulls the pin 8, the pin 8 is pulled out from the folded end of the Kevlar belt 6, the Kevlar belt 6 slides out of the metal ring 5, the releasing steel cable 4 is separated from the Kevlar belt 6, the rubber rope 9 quickly pulls the releasing steel cable 4 close to the wheel (or the track) to the center of the buffer system 1, the releasing steel cable 4 is also separated from the connection relation with the war chariot, so that the interference on the wheel (or the track) of the war chariot is avoided, only one section of the Kevlar belt 6 is left on the wheel (or the track), and the march of the war chariot cannot be interfered and influenced.
The invention solves the problem that the buffer system tied on the rear wheels (or tracks) of the war chariot releases the steel cable from smoothly separating from the war chariot after the prior air-drop war chariot using the cargo-free air-drop system lands, thereby avoiding the damage to the wheel axle (or tracks) of the wheels, eliminating the interference factors of the war chariot marching, shortening the preparation time for fighting, and being suitable for all vehicle types which are arranged in a train and take the air-drop system without the cargo-free platform as the air-drop carrier.
The foregoing merely represents embodiments of the present application, which are described in greater detail and detail, and therefore should not be construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application.
Claims (8)
1. A marching anti-interference method after an air-drop war chariot is landed is characterized by comprising the following steps:
forming two tamper assemblies, each tamper assembly comprising: one end of each of the release steel cable (4), the Kevlar belt (6), the pin pulling belt (7), the rubber rope (9) and the connecting piece is connected with the connecting piece; the folded end of the Kevlar belt (6) is connected with a connecting piece,
installing a buffer system (1) below an air-drop war chariot;
installing a connecting ring (14) at the front part of the chariot on a front beam (11) of the buffer system (1), and locking the connecting ring (14);
the method comprises the following steps that the ends of two releasing steel ropes (4) are respectively connected to two stoppers (2) in the middle of a front beam (11) of a buffer system (1), the other ends of two rubber ropes (9) are respectively tied and stayed at 1/4 of two longitudinal beams (13) in the middle of the buffer system (1), a pin pulling belt (7) is tied and stayed on a rear beam (12) of the buffer system (1) on the corresponding side, two Kevlar belts (6) are respectively tied and stayed at preset positions of rear wheels on the corresponding side, and the Kevlar belt (6), the releasing steel ropes (4) and the rubber ropes (9) have no loosening allowance;
the rear buffer system (1) is disengaged from a chassis of the war chariot after the war chariot airdrops and lands, when the war chariot slowly moves forwards, the preset position of the rear wheel moves backwards, the Kevlar belt (6) pulls the disengaging steel cable (4), the disengaging steel cable (4) rotates the stopper (2) when moving backwards, the front beam (11) is further disengaged from the chassis of the war chariot, and the front end of the buffer system (1) falls and lands; when the war chariot moves forward, the rear beam (12) and the war chariot chassis move relatively to slide out of the sliding groove, the buffer system (1) is released from the war chariot chassis, and in the releasing process, the pulling stroke of the releasing steel cable (4) backwards is not more than 10cm at the preset position of the rear wheel;
in the following forward movement of the war chariot, the mooring point position of the Kevlar belt (6) at the preset position starts to move upwards or forwards, the pin pulling belt (7) is straightened and pulls the pin (8), the pin (8) is pulled out from the folded end of the Kevlar belt (6), the Kevlar belt (6) slides out from the metal ring (5), the releasing steel cable (4) is separated from the Kevlar belt (6), the rubber rope (9) quickly pulls the releasing steel cable (4) close to the wheels or the crawler belt to the center of the buffer system (1), and the releasing steel cable (4) is separated from the war chariot.
2. The method of claim 1, wherein the connector comprises: metal ring (5), bolt (8) and cotton rope (10), the formation process of every group jam-proof subassembly includes:
one end of a releasing steel rope (4) is pressed and connected with a metal ring (5), a rubber rope (9) is sleeved on the metal ring (5), a Kevlar belt (6) is folded from the middle position, the folded end penetrates through the metal ring (5) at the end of the releasing steel rope (4) from bottom to top, a plug pin (8) connected with a pin pulling belt (7) is inserted into the folded end of the Kevlar belt (6) from back to front, and the plug pin (8) and the metal ring (5) are tied and secured by a cotton rope (10).
3. The method of claim 1, wherein the predetermined location is under a hub or under a rear lower track.
4. Method according to claim 1, characterized in that said mounting of the buffer system (1) under the aerial delivery vehicle comprises:
a convex part in the middle of a rear beam (12) of the buffer system (1) is arranged in a groove at the tail part of the chariot.
5. The method of claim 1, wherein said mounting the chariot front attachment ring (14) on the bumper system (1) front beam (11) and locking the attachment ring (14) comprises:
a connecting ring (14) at the front part of a chariot is arranged in a groove at the middle part of a front beam (11) of a buffer system (1), the connecting ring (14) is locked by a stopper (2) on the front beam (11), and the stopper (2) is matched with the connecting ring (14) in a half-moon shape.
6. The utility model provides an air-drop war chariot marching interference preventer after landing which characterized in that includes: two tamper assemblies, each tamper assembly comprising: one end of each of the release steel cable (4), the Kevlar belt (6), the pin pulling belt (7), the rubber rope (9) and the connecting piece is connected with the connecting piece; the folded end of the Kevlar belt (6) is connected with the connecting piece;
the end of the releasing steel cable (4) is connected with a stopper (2) at the middle part of a front beam (11) of the buffer system (1),
the other end of the rubber rope (9) is tied at 1/4 of the middle longitudinal beam (13) of the buffer system (1),
the pin pulling belt (7) is tied on the back beam (12) of the buffer system (1) at the corresponding side,
the Kevlar belt (6) is tied and tied at a preset position of the corresponding side rear wheel.
7. The apparatus of claim 6, wherein the connector comprises: a metal ring (5), a bolt (8) and a cotton rope (10),
one end of the releasing steel cable (4) is pressed with a metal ring (5),
a rubber rope (9) is sleeved on the metal ring (5),
the doubling-over end of the Kevlar belt (6) doubled over from the middle position is connected with the metal ring (5),
the pin pulling belt (7) is connected with the pin (8),
a bolt (8) is inserted into the folded end of the Kevlar belt (6),
the cotton rope (10) is used for tying the bolt (8) and the metal ring (5) to be secured.
8. The apparatus of claim 7,
the weight of the cotton rope (10) is 5 kg-11 kg.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111472387.7A CN114030616A (en) | 2021-12-03 | 2021-12-03 | Anti-interference method and device for marching after air-drop war chariot landing |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111472387.7A CN114030616A (en) | 2021-12-03 | 2021-12-03 | Anti-interference method and device for marching after air-drop war chariot landing |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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| CN115871927A (en) * | 2022-11-18 | 2023-03-31 | 航宇救生装备有限公司 | Gravity air-drop method suitable for war chariot air-drop system |
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Application publication date: 20220211 |