CN205580295U - Air kinetic energy ejection orbit big gun - Google Patents
Air kinetic energy ejection orbit big gun Download PDFInfo
- Publication number
- CN205580295U CN205580295U CN201620381302.2U CN201620381302U CN205580295U CN 205580295 U CN205580295 U CN 205580295U CN 201620381302 U CN201620381302 U CN 201620381302U CN 205580295 U CN205580295 U CN 205580295U
- Authority
- CN
- China
- Prior art keywords
- air
- pressure
- blind plate
- rail
- gas receiver
- 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.)
- Active
Links
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses an air kinetic energy ejection orbit big gun, including inflating mechanism, highly -compressed air gas receiver, perhaps the vaporization is gaseous for the gas receiver provides compressed gas with highly -compressed air gas receiver intercommunication to inflate the mechanism, and the trilateral of highly -compressed air gas receiver is sealed, and blind plate cover and blind plate are installed by the port department of another side, and electromagnetic drive unit is connected to the blind plate cover, port department has still set up launches the rail, and the track cross sectional shape that launches the rail matches with the shape of blind plate makes the blind plate can do the sling movement in launching the rail under air pressure's promotion, and the exit of launching the rail is installed to barrel one end, perhaps rail and barrel launch with launching the replacement of rail barrel in port department, and the track cross sectional shape that launches the rail barrel matches with the shape of blind plate makes the blind plate can do the sling movement in launching the rail barrel under air pressure's promotion. The utility model discloses an air kinetic energy launches the big gun can provide the powerful thrust of launching, can reach and hit, the purpose of destroying promptly, and launch with low costsly.
Description
Technical field
Embodiment of the present utility model relates to the transmitting field of shell and guided missile, more specifically, this practicality is new
The embodiment of type relates to a kind of utilizing pressure-air kinetic energy to fire shells or the aerodynamic energy ejection orbit of guided missile
Big gun.
Background technology
The mode that present big gun is penetrated is launched a guided missile or last quick shell is most economical.In the U.S., one piece of battleax formula
The procurement price of cruise missile is at 1,500,000 dollars to 1,690,000 dollars, and uses electromagnetic railgun to launch one piece
The expense of guided missile only has 2.5 ten thousand dollars.But under prior art conditions, there is also following deficiency: (one) is subject to
Emission part powder charge quantitative limitation, launches a guided missile with common big gun or last quick shell, and the bullet launched is less,
The distance launched is the shortest;(2) though present state-of-the-art electromagnetic railgun, in the technology that can reach now
Under the conditions of, the warhead section weight launched also only has 22.7kg, and transmitting range is also at below 160km;(3)
Use the guided missile of prior art transmitting or last quick shell, limited with pushing away speed by the thrust that can reach, speed
Relatively low, the speed kinetic energy still difficulty being had realizes " hit and i.e. destroy " to target (particularly armored target)
Purpose.
It addition, current almost all of steel pressure vessel, monolayer material is all used to combine, and
For needing the pressure vessel of the most tens of MPa, then excessive because of required container wall thickness, weight also mistake
Weigh and practical purpose can not be reached, such as the hydrogen cylinder sold on Japanese market, be only filled with Hydrogen Vapor Pressure
14.7MPa, stores hydrogen 6m only3The hydrogen bottle of (standard state) weighs 60kg, the pressure that Chinese market is sold
Contracting natural gas bottle is filled with gas pressure and only has 20MPa, dischargeable capacity to only have the gas cylinder of 65L then to weigh 98kg,
Storing the spherical tank of compressed natural gas, when wall thickness reaches 30mm, the gas pressure that can be filled with also can only control
At below 1.6MPa.
Utility model content
This utility model overcomes the deficiencies in the prior art, it is provided that one utilizes pressure-air kinetic energy to fire shells
Or the embodiment of the aerodynamic energy ejection orbit big gun of guided missile, existing shell can be solved with expectation or guided missile is sent out
The thrust penetrated and to push away speed limited, causes launching bullet weight is low, transmitting range is short problem.
For solving above-mentioned technical problem, a kind of embodiment of the present utility model by the following technical solutions:
A kind of aerodynamic energy ejection orbit big gun, including inflation mechanism, pressure-air gas receiver, described inflator
Structure connects with pressure-air gas receiver provides compressed gas or bog, described pressure-air into gas receiver
The installation inner edge, port of the opening of gas receiver is the blind plate set of gear-like, and installing outer rim in blind plate set is tooth
The blind plate of colyliform, described blind plate set connects electromagnetic actuator device, and described electromagnetic actuator device detects that high pressure is empty
Air pressure in gas gas receiver is manipulated electromagnetic actuator device by operator after reaching preset value and drives blind plate set rotation one
Individual tooth position;The port of described opening is also provided with launching rail, launches rail section shape and the blind plate of rail
Form fit make described blind plate can make sling movement, gun tube under the promotion of air pressure in launching rail
One end is installed to launch the exit of rail, one end adjacent with launching rail on gun tube equipped with armed shell or
Guided missile;Or rail and gun tube are launched with launching the replacement of rail gun barrel in the port of described opening, launch rail gun barrel
Rail section shape make described blind plate can launch under the promotion of air pressure with the form fit of blind plate
Making sling movement in rail gun barrel, armed shell or guided missile are contained in launching rail gun barrel and act as bullet with blind plate one
Penetrate motion.
In above-mentioned aerodynamic energy ejection orbit big gun, a kind of embodiment of the present utility model is, described inflator
Structure includes liquefied air storage tank, liquefied air pump and helix tube type carburator, the liquefaction in liquefied air storage tank
Air pumps out through liquefied air pump, then by after the vaporization of helix tube type carburator, bog is imported pressure-air
In gas receiver.
In above-mentioned aerodynamic energy ejection orbit big gun, another embodiment of the present utility model is, described inflation
Mechanism includes motor and air compressor, and described motor driven air compressor is to pressure-air gas receiver
Pump into compressed air.
In above-mentioned aerodynamic energy ejection orbit big gun, described electromagnetic actuator device has pressure transducer, and pressure passes
Sensor detects the air pressure in pressure-air air accumulator and passes to electromagnetic actuator device.
In above-mentioned aerodynamic energy ejection orbit big gun, described pressure-air gas receiver is trapezoidal with many cross sections
Shape tube after being rolled into pressure-air gas storage tubular, built-up welding in the seam naturally constituted, and at shape tube
It is filled with in tube chamber than the compressed air of described pressure-air high 10% pressure of gas receiver air pressure preset value or high
The water of 20% pressure forms.
In above-mentioned aerodynamic energy ejection orbit big gun, described cross section be the caliber size of trapezoidal shape tube be the upper end
Wide 120mm, lower bottom width 122.5mm, high 120mm, shape tube wall thickness 10mm.
Compared with prior art, one of the beneficial effects of the utility model are:
(1) air volume-diminished 816 times after liquefaction, say, that the liquefied air pumped into is at abundant vapour
Can there is the carburetted air pressure of 81.6MPa after change, therefore use the air of the present utility model of liquefied air
Kinetic energy launches railgun, has the advantages that energy reserve air pressure big, available is big.
(2) the aerodynamic energy ejection orbit big gun of the present utility model that make use of pressure-air kinetic energy has powerful
Ejection propulsion, such as when blind plate diameter 1.2m, air pressure at 80MPa time, available launching pushes away
Power reaches more than 88,000,000 newton.
(3) aerodynamic energy ejection orbit big gun of the present utility model fires shells, the speed of guided missile significantly increases,
Such as under the powerful motive force of pressure-air, the ejection speed of its blind plate is up to 3~300,000 meter per seconds, such as
The lower guided missile launched of promotion of this blind plate ejection speed at a high speed or shell, it goes out thorax speed can be more than 30,000
Meter per second (100 Mach), is the decades of times of general shell, missile velocity, this ultrahigh speed kinetic energy shell or lead
Bullet, lethality is strong, can reach the purpose of " hit and i.e. destroy ", also can do with general chemistry energy guided missile or armor-piercing bullet
Be difficult to tackle puts on a suit of armour reactive armor and active defense armor system.
(4) launch cost of aerodynamic energy ejection orbit big gun of the present utility model is low, for example with this practicality
Novel aerodynamic energy ejection orbit big gun launch the guided missile of a bullet weight 80kg or last quick shell to 1000km with
During upper target, air consumption only has about 2000m3, air-fluidized power consumption only has about 500kW h, launch cost
The 1%~3% of only general chemical energy guided missile.
(5) compare with the pressure vessel of the same pressure rating of prior art manufacture, use shape tube to make
Pressure-air gas receiver, its wall thickness and corresponding weight can reduce (gently) 50%~80%, fill in tube chamber
After entering compressed air or water, grade that it is pressure also can improve 15%~30%, uses the gas receiver that shape tube makes
Having the advantage that pressure rating stored under equal converting thickness is high, its storage pressure and storage capacity can
Reach 10 times of Ordinary Compression Natural Gas Spherical.
Accompanying drawing explanation
Fig. 1 shows the structural representation of the aerodynamic energy ejection orbit big gun of this utility model embodiment 1.
What Fig. 2 showed the aerodynamic energy ejection orbit big gun of this utility model embodiment 1 launches rail structural representation
Figure.
Fig. 3 shows the structural representation of the aerodynamic energy ejection orbit big gun of embodiment 2 of the present utility model.
Fig. 4 shows the blind plate set planar structure schematic diagram of aerodynamic energy ejection orbit big gun of the present utility model.
Fig. 5 shows the blind plate set cross-sectional view of aerodynamic energy ejection orbit big gun of the present utility model.
Fig. 6 shows the blind plate planar structure schematic diagram of aerodynamic energy ejection orbit big gun of the present utility model.
Fig. 7 shows the blind plate cross-sectional view of aerodynamic energy ejection orbit big gun of the present utility model.
Fig. 8 shows launching rail or launching rail gun barrel of aerodynamic energy ejection orbit big gun of the present utility model
Cross-sectional view.
Fig. 9 shows that the cross section of the pressure-air gas receiver of aerodynamic energy ejection orbit big gun of the present utility model shows
It is intended to.
Figure 10 is the partial enlarged drawing of Fig. 9.
In figure, 1-liquefied air storage tank, 2-liquefied air pump, 3-helix tube type carburator, 4-pressure-air stores up
Inflator, 5-electromagnetic actuator device, 6-blind plate set, 7-blind plate, 8-launches rail, 9-shell/guided missile, 10-gun tube,
11-launches rail gun barrel, 12-electromotor, 13-air compressor, and 1001-cross section is trapezoidal shape tube, 1002-
Shape tube tube wall, 1003-shape tube tube chamber, the seam naturally constituted between 1004-shape tube.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with enforcement
Example, is further elaborated to this utility model.Should be appreciated that specific embodiment described herein
Only in order to explain this utility model, it is not used to limit this utility model.
Embodiment 1
Such as Fig. 1, shown in 4~10, the aerodynamic energy ejection orbit big gun of the present embodiment includes inflation mechanism, high pressure
Air gas receiver 4, described inflation mechanism connects with pressure-air gas receiver 4 provides bog into gas receiver.
Described inflation mechanism includes liquefied air storage tank 1, liquefied air pump 2 and helix tube type carburator 3, liquefied air
Liquefied air in storage tank pumps out through liquefied air pump, then by helix tube type carburator vaporize after by bog
Import in pressure-air gas receiver.The installation inner edge, port of the opening of described pressure-air gas receiver is tooth
The blind plate set 6 of colyliform, installs the blind plate 7 that outer rim is gear-like in blind plate set, described blind plate set 6 is connected to fix
Electromagnetic actuator device 5 on pressure-air gas receiver 4.Air pressure in described pressure-air gas receiver 4 reaches pre-
If can be needed to manipulate electromagnetic actuator device 5 by operator after value to drive one tooth position of blind plate set 6 rotation;Described height
The port of pressure air gas receiver 4 opening is also provided with launching rail 8, launches the rail section shape of rail 8 with blind
The form fit of plate 7 makes described blind plate 7 can make sling movement in launching rail under the promotion of air pressure,
Gun tube 10 one end is installed to launch the exit of rail, and one end adjacent with launching rail on gun tube is equipped with armed
Shell or guided missile 9.
The pressure-air gas receiver of the present embodiment is to be that trapezoidal shape tube 1001 is through being rolled into storage with many cross sections
After inflator shape, built-up welding in the seam 1004 naturally constituted between shape tube, and be filled with in the tube chamber of shape tube
Form than the compressed air of described high 10% pressure of gas receiver air pressure preset value.Cross section is trapezoidal shape tube tube chamber
The size (caliber size) of 1003 is upper bottom width 120mm, lower bottom width 122.5mm, high 120mm, special-shaped
The wall thickness of tube wall 1002 is 10mm.
The transmitting flow process of the aerodynamic energy ejection orbit big gun of the present embodiment is:
First blind plate 7 is placed in blind plate set 6, and is driven blind plate set 6 one tooth of motion by electromagnetic actuator device 5
Clamping blind plate 7 after Wei, now the gear of blind plate 7 is one to one with the gear of blind plate set 6, makes blind plate 7 not
Sling movement can be made in launching rail 8.Liquefied air in liquefied air storage tank 1 is by liquefied air pump 2 pump
Go out and after helix tube type carburator 3 vaporizes, enter pressure-air gas receiver 4, in pressure-air gas receiver 4
After carburetted air pressure reaches desirable pressure, electromagnetic actuator device 5 can be manipulated as required by operator and drive blind
Sleeve-board 6 moves a tooth position (positive movement or adverse movement), now the tooth of the gear of blind plate 7 and blind plate set 6
Wheel breach one_to_one corresponding, blind plate 7 launches shock shell or guided missile 9 under the promotion of air pressure, shell or lead
Under blind plate 7 clashes into the promotion of kinetic energy, rail 8 is launched on edge to bullet 9 and gun tube 10 is launched.
Embodiment 2
As in figure 2 it is shown, as different from Example 1, the aerodynamic energy ejection orbit big gun of the present embodiment is with launching
Rail gun barrel 11 is replaced and is launched rail 8 and gun tube 10, launches the rail section shape of rail gun barrel 11 and the shape of blind plate 7
Coupling makes described blind plate 7 can make sling movement in launching rail gun barrel under the promotion of air pressure, to be launched
Shell or guided missile 9 be contained in launch and act as sling movement, and bullet (throwing) at gun muzzle with blind plate one in rail gun barrel
Penetrate transmitting;It addition, the pressure-air gas receiver of the present embodiment is to be that trapezoidal shape tube is through roller with many cross sections
After being pressed into gas storage tubular, built-up welding in the seam naturally constituted, and be filled with than described storage in the tube chamber of shape tube
The water of high 20% pressure of inflator air pressure preset value forms.In addition to the above-mentioned structure different from embodiment 1, other
Structure is same as in Example 1.
Embodiment 3
As it is shown on figure 3, as different from Example 1, the inflation of the aerodynamic energy ejection orbit big gun of the present embodiment
Mechanism includes motor 12 and air compressor 13, and motor 12 drives air compressor 13 to store up to pressure-air
Inflator 4 pumps into compressed air.In addition to the above-mentioned structure different from embodiment 1, other structure and embodiment 1 phase
With.
The transmitting flow process of the aerodynamic energy ejection orbit big gun of the present embodiment is:
First blind plate 7 is placed in blind plate set 6, and is driven blind plate set 6 one tooth of motion by electromagnetic actuator device 5
Clamping blind plate 7 after Wei, now the gear of blind plate 7 is one to one with the gear of blind plate set 6, makes blind plate 7 not
Sling movement can be made in launching rail 8.Air pressure in pressure-air gas receiver 4 is driven at motor 12
After engine-driven air compressor 13 reaches desirable pressure, electromagnetic actuator device 5 can be manipulated as required by operator and drive
One tooth position of blind plate set 6 motion, now the gear of blind plate 7 and blind plate overlap the notch gear one_to_one corresponding of 6, blind plate
7 launch under the promotion of air pressure shock shell or guided missile 9, shell or guided missile 9 clash into kinetic energy at blind plate 7
Promote lower edge to launch rail 8 and gun tube 10 is launched.
This utility model is described by explanatory embodiment the most of the present utility model, but,
It should be understood that those skilled in the art can be designed that a lot of other amendments and embodiment, these amendments
To fall within spirit disclosed in the present application and spirit with embodiment.More specifically, in the application
In scope of disclosure, the building block of theme composite configuration and/or layout can be carried out multiple modification and improvement.
Except modification that building block and/or layout are carried out with in addition to improving, to those skilled in the art, its
His purposes also will be apparent from.
Claims (6)
1. an aerodynamic energy ejection orbit big gun, it is characterised in that include inflation mechanism, pressure-air gas receiver (4),
Described inflation mechanism connects with pressure-air gas receiver (4) provides compressed gas into pressure-air gas receiver
Or bog, the installation inner edge, port of the opening of described pressure-air gas receiver is gear-like
Blind plate set (6), installing outer rim in blind plate set is the blind plate (7) of gear-like, described blind plate set (6)
Connecting electromagnetic actuator device (5), described electromagnetic actuator device (5) detects pressure-air gas receiver (4)
In air pressure reach preset value after by operator manipulate electromagnetic actuator device drive blind plate set rotate a tooth
Position;The port of described opening is also provided with launching rail (8), launches the rail section shape of rail (8)
The form fit of shape and blind plate (7) makes the described blind plate (7) can be at bullet under the promotion of air pressure
Making sling movement in penetrating rail, gun tube (10) one end is installed to launch the exit of rail, with bullet on gun tube
Penetrate the adjacent one end of rail equipped with armed shell or guided missile (9);Or the port of described opening
Launch rail (8) and gun tube (10) with launching rail gun barrel (11) replacement, launch rail gun barrel (11)
Rail section shape makes described blind plate (7) in the promotion of air pressure with the form fit of blind plate (7)
Under can make sling movement, armed shell or guided missile (9) in launching rail gun barrel and be contained in and launch rail
Sling movement is acted as with blind plate one in gun barrel.
Aerodynamic energy ejection orbit big gun the most according to claim 1, it is characterised in that described inflation mechanism bag
Include liquefied air storage tank (1), liquefied air pump (2) and helix tube type carburator (3), liquefied air
Liquefied air in storage tank pumps out through liquefied air pump, then will be vaporized by after the vaporization of helix tube type carburator
Gas imports in pressure-air gas receiver.
Aerodynamic energy ejection orbit big gun the most according to claim 1, it is characterised in that described inflation mechanism bag
Including motor (12) and air compressor (13), described motor driven air compressor is empty to high pressure
Gas gas receiver pumps into compressed air.
Aerodynamic energy ejection orbit big gun the most according to claim 1, it is characterised in that described Electromagnetic Drive fills
Putting (5) and have pressure transducer, pressure transducer detects the air pressure in pressure-air air accumulator and transmits
To electromagnetic actuator device.
Aerodynamic energy ejection orbit big gun the most according to claim 1, it is characterised in that described pressure-air stores up
Inflator be with many cross sections be trapezoidal shape tube after being rolled into pressure-air gas storage tubular, at nature
Built-up welding in the seam constituted, and it is filled with more pre-than described pressure-air gas receiver air pressure in the tube chamber of shape tube
If the water of the compressed air or high 20% pressure that are worth high 10% pressure forms.
Aerodynamic energy ejection orbit big gun the most according to claim 5, it is characterised in that described cross section is trapezoidal
The caliber size of shape tube be upper bottom width 120mm, lower bottom width 122.5mm, high 120mm, shape tube
Wall thickness 10mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620381302.2U CN205580295U (en) | 2016-04-29 | 2016-04-29 | Air kinetic energy ejection orbit big gun |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620381302.2U CN205580295U (en) | 2016-04-29 | 2016-04-29 | Air kinetic energy ejection orbit big gun |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205580295U true CN205580295U (en) | 2016-09-14 |
Family
ID=56858862
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201620381302.2U Active CN205580295U (en) | 2016-04-29 | 2016-04-29 | Air kinetic energy ejection orbit big gun |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205580295U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105783588A (en) * | 2016-04-29 | 2016-07-20 | 杨文清 | Air kinetic energy ejection rail gun |
-
2016
- 2016-04-29 CN CN201620381302.2U patent/CN205580295U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105783588A (en) * | 2016-04-29 | 2016-07-20 | 杨文清 | Air kinetic energy ejection rail gun |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7337774B2 (en) | Projectile firing device using liquified gas propellant | |
US8201486B1 (en) | Two-stage light gas gun | |
US4096804A (en) | Plastic/mischmetal incendiary projectile | |
US9470499B2 (en) | Explosive disruption container | |
CN205580295U (en) | Air kinetic energy ejection orbit big gun | |
CN105947229A (en) | Air kinetic energy ejection launcher for spacecraft | |
CN105783588A (en) | Air kinetic energy ejection rail gun | |
US6789454B2 (en) | Gun barrel for launching large projectiles | |
US11359895B2 (en) | Supercharged accelerating projectile fired in a flight trajectory towards a target | |
CN203869588U (en) | High initial velocity projectile launching device | |
CN1800769A (en) | Spiral pipe emission mechanism | |
CN205837227U (en) | A kind of aerodynamic energy airborne vehicle catapult-launching gear | |
CN206281410U (en) | One kind is without shell case sniper rifle | |
CN203657606U (en) | Liquid nitrogen icebound system for explosive device | |
US10302402B2 (en) | Munitions with increased initial velocity projectile | |
CN101435684A (en) | Defense missile | |
CN105698001B (en) | A kind of aerodynamic energy aircraft catapult-launching gear | |
US5271330A (en) | Oxygen enhanced cruise missile weapon system | |
CN103047909A (en) | Method for improving initial speed of bullets and shells | |
CN105333769A (en) | Portable type spring throwing device | |
WO2003056272A1 (en) | Traumatic cartridge and traumatic element for a barrelless weapon | |
AU2002336805B2 (en) | Projectile firing device using liquified gas propellant | |
CN107300340A (en) | 400 kilometers of range artilleries | |
CN201173746Y (en) | Training exercise target bomb for counteracting parachute descent and its emission device | |
CN1664488A (en) | Equivalent armor protection by vertical momentum |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |