CN113587724A - Underwater balance launching device and launching method thereof - Google Patents
Underwater balance launching device and launching method thereof Download PDFInfo
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- CN113587724A CN113587724A CN202110665435.8A CN202110665435A CN113587724A CN 113587724 A CN113587724 A CN 113587724A CN 202110665435 A CN202110665435 A CN 202110665435A CN 113587724 A CN113587724 A CN 113587724A
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- 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
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
Abstract
The invention discloses an underwater balance launching device and a launching method thereof, the underwater balance launching device comprises a launching tube, a bottom support and a balance cavity, the launching tube comprises a launching section and a power section, a launcher is arranged in the launching section, a power source is arranged in the power section, the launching section and the power section are separated by the bottom support, the bottom support can slide along the launching section under the action of external force, and the power source is prevented from leaking outside the launching tube and external water flows into the launching tube; the balance cavity is internally provided with a liquid pushing component, liquid is filled in the balance cavity, one end of the balance cavity is communicated with the power section, the other end of the balance cavity is communicated with the outside, and the liquid pushing component can move along the balance cavity under the action of external thrust. The invention can reduce the recoil of underwater launching and simultaneously takes the problems of high-pressure gas overflow, water hammer impact and the like into consideration.
Description
Technical Field
The invention relates to the technical field of underwater launching, in particular to an underwater balance launching device and a launching method.
Background
Underwater launch has a great deal of difficulty compared to ground launch. Including underwater seals, high pressure gas impingement, cross flow loading, etc., all make existing launch modes more limited in use. One of the difficulties of underwater launching is that when launching on a small platform, recoil in the launching process can cause the platform to generate great attitude change, which affects the normal work of the platform and also affects the posture of the missile when the missile goes out of the barrel. Thus, by balancing recoil, larger projectiles can be fired on smaller platforms.
As shown in fig. 1, the conventional underwater launching device includes a launch canister and a gas generator. When the aircraft in the launch canister needs underwater launching, after the engine or the fuel gas generator is ignited, a high-pressure area is formed at the tail part of the aircraft, the aircraft is pushed forwards, and the launch canister is pushed backwards. The launching mode enables the launch velocity of the aircraft to have a correlation with the recoil force applied to the platform. For small platforms, the magnitude of recoil severely impacts normal navigation after launch.
The existing underwater launching device has the following defects in the underwater launching process in summary:
1. the recoil of the platform is closely related to the aircraft launch velocity. So that the launch velocity of the aircraft is limited by the recoil that the platform can withstand. Meanwhile, the arrangement position of the launch canister is limited accordingly.
2. A large amount of bubbles are generated in the underwater launching process, and the launching characteristics are obvious. For submarines or other underwater vehicles in underwater battles, the position information of the submarines or other underwater vehicles is hopefully not exposed as much as possible in the launching process. Therefore, it is generally more desirable to have as little as possible amount of gas spilled after launch. And the adoption of high-pressure fuel gas for emission can cause a large amount of gas to leak out, so that the self position is exposed.
3. The water hammer impact characteristics after the shooting are obvious. After underwater launching, seawater outside the launching tube rushes into the launching tube, and under the combined action of inertia force and air mass elasticity, the bottom of the tube bears the shock impact of pressure circulation, and the shock peak value is probably far higher than the local external pressure. Adversely affecting both safety and stealth performance of the aircraft.
Disclosure of Invention
Aiming at the problems in the prior art, the invention aims to provide an underwater balance launching device and a launching method thereof, which can solve the problems of underwater launching recoil, high-pressure gas overflow, water hammer impact and the like.
In order to achieve the above object, a first aspect of the present invention provides an underwater balanced launching device, including a launching tube, a base, and a balance cavity, where the launching tube includes a launching section and a power section, a launcher is arranged in the launching section, a power source is arranged in the power section, the launching section and the power section are separated by the base, the base can slide along the launching section under the action of external force, and blocks the power source from leaking out of the launching tube and external water from flowing into the launching tube; a liquid pushing component is arranged in the balance cavity and is filled with liquid, one end of the balance cavity is communicated with the power section, the other end of the balance cavity is communicated with the outside, and the liquid pushing component can move along the balance cavity under the action of external thrust; the power source pushes the bottom support to move towards the outside of the launching section, so that the launched objects are driven to be launched towards the outside of the launching barrel, meanwhile, the liquid pushing component can be driven to push liquid towards the outside of the balance cavity, and then recoil is offset.
Furthermore, one end of the launching tube is opened, the other end of the launching tube is closed, and the power section is formed between the bottom support and the closed end of the launching tube; the underwater balance launching device further comprises an outer barrel and a connecting pipeline, the launching barrel is sleeved in the outer barrel, one end of the outer barrel is provided with an end cover, the other end of the outer barrel is communicated with the outside, an annular area between the launching barrel and the outer barrel forms the balance cavity, the liquid pushing component is an annular piston matched with the annular area in size, and the balance cavity is communicated with the power section through the connecting pipeline.
Furthermore, one end of the launching tube is opened, the other end of the launching tube is closed, and the power section is formed between the bottom support and the closed end of the launching tube; the underwater balance launching device further comprises an outer barrel and a connecting pipeline, the outer barrel and the launching barrel are arranged side by side, one end of the outer barrel is provided with an end cover, the other end of the outer barrel is communicated with the outside, the balance cavity is formed inside the outer barrel, the liquid pushing component is a piston matched with the inner diameter of the outer barrel, and the balance cavity is communicated with the power section through the connecting pipeline.
Furthermore, the collet and the liquid pushing component are arranged in the launching tube in a sliding mode, the liquid pushing component is a piston matched with the inner diameter of the launching tube in size, the collet and the piston are arranged at intervals, the power section is formed between the collet and the piston, the launching section is formed in the area between the collet and the port of the launching tube, and the balance cavity is formed in the area between the piston and the other port of the launching tube.
Furthermore, one side of the balance cavity communicated with the outside is provided with a limiting structure for resisting the liquid pushing component.
Further, the end cover is arranged at one end of the outer barrel corresponding to the opening of the launching barrel, one end of the connecting pipeline is connected with the end cover, and the other end of the connecting pipeline is connected with the closed end of the launching barrel.
Further, the launching tube and the outer tube are concentrically arranged.
Further, the launcher is an aircraft, and the power source is high-pressure gas.
Furthermore, a limiting structure for resisting the bottom support is arranged on one side of the launching port of the launching tube.
A second aspect of the present invention provides an underwater launching method, comprising:
the underwater balance launching device is configured;
filling the balancing cavity with liquid;
the bottom support is pushed by the power source to move towards one side of an outlet of the launching tube, so that the launched objects are driven to be launched out of the launching tube;
the liquid pushing component is pushed by the power source to move towards one side of the outlet of the liquid storage cavity communicated with the outside, and then recoil is counteracted.
Compared with the prior art, the invention has the following beneficial technical effects:
1. the recoil force during launching is guided to the balance cavity to push the liquid pushing component and the water body to move in the opposite direction of launching, so that the forward and backward impulse is offset to a certain degree, the recoil force during launching of the underwater launching device is reduced, the limitation of a launching platform is relieved, a vehicle with larger mass can be launched on a small and miniature platform, and the speed of discharging the vehicle is not limited too much. The platform attitude is little interfered by the launching process, and continuous launching can be better realized.
2. After the propellant is emitted from the launching tube, the bottom support and the liquid pushing component can seal the high-pressure gas after being emitted in the launching tube and the balance cavity, so that the exposure of the position of the launching platform caused by the leakage of the high-pressure gas after being emitted is avoided.
3. Because the collet seals high-pressure gas with liquid pushing component, outside rivers can't form in the launch canister and vibrate the impact in can not getting into, launch platform's transmission security and transmission noise homoenergetic can show the reduction.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
FIG. 1 is a schematic diagram of a prior art underwater launch device;
FIG. 2 is a schematic structural diagram of an underwater balanced launching device according to an embodiment of the present invention;
FIG. 3 is a schematic structural diagram of an underwater balanced launching device according to another embodiment of the present invention;
FIG. 4 is a schematic structural diagram of an underwater balanced launching device according to another embodiment of the present invention;
FIG. 5 is a schematic view of the launching principle of the underwater balanced launching device in FIG. 2;
fig. 6 is a schematic flow chart of an underwater launching method according to an embodiment of the present invention.
Detailed Description
Example embodiments will now be described more fully with reference to the accompanying drawings. Example embodiments may, however, be embodied in many different forms and should not be construed as limited to the examples set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of example embodiments to those skilled in the art.
Furthermore, the described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided to provide a thorough understanding of embodiments of the invention. One skilled in the relevant art will recognize, however, that the invention may be practiced without one or more of the specific details, or with other methods, components, devices, steps, and so forth. In other instances, well-known methods, devices, implementations or operations have not been shown or described in detail to avoid obscuring aspects of the invention.
The flow charts shown in the drawings are merely illustrative and do not necessarily include all of the contents and operations/steps, nor do they necessarily have to be performed in the order described. For example, some operations/steps may be decomposed, and some operations/steps may be combined or partially combined, so that the actual execution sequence may be changed according to the actual situation.
The underwater balance launching device comprises a launching tube, a bottom support and a balance cavity, wherein the launching tube comprises a launching section and a power section, a launcher is arranged in the launching section, a power source is arranged in the power section, the launching section and the power section are separated by the bottom support, the bottom support can slide along the launching section under the action of external force, and the power source is prevented from leaking outside the launching tube and external water flows into the launching tube; a liquid pushing component is arranged in the balance cavity and is filled with liquid, one end of the balance cavity is communicated with the power section, the other end of the balance cavity is communicated with the outside, and the liquid pushing component can move along the balance cavity under the action of external thrust; the power source pushes the bottom support to move towards the outside of the launching section, so that the launched objects are driven to be launched towards the outside of the launching barrel, meanwhile, the liquid pushing component can be pushed to move along the opposite direction, and then the recoil is offset.
The invention leads the recoil force during launching to the balance cavity to push the liquid pushing component and the water body to move in the opposite direction of launching, so that the forward and backward impulse is counteracted to a certain extent, the recoil force during launching of the underwater launching device is reduced, the limitation of a launching platform is relieved, an aircraft with larger mass can be launched on a small and miniature platform, and the speed of discharging the aircraft is not limited too much. The platform attitude is little interfered by the launching process, and continuous launching can be better realized.
Fig. 2 is a schematic structural diagram of an underwater balanced launch device according to an embodiment of the invention. As shown in fig. 2, the underwater balanced launching device comprises a launching tube 21, an outer tube 22, a bottom support 23, a piston 24 and a connecting pipeline 25, wherein one end of the launching tube 21 is open, the other end of the launching tube 21 is closed, the bottom support 23 is slidably arranged in the launching tube 21 and divides the launching tube 21 into a launching section 211 and a power section 212, a launcher to be launched is arranged in the launching section 211, and a power source capable of generating high-pressure gas is arranged in the power section 212. The inner diameter of the outer cylinder 22 is larger than the outer diameter of the launching cylinder 21, the launching cylinder 21 is sleeved in the outer cylinder 22, one end of the outer cylinder 22 is provided with an end cover 26, the other end of the outer cylinder 22 is communicated with the outside, an annular area between the launching cylinder 21 and the outer cylinder 22 forms the balance cavity 221, the balance cavity 221 is internally provided with a piston 24 in a sliding mode, and the balance cavity 221 is communicated with the power section 212 through a connecting pipeline 25. The piston 24 is an annular piston matched with the size of the annular area of the balance cavity 221, the piston 24 plays a certain supporting role on the outer cylinder 22 and can prevent the outer cylinder 22 from deforming, the end cover 26 is in an annular shape matched with the size of the annular area of the balance cavity 221, and the end cover 26 is arranged at one end of the outer cylinder 21 and is fixedly connected with the outer cylinder 22 and the launching cylinder 21 respectively so as to fix the launching cylinder 21 and the outer cylinder 22 relatively and seal one end of the balance cavity 221. The through hole connected with the connecting pipeline 25 is arranged on the closed end of the launching tube 21 and the end cover 26, one end of the connecting pipeline 25 is connected with the end cover 26 of the launching tube 21, the other end of the connecting pipeline 25 is connected with the closed end of the launching tube 21 so as to communicate the power section 212 with the balance cavity 221, high-pressure fuel gas generated by the power section 212 in the launching process can be led into the balance cavity 221 through the connecting pipeline 25, the piston 24 is driven to push the water in the balance cavity 221 to move out of the balance cavity 221, and recoil in the launching process is counteracted. The body of water within the equalizing chamber 221 can enter from the outside environment during launch, freely filling the equalizing chamber 221.
The size of the underwater balance launching device can be reduced by nesting the launching tube and the outer tube in the embodiment, the annular area between the launching tube and the outer tube serves as a balance cavity, the launching process piston can move along the balance cavity under the driving of high-pressure gas generated by the power section, so that water in the balance cavity is pushed to move outwards, the recoil of the launching process is offset, the limitation of the launching platform is removed, a vehicle with high quality can be launched on a small and miniature platform, and the speed of the vehicle leaving the tube is not limited too much. The platform attitude is little interfered by the launching process, and continuous launching can be better realized. The bottom support and the piston can also seal high-pressure gas generated in the emission process in the emission barrel and the outer barrel, so that the emission platform is prevented from being exposed due to the leakage of the high-pressure gas after emission. Because collet and piston seal high-pressure gas, outside rivers can't form in getting into the launching tube and vibrate the impact in the launching tube, and the transmission security and the transmission noise homoenergetic of launching platform can show the reduction.
Alternatively, the launch canister 21 and the outer canister 22 may be concentrically arranged.
It should be noted that in the present embodiment, the end cap 26 is disposed at one end of the outer cylinder 22 corresponding to the emission opening of the emission tube 21, so as to extend the disposed length of the connection pipeline 25, however, the present invention is not limited thereto, and the end cap 26 may be disposed at one end of the outer cylinder 22 corresponding to the closed end of the emission tube 21.
The radius of the launch canister depends on the radius r of the projectile to be launchedInner partThe radius of the launch canister is considered to be the same as the diameter of the launched object, and the cross-sectional area is
The inner diameter of the outer cylinder is rOuter coverThe outer diameter of the launch canister is RInner part. The cross-sectional area between the inner and outer cylinders is
Since the gas flow speed is high and the pressure conduction is rapid, the pressure at the bottom of the inner cylinder is considered to be the same as the pressure in the gap between the inner cylinder and the outer cylinder. When equilibrium of recoil is reached, there is psInner part＝psWorkshopI.e. sInner part＝sWorkshop. Neglecting the thickness of the inner cylinder, then rOuter cover＝rInner part. Can obtain
Namely, it is
The recoil force can be controlled within an acceptable range by adjusting the related dimension according to the actual space, and when the recoil force is within the acceptable range
Recoil is minimal.
In order to make the working principle of the underwater balanced launching device of the present embodiment more clearly understood by those skilled in the art, the launching principle of the underwater balanced launching device is described below with reference to the accompanying drawings as follows:
as shown in FIG. 5, the bottom support 23 and the piston 24 are respectively at initial positions in an initial state, when the underwater balance launching device launches, a power source of a power section in the launching tube generates high-pressure gas, the high-pressure gas continuously pushes the bottom support 23 and the piston 24 to move in the direction of an arrow, the launched objects are launched out of the launching tube, when the bottom support 23 and the piston 24 respectively move to openings of the launching tube and the outer tube, the bottom support 23 and the piston 24 are limited at the tube opening, and the high-pressure gas is sealed in the tube.
Fig. 3 is a schematic structural diagram of an underwater balanced launch device according to an embodiment of the invention. As shown in fig. 3, the underwater balanced launching device comprises a launching tube 31, an outer tube 32, a bottom support 33, a piston 34 and a connecting pipeline 35, wherein one end of the launching tube 31 is open, the other end of the launching tube 31 is closed, the bottom support 33 is slidably arranged in the launching tube 31 and divides the launching tube 31 into a launching section 311 and a power section 312, a launcher to be launched is arranged in the launching section 311, and a power source capable of generating high-pressure gas is arranged in the power section 312. The outer cylinder 32 and the launching cylinder 31 are arranged side by side and stacked on the launching cylinder 31, one end of the outer cylinder 32 is provided with an end cover 36, the other end of the outer cylinder is communicated with the outside, the balance cavity 321 is formed inside the outer cylinder 32, a piston 34 is arranged in the balance cavity 321 in a sliding mode, and the balance cavity 321 is communicated with the power section 312 through a connecting pipeline 35. The piston 34 is matched with the inner diameter of the outer cylinder 32, the piston 34 plays a certain supporting role on the outer cylinder 32 and can prevent the outer cylinder 32 from deforming, and the end cover 36 is arranged at one end of the outer cylinder 32 and is fixedly connected with the outer cylinder 32 and the launching cylinder 31 so as to fix the launching cylinder 31 and the outer cylinder 32 relatively and simultaneously seal one end of the balance cavity 321. Through holes connected with the connecting pipeline 35 are formed in the closed end of the launching tube 31 and the end cover 36, one end of the connecting pipeline 35 is connected with the end cover 36 of the launching tube 31, the other end of the connecting pipeline 35 is connected with the closed end of the launching tube 31, so that the power section 312 is communicated with the balance cavity 321, high-pressure fuel gas generated by the power section 312 in the launching process can be guided into the balance cavity 321 through the connecting pipeline 35, the piston 34 is driven to push water in the balance cavity 321 to move out of the balance cavity 321, and recoil in the launching process is counteracted. The body of water in the balance cavity 321 can enter from the external environment during launch, freely filling the balance cavity 321.
This embodiment stacks urceolus and launching tube, and the area is as balanced chamber in the urceolus, and the launching process piston can remove along balanced chamber under the drive of the high-pressure gas that the power section produced, and then promotes the water of balanced intracavity and outwards moves, offsets the recoil of launching process, has removed launching platform's restriction, also can launch the great navigation ware of quality on small-size, miniature platform, and does not carry out too much restriction to going out a section of thick bamboo speed. The platform attitude is little interfered by the launching process, and continuous launching can be better realized. The bottom support and the piston can also seal high-pressure gas generated in the emission process in the emission barrel and the outer barrel, so that the emission platform is prevented from being exposed due to the leakage of the high-pressure gas after emission. Because collet and piston seal high-pressure gas, outside rivers can't form in getting into the launching tube and vibrate the impact in the launching tube, and the transmission security and the transmission noise homoenergetic of launching platform can show the reduction.
Fig. 4 is a schematic structural diagram of an underwater balanced launch device according to an embodiment of the invention. As shown in FIG. 4, the underwater balanced launching device may also be provided with only one launching tube 41, the shoe 42 and the piston 43 are slidably disposed in the launching tube 41, the piston 43 is a piston 43 matched with the inner diameter of the launching tube 41, the shoe 42 and the piston 43 are spaced apart, the shoe 42 and the piston 43 divide the launching tube 41 into a launching section 411, a power section 412 and a balance cavity 413, the area between the shoe 42 and the launching port of the launching tube 41 is used as a launching section 411, and the launched objects are disposed in the launching section 411. The area between shoe 42 and piston 43 serves as power section 412, and a power source for generating high pressure gas is disposed in power section 412. The area between the piston 43 and the other opening of the launch barrel 41 serves as a balance chamber 413. The high-pressure gas generated by the power section 412 in the launching process can drive the piston 43 to push the water body in the balance cavity 413 to move towards the outside of the balance cavity 413, so that the recoil force in the launching process is counteracted. The body of water in the equalizing chamber 413 can enter from the external environment during launch, freely filling the equalizing chamber 413.
In the embodiment, the outer cylinder of the embodiment is omitted, the launching cylinder is lengthened and is divided into the launching section, the power section and the balance section through the bottom support and the piston, and the structure of the underwater balance launching device is simplified. The launching process piston can move along the balance cavity under the driving of high-pressure gas generated by the power section, so that water in the balance cavity is pushed to move outwards, the recoil of the launching process is counteracted, the limitation of the launching platform is removed, a vehicle with large mass can be launched on a small-sized and miniature platform, and the speed of discharging the vehicle is not limited too much. The platform attitude is little interfered by the launching process, and continuous launching can be better realized. The bottom support and the piston can also seal high-pressure gas generated in the emission process in the emission barrel and the outer barrel, so that the emission platform is prevented from being exposed due to the leakage of the high-pressure gas after emission. Because collet and piston seal high-pressure gas, outside rivers can't form in getting into the launching tube and vibrate the impact in the launching tube, and the transmission security and the transmission noise homoenergetic of launching platform can show the reduction.
Optionally, a limiting structure for resisting the liquid pushing component is arranged on one side, communicated with the outside, of the balance cavity in the above embodiment. The limiting structure can be a limiting screw or a limiting stop block arranged in the balancing cavity. This limit structure can keep out the liquid pushing component, prevents to push out the liquid component and fall out when removing to balanced chamber afterbody to the liquid pushing component is fixed a position behind balanced chamber afterbody by this limit structure, can all seal balanced chamber both ends, avoids the high-pressure gas that the emission process produced to leak from balanced chamber to the outside.
Optionally, in the above embodiment, a limiting structure for blocking the bottom support is disposed on one side of the emission opening of the emission tube. The limiting structure can be a limiting screw or a limiting stop block arranged at a launching port in the launching tube, and the height of the limiting structure cannot limit the laundries to be launched from the launching tube. This limit structure can keep out the collet, prevents that the collet from removing to the transmission mouth department of launch canister and from falling out to the collet is fixed a position in the transmission mouth department of launch canister by this limit structure, can seal the transmission mouth of launch canister, and the high-pressure gas of avoiding the emission process to produce leaks to outside and stops outside water to gush into the launch canister.
Optionally, the connection pipeline in the above embodiment may be arranged according to structural characteristics, and when the thickness of the launch canister is sufficient, the air guide hole may be directly processed in the wall of the launch canister, so that the high-pressure gas enters the gap between the launch canister and the outer canister through the air guide hole.
The projectile in the above embodiments may be an aircraft, a missile, or the like, and the power source may be high-pressure gas generated by an ignition device or high-pressure gas generated by an engine of the aircraft, which is not limited in the present invention.
As shown in fig. 6, the underwater launching method of the present invention includes the following steps:
step S600: configuring the underwater balance launching device in any one of the above embodiments;
step S610: filling the balancing cavity with liquid; the liquid may be a body of water that fills the balance cavity in an external environment.
Step S620: the bottom support is pushed by the power source to move towards one side of an outlet of the launching tube, so that the launched objects are driven to be launched out of the launching tube;
step S630: the liquid pushing component is pushed by the power source to move towards one side of the outlet of the liquid storage cavity communicated with the outside, and then recoil is counteracted.
Through the balanced type launching mode, the beneficial effects that can be brought are as follows:
1. reducing recoil during firing. By pushing outside water as a source of reverse impulse, the recoil can be close to zero in an ideal state.
In practical application, the capability of zero recoil launching in the invention can be utilized to launch an aircraft with larger mass on a small-sized and miniature platform, and the speed of the aircraft out of a cylinder is not limited too much. The platform attitude is little interfered by the launching process, and continuous launching can be better realized.
2. Reducing the emission characteristics. Through sealing the gas between the inner and outer barrels, after the launching process is finished, high-pressure gas does not leak, and the self-position exposure of the launching platform caused by the fact that the gas for launching the gas floats to the water surface is avoided.
When the stealthy requirement of transmission platform is higher, the mode of retrieving gas after traditional transmission is difficult to be gaseous recovery completely, and the gas after retrieving can cause the atmospheric pressure in the platform to increase, influences operational environment. This balanced launch structure has avoided retrieving high-pressure gas's problem.
3. The water hammer impact effect of the launch canister is avoided. Because the high-pressure gas is closed after the emission, external water flow can not enter the barrel, and oscillation impact can not be formed in the barrel. The transmission safety and the transmission noise of the platform can be obviously reduced.
Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. This application is intended to cover any variations, uses, or adaptations of the invention following, in general, the principles of the invention and including such departures from the present disclosure as come within known or customary practice within the art to which the invention pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.
It will be understood that the invention is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the invention is limited only by the appended claims.
Claims (10)
1. An underwater balance launching device is characterized by comprising a launching tube, a bottom support and a balance cavity, wherein the launching tube comprises a launching section and a power section, a launcher is arranged in the launching section, a power source is arranged in the power section, the launching section and the power section are separated by the bottom support, the bottom support can slide along the launching section under the action of external force and can prevent the power source from leaking outside the launching tube and prevent external water from flowing into the launching tube; a liquid pushing component is arranged in the balance cavity and is filled with liquid, one end of the balance cavity is communicated with the power section, the other end of the balance cavity is communicated with the outside, and the liquid pushing component can move along the balance cavity under the action of external thrust; in the launching process, the power source pushes the bottom support to move towards the outside of the launching section, so that the launched objects are driven to be launched towards the outside of the launching barrel, and meanwhile, the liquid pushing component can be driven to push liquid towards the outside of the balance cavity, and the recoil is further counteracted.
2. The underwater balanced launch device of claim 1 wherein one end of the launch canister is open and the other end of the launch canister is closed, the power section being formed between the shoe and the closed end of the launch canister; the underwater balance launching device further comprises an outer barrel and a connecting pipeline, the launching barrel is sleeved in the outer barrel, one end of the outer barrel is provided with an end cover, the other end of the outer barrel is communicated with the outside, an annular area between the launching barrel and the outer barrel forms the balance cavity, the liquid pushing component is an annular piston matched with the annular area in size, and the balance cavity is communicated with the power section through the connecting pipeline.
3. The underwater balanced launch device of claim 1 wherein one end of the launch canister is open and the other end of the launch canister is closed, the power section being formed between the shoe and the closed end of the launch canister; the underwater balance launching device further comprises an outer barrel and a connecting pipeline, the outer barrel and the launching barrel are arranged side by side, one end of the outer barrel is provided with an end cover, the other end of the outer barrel is communicated with the outside, the balance cavity is formed inside the outer barrel, the liquid pushing component is a piston matched with the inner diameter of the outer barrel, and the balance cavity is communicated with the power section through the connecting pipeline.
4. The underwater balanced launching device of claim 1, wherein the shoe and the liquid pushing component are slidably disposed in the launching tube, the liquid pushing component is a piston matched with the inner diameter of the launching tube, the shoe and the piston are spaced apart from each other and form the power section between the shoe and the piston, the area between the shoe and the port of the launching tube forms the launching section, and the area between the piston and the other port of the launching tube forms the balancing cavity.
5. The underwater balanced launch device of any one of claims 2 to 4 wherein the side of the balance cavity communicating with the outside is provided with a limit structure for resisting the liquid pushing component.
6. The underwater balanced launching device of claim 2 or 3, wherein the end cap is provided at one end of the outer cylinder corresponding to the opening of the launch canister, one end of the connection line is connected to the end cap, and the other end of the connection line is connected to the closed end of the launch canister.
7. The subsea balance launch device of claim 2, wherein said launch canister and said outer canister are concentrically disposed.
8. The underwater balance launching device of claim 1 wherein the launcher is an aircraft and the power source is a high pressure gas.
9. The underwater balanced launching device of claim 1, wherein a limiting structure for resisting against the bottom support is arranged on one side of the launching port of the launching tube.
10. An underwater launching method, comprising:
configuring the subsea launch device of any of claims 1-9;
filling the balancing cavity with liquid;
the bottom support is pushed by the power source to move towards one side of an outlet of the launching tube, so that the launched objects are driven to be launched out of the launching tube;
the liquid pushing component is pushed by the power source to move towards one side of the outlet of the liquid storage cavity communicated with the outside, and then recoil is counteracted.
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| CN202110665435.8A CN113587724A (en) | 2021-06-16 | 2021-06-16 | Underwater balance launching device and launching method thereof |
| CN202111346184.3A CN113834381A (en) | 2021-06-16 | 2021-11-15 | Underwater balance launching device and launching method thereof |
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| CN202110665435.8A CN113587724A (en) | 2021-06-16 | 2021-06-16 | Underwater balance launching device and launching method thereof |
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| CN202110665435.8A Pending CN113587724A (en) | 2021-06-16 | 2021-06-16 | Underwater balance launching device and launching method thereof |
| CN202111346184.3A Pending CN113834381A (en) | 2021-06-16 | 2021-11-15 | Underwater balance launching device and launching method thereof |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202111346184.3A Pending CN113834381A (en) | 2021-06-16 | 2021-11-15 | Underwater balance launching device and launching method thereof |
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Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2001758C3 (en) * | 1970-01-16 | 1974-03-21 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Launching device for projectiles for anti-tank fighting |
| US6286408B1 (en) * | 2000-01-04 | 2001-09-11 | The United States Of America As Represented By The Secretary Of The Navy | Energy-absorbing countermass assembly for recoilless weapons |
| US6701819B1 (en) * | 2002-08-19 | 2004-03-09 | The United States Of America As Represented By The Secretary Of The Navy | Apparatus for launching an object in a fluid environment |
| DE602005017736D1 (en) * | 2005-03-21 | 2009-12-31 | Saab Ab | Countermass and counter-mass weapon |
| CN102207358A (en) * | 2009-11-05 | 2011-10-05 | 柯兆宾 | Automatic principle of hydraulic gunlock of non-recoil gun |
| CN102141357B (en) * | 2011-01-06 | 2013-03-06 | 北京机械设备研究所 | Recoil-free ejecting device |
| JP5860956B2 (en) * | 2011-06-29 | 2016-02-16 | 北京机械▲設▼▲備▼研究所 | Pollution-free liquid balance device |
| CN107813943B (en) * | 2017-11-23 | 2023-05-23 | 航宇救生装备有限公司 | Three-stage ejection cylinder |
| CN212058476U (en) * | 2020-04-20 | 2020-12-01 | 胜洁科技股份有限公司 | Recoil regulator for airborne gas emission |
| CN111692913B (en) * | 2020-06-22 | 2022-09-06 | 中国船舶重工集团公司第七一三研究所 | Universal large-depth underwater missile launching cylinder cover structure device |
-
2021
- 2021-06-16 CN CN202110665435.8A patent/CN113587724A/en active Pending
- 2021-11-15 CN CN202111346184.3A patent/CN113834381A/en active Pending
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| CN113834381A (en) | 2021-12-24 |
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Application publication date: 20211102 |