CN101013017A - Troops and munitions battlefield rapid transportation system device - Google Patents
Troops and munitions battlefield rapid transportation system device Download PDFInfo
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- CN101013017A CN101013017A CN 200510132498 CN200510132498A CN101013017A CN 101013017 A CN101013017 A CN 101013017A CN 200510132498 CN200510132498 CN 200510132498 CN 200510132498 A CN200510132498 A CN 200510132498A CN 101013017 A CN101013017 A CN 101013017A
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Abstract
The invention discloses a device for transmitting force and military supplies into target field quickly, comprising an emitting system with carrier multiple rocket, a rocket injector, a rocket engine at the back of rocket injector, and 1-3 cobble solder chamber at the front of rocket injector, wherein, each chamber can hold one armed solder with parachute. The bottom of chamber is mounted with an ejecting rocket similar like the injecting seat of fighter. The front taper frame of chamber is mounted with a power supply and a program-controlled computer chip for automatic igniting the ejecting rocket above the target to eject out the chamber and the armed solder outside the main body of rocket injector, and the chamber will be separated from the solder, and automatically open the parachute. The invention can avoid runway of plane and transmit solders to target quickly.
Description
Technical field
The present invention relates to the quick delivery system device of battlefield troops of military field, particularly relate to a kind of rocket vehicle that troops are dropped in the battlefield fast that is used for.
The invention still further relates to this rocket vehicle is used for dropping fast under the condition of battlefield small arms equipment and military material.
Background technology
Rocket is a kind of reaction propelled aerial, spacecraft that utilizes, and its instantaneous burst power is strong, and speed is fast, can take off vertically, and does not need the airfield runway of aircraft utilization, is a kind of aerial efficiently, space carrier vehicle; Yet, because rocket is disposable use mostly, the cost height, fuel used value costliness, cost effectiveness is far below jet plane.So, only be applied to aviation at present, navigate greatly and the various precision guidance missiles of military field.
According to the interrelated data introduction of internet, the U.S. once had the human rocket to do delivering mail test fast, and the result is also undesirable, and is not dropped into practical.Because rocket is subjected to all multifactor restrictions, rocket also of no use is so far done the precedent that common transporter aircraft uses.
Vehicle-mounted multibarrel launcher also is a kind of rocket-powered shell, and its emission rate is fast, penetrates apart from far away, and power is big, and is vehicle-mounted emission system, but the fast reserve emission is simple in structure because of it, cheap, and is generally equipped by all armies in the world.
Recognize from the relevant military webpage of internet, the development and production of China river boat parent company a kind of super-range rocket big gun WS-2 type, be bore maximum in the world at present, range rocket gun farthest; Its diameter reaches 406mm, penetrates highly 60 kilometers, and initial velocity 50m/ second, 5.6 Mach of flying speeds are penetrated apart from 360 kilometers, the long 7.15m of bullet, and 1275 kilograms of complete round weights, bullet weigh 200 kilograms, and the ratio that bullet accounts for complete round weight is generally 21.2% to 37.5%.
The general initial velocity of artillery rocket only is equivalent to up to a hundred kilometers automobile speed per hour second at 30-50m/, penetrate high below 60 kilometers, a little more than the stratospheric top dead centre of earth atmosphere, 300 to 1000m/ seconds of normal flight speed.Because artillery rocket is the shell that promotes flight with rocket, its launch velocity, acceleration, flying height, flying speed, penetrate distance, diameter, weight, volume etc., all can manufacture and design according to actual needs.
Summary of the invention
An object of the present invention is to provide that a kind of airbound target is little under condition of battlefield, speed is fast, and difficult interception do not need the airfield runway of aircraft, but fast reserve all can be dropped the disposable rocket vehicle of troops whenever and wherever possible.
Another object of the present invention is under condition of battlefield this rocket vehicle to be used for delivering fast small arms to equip and military material.
The objective of the invention is to deliver fast that troops and military material system and device realize, comprising: vehicle-mounted emission system and rocket Casting device by a kind of battlefield with following structure; Described vehicle-mounted emission system is a kind of vehicle-mounted multibarrel launcher emission system, and several transmitting tubes are secured together the formation launcher, and on the chassis that installs to the carrier car, launch data caliberating device and emission igniter all are installed in the driver's cabin.Described rocket Casting device is a device that is similar to artillery rocket, and the rear portion of body is a cylindrical shape, and by rocket engine, fuel compartment and stable vane are housed, the diameter of this part, length can increase and decrease according to the distance of penetrating distance.
The body portion of rocket Casting device is the irregular cylindrical shape of diameter 600mm, length 2.5m to 3m, it is interior by adorning 13 avette manned capsule of goose at the most. and the longitudinal length of this manned capsule is 680mm, transverse width is 560mm, highly be 900mm, because the anterior body diameter of rocket Casting device has only 600mm, must protrude 150mm downwards by the corresponding bottom of dress manned capsule at this body, with manned capsule when installing to the correspondence position of rocket Casting device body, hatchcover part palpus this body 150mm protruding upward of manned capsule, it highly just can reach 900mm up and down like this, can hold one and bear parachute, helmet, earplug, the fully armed soldier of anti-high wind face shield and oxygen unit squats.
In the space that the bottom of this manned capsule raises up by shooting the ejection-rocket of penetrating manned capsule.In the cone-shaped hood of described rocket Casting device front, power supply and microcomputer chip are housed, be used for program control rocket Casting device and launch the flight time through accurate Calculation, after arriving the predeterminated target sky, automatically light the ejection-rocket of manned capsule bottom, with manned capsule and take the soldier and launch out rocket Casting device body together, then, manned capsule separates automatically with the soldier, and automatic deployment drops to ground with the soldier.
Described manned capsule, form by hatchcover and two semicircle cabin bodies, when installing to the corresponding position of rocket Casting device body, 4 bar shaped guide rails that vertically are equally spaced with the manned capsule outer surface, broadcast in interior corresponding 4 the U-shaped guide-track grooves of rocket Casting device body, bottom at 4 bar shaped guide rails, be provided with fixedly jump ring of manned capsule, be provided with the fixedly jump ring groove of U-shaped guide-track groove in 4 U-shaped guide-track grooves and the position that fixedly jump ring is corresponding, be used for manned capsule is fixed in the body of rocket Casting device, when ejection-rocket launches manned capsule, rely on of 4 the fixedly jump ring destructions of the powerful thrust of ejection-rocket with manned capsule, free fixingly, make manned capsule successfully launch out the body of rocket Casting device.
Described manned capsule hatchcover, if when adorning a manned capsule, be a little circular arc, if when adorning three manned capsules, then form a great circle arc by three separate hatchcovers, corresponding both sides, the below of each hatchcover are provided with two lock pins that protrude downwards, are provided with lockhole at the manned capsule cabin of two compositions body by corresponding both sides, seam place, lock pin inserts lockhole, hatchcover is fixed on the cabin body of manned capsule.
Described manned capsule ejection-rocket be a kind of fighter plane launch seat the ejection-rocket that generally adopts, be installed in the manned capsule bottom outside from bottom to top in the space of projection.
Described manned capsule is when installing in the rocket Casting device body, and manned capsule seals, but and on hatchcover, leave the ventilating opening of taking soldier's switch, the cabin body adopts the light material manufacturing of thermal insulating, sound insulation and vibration damping impact resistance.
The transmitting tube of described vehicle-mounted multibarrel launcher emission system, its diameter, length and shape should be suitable with diameter, length and the outer shape of described rocket Casting device.
In order to realize under the condition of battlefield, be used for delivering fast small arms equipment and military material, the present invention becomes cargo hold with the partial reequipping of rocket Casting device manned capsule, the front portion that is about to be used to penetrate the rocket Casting device of throwing troops is repacked a long 2.5m to 3m into, the cylindrical shape cargo hold of diameter 600mm, military material to tens that can disposable air-drop hundreds of kilogram weight is to the hundreds of kilometer, preceding cone-shaped hood as this cargo hold hatchcover, suit is to the forehatch of cargo hold, with a threaded drift bolt that connects holdhatch and be sleeved on the preceding taper bell-type hatchcover two ends of cargo hatch, this hatchcover is fixed on the cargo hold, and at the interface of the fuel compartment of cargo hold and rocket engine, add the blasting charge separator, after the rocket Casting device is launched into the target sky,, cargo hold is partly exploded with rocket engine separate by the program control igniter explosive blasting of microcomputer chip separator, the free falling of rocket engine part, the cargo hold part is opened the built-in ground that bales out automatically.
Battlefield of the present invention is delivered troops and military material system and device fast, compare with airborne troops of air force, has suitable advantage, because of the present invention is vehicle-mounted emission system, maneuverability, rocket Casting device single target is little, and flying speed is fast, difficult interception, penetration ability is strong, do not need airfield runway, whenever and wherever possible all can be remote, extensive troops and the military material delivered, particularly cost is low, the value that only is higher than one piece of heavy rocket shell, and deliver troops and military material simply rapid, do not need to escort and collaborative in many ways, can finish the delivery task separately; Particularly can give full play to the advantage of my powerful ground force, play land battle, close combat with the enemy, point-blank encounter makes the enemy be difficult to bring into play the advantage of its high-tech and mechanization heavy equipment, and war is made short work of, and few destruction bled less.The present invention can be used for major war, campaign and local war, also can be used for the scout, the tactical assault operation of special technical soldier, troops reinforce fast for the battlefield, tackling multinomial military operation such as shallow bid arms terrorist all is the optimal selection and the sharp weapon of winning victory, and for air-drop troops of my army have increased new means again, for my army has increased a parachutist's of ground force new branch of the armed forces again, for the logistics support of my army has increased the guarantee means of air-drop fast again.
Below in conjunction with accompanying drawing and example the present invention is described in further detail.
Fig. 1 is a vehicle-mounted emission system side view of the present invention.
Fig. 2 is the side view that the present invention is used for delivering fast the rocket Casting device of troops.
Fig. 3 is the cutaway view of rocket Casting device shown in Figure 2.
Fig. 4 is the manned capsule perspective view of rocket Casting device shown in Figure 3.
Fig. 5 is the cutaway view of the guide-track groove binding site of manned capsule guide rail shown in Figure 4 and body.
Fig. 6 is the cutaway view that the present invention is used for delivering fast the rocket Casting device of military material.
What Fig. 1 was extremely shown in Figure 5 is the system and device that troops are delivered in battlefield of the present invention fast, vehicle-mounted emission system is a kind of rocket gun emission system, launcher 2 is to be secured together with many cylindrical shape transmitting tubes, on the chassis that installs to carrier car 1, launch data caliberating device 3 and emission igniter 4 all are installed in the driver's cabin.Certainly, launcher 2 also can adopt guide tracked or box launcher.
It is devices that are similar to artillery rocket that rocket is thrown device 5, its rear body is a cylindrical shape, by rocket engine 6 and fuel compartment 7 are housed, and on the corresponding both sides of fuel compartment 7 by adorning two stable vanes 30, to guarantee rocket Casting device 5 low speed rotation unlike artillery rocket awing; This section diameter, length can increase and decrease according to the distance of transmitting range.The body portion of rocket Casting device 5 is the irregular cylindrical shapes of diameter 600mm, length 2.5m to 3m, and by adorning 13 avette manned capsule 8 of goose at the most, the longitudinal length of manned capsule 8 is 680mm in it, transverse width 560mm, height 900mm; Because the body portion diameter of rocket Casting device 5 has only 600mm, must protrude 150mm downwards by the corresponding bottom of dress manned capsule 8 at this body, with manned capsule 8 when installing to the body correspondence position of rocket Casting device 5, hatchcover 13 parts palpus this body 150mm protruding upward of manned capsule 8, it highly could cross 900mm up and down like this, can hold one and bear parachute 15, helmet 32, earplug 35, the fully armed upward soldier of anti-high wind face shield 24 and oxygen unit 20 squats, the bottom outside of manned capsule 8 from bottom to top the projection the space in penetrate rocket 12 by shooting, this ejection-rocket 12, be present fighter plane driver, run into the ejection-rocket that launches seat of emergency life-saving, according to the data introduction, can under the situation of 1500 kilometers of zero to 5000m height speed per hours, driver safety be launched outside the deliver from vault.
Manned capsule 8 is made up of hatchcover 13 and two equal semicircle cabin bodies, when installing to the corresponding position of rocket Casting device 5 bodies, the 4 bar shaped guide rails 17 that are equally spaced by manned capsule 8 outer surfaces insert in the body of rocket Casting devices 5 in corresponding 4 U-shaped guide-track grooves 16, be provided with the fixedly jump ring 18 of manned capsule 8 in the latter half of every bar shaped guide rail 17, in the latter half of U-shaped guide-track groove 16 and the fixing corresponding position of jump ring, be provided with the jump ring groove 19 of U-shaped guide-track groove 16, be used for manned capsule 8 is fixed in the body of rocket Casting device 5, when preventing that ejection-rocket 12 from launching manned capsule 8, because of the center of gravity of high-speed flight or manned capsule 8 is unbalance manned capsule 8 is stuck in the body of rocket Casting device 5; When ejection-rocket 12 launches manned capsule 8, rely on the powerful thrust of ejection-rocket 12, can be easily with 4 of manned capsule 8 fixedly jump ring destroy, free fixingly, make manned capsule 8 can successfully launch out the body of rocket Casting device 5.And be connected with micro computer programmed chip 10, microcomputer program setting device 11 and ejection-rocket 12 with cable, be used for the igniting in good time of program control ejection-rocket 12 and launch manned capsule 8.
The hatchcover 13 of manned capsule 8, if by adorning a manned capsule 8 then hatchcover 13 is a little circular arc, if by adorning 3 cabins, then by 3 difference independently hatchcover 13 form a great circle arc, so that reduce air drag and keep the stability of flight, and be provided with the ventilating opening 23 that can supply to take soldier's switch in the front upper place of hatchcover 13; The lock pin 14 of two hatchcovers 13 is stretched out on corresponding both sides below the hatchcover 13 of manned capsule 8, and at the cabin of two semicircle manned capsules 8 body seam crossing, corresponding both sides are provided with lockhole 31, in the lock pin 14 insertion cabin body lockholes 31 with hatchcover 13, hatchcover 13 is fixed on the manned capsule 8.
Fig. 6 shows another embodiment that troops' military material system and device is delivered in battlefield of the present invention fast, remove the manned capsule in first embodiment 8 is repacked into outside the cargo hold 25, installed the parachute 27 of explosive separator 26 and cargo hold 25 additional, fixedly jump ring 29 and cargo hatchcover fixture, other parts all are the same.
Under condition of battlefield, be used to realize deliver fast small arms equipment and military material, the present invention becomes cylindrical shape cargo hold 25 with manned capsule 8 partial reequippings of rocket Casting device 5, preceding cone-shaped hood 21 as these cargo hold 25 hatchcovers, suit is to the hatch 34 of cargo hold 25, hatch 34 and the threaded drift bolt 32 that is sleeved on taper bell-type hatchcover 21 two ends of cargo hold 25 hatch 34 with a perforation cargo hold 25, taper bell-type hatchcover 21 is fixed on the cargo hold 25, and at connecting port 28 places of cargo hold 25 with the fuel compartment 7 of rocket engine 6, add blasting charge separator 26 and fixing jump ring 29, after treating that rocket is penetrated a device 5 arrival target sky, by micro computer programmed ignition device, two parts blast is separated, rocket engine 6 and fuel compartment 7 part free fallings, the cargo hold part is opened the built-in ground that bales out automatically.
When battlefield of the present invention is delivered troops and the emission of military material system and device fast, earlier by being installed in the launch data caliberating device 3 in the driver's cabin, the launch data of launcher 2 is demarcated in operation, take the soldier simultaneously and worn the helmet 32, earplug 35, anti-high wind face shield 24, oxygen unit 20, bear parachute 15 and carry the small arms equipment, enter the manned capsule 8 of rocket Casting device 5, build hatchcover 13, set the program of micro computer 10 by microcomputer program setting device 11 by operating personnel, load the into transmitting tube of launcher 2 by automatic loading mechanism again, by the emission igniter 4 igniting emissions that are installed in the driver's cabin, start the program that ejection-rocket 12 is lighted in the timing of micro computer 10 simultaneously, after arriving the overhead height in good time of target, automatically light ejection-rocket 12, with manned capsule 8 with take the body that the soldier together launches out rocket Casting device 5, because the cabin body of manned capsule 8 is formed by two, no longer include any constraint after launching out the body of rocket Casting device 5, automatically with take the soldier and separate, the fixedly lock pin 14 of hatchcover 13 is just in time at the cabin of two compositions body seam crossing, after the cabin body separates, hatchcover 13 also separates automatically, bear hatchcover 13 that the ripcord 22 of parachute 15 link to each other with the soldier this moment, because of high wind blows and takes the soldier and separate and spur ripcord 22, the parachute 15 that the soldier is born is opened automatically, and simultaneously the ripcord that links to each other with soldier's parachute 15 of hatchcover 13 22 is broken by high wind.
The emission process of another embodiment of the invention is that the part of manned capsule 8 is different with first, is about to put into military materials in the cargo hold 25, and the other parts operation is identical.
Rocket Casting device of the present invention, behind its launch velocity, acceleration, flying height, flying speed, the arrival target sky, flying speed when ejection-rocket launches manned capsule and height, and rocket Casting device entire length and rear portion diameter length etc. all can be penetrated distance and actual needs and the specialized designs manufacturing according to different, its basic principle is the launch velocity of rocket Casting device, acceleration, flying height, flying speed, ejection speed etc. all must remain on to be taken in the limit range that soldier's life can bear.
Rocket Casting device of the present invention, owing to be to deliver troops and military material, the dispersal point error of landing can not influence the delivery effect a little louder yet, needn't be accurate as shell and guided missile, therefore do not need the precise guidance device, so not only production technology is simple, also greatly reduces cost.
For the rocket Casting device that the present invention is used to deliver troops safer reliable when ejection-rocket launches manned capsule, can in the preceding cone-shaped hood of rocket Casting device, install laser ranging system additional, and be connected with microcomputer chip, when land earthward in the rocket Casting device arrival target sky, before after laser ranging system in the cone-shaped hood leads direction and detects suitable distance earthward along bullet, start ejection-rocket automatically.Also can adopt and on first manned capsule, install the device that visual and manual ignition launches manned capsule additional.But, no matter be that class is improved,, all should be considered as in protection scope of the present invention so long as add ejection-rocket and the form air-drop troops and the military material of the separate type cargo hold that explodes with the formula manned capsule of firing a rocket.
Claims (6)
1, troops' system and device is delivered in a kind of battlefield fast, comprise: vehicle-mounted emission system and rocket Casting device, it is characterized in that: described vehicle-mounted emission system is a kind of multibarrel launcher emitter, the profile of the transmitting tube of its launcher 2 and described rocket Casting device 5, diameter, length are suitable, the rear body of described rocket Casting device 5 is cylindrical shapes, by dress rocket engine 6 and fuel compartment 7, and on the corresponding both sides of fuel compartment 7 by adorning two stable vanes 30; The front portion of described rocket Casting device 5 is the irregular cylindrical shapes of diameter 600mm, length 2.5m to 3m, it is interior by adorning 13 avette manned capsule 8 of goose at the most, in the space that the bottom of this manned capsule 8 raises up by shooting the ejection-rocket 12 of penetrating manned capsule 8, in the cone-shaped hood of rocket Casting device 5 fronts, press dress power supply 9 and microcomputer chip 10, and be connected with ejection-rocket 12 with microcomputer chip 10 with power supply.
2, deliver troops' system and device fast according to claim 1 described battlefield, it is characterized in that: described manned capsule 8 is made up of two semicircles that equate or hatchcover 13.
3, deliver troops' system and device fast according to claim 2 described battlefields, it is characterized in that: if described hatchcover 13 rocket Casting devices 5 are when adorning a manned capsule 8, hatchcover 13 is a little circular arc, if when adorning 3 manned capsules 8, then form a great circle arc by 3 hatchcovers 13, each independently below the hatchcover 13 symmetrical both sides be provided with two lock pins 14, be provided with lockhole 31 on the corresponding both sides of body upper end, the cabin seam crossing of the manned capsule 8 of two compositions.
4, deliver troops' system and device fast according to claim 1 or 2 described battlefields, it is characterized in that: the external surface peripheral at described manned capsule 8 is uniform-distribution with 4 bar shaped guide rails 17, is provided with the fixedly jump ring 18 of 4 manned capsules 8 in the bottom of 4 guide rails 17; In the body of rocket Casting device 5, be provided with 4 U-shaped guide-track grooves 16 with the correspondence position of guide rail 17 by dress manned capsule 8, be provided with the jump ring groove 19 of 4 guide-track grooves 16 at the correspondence position of the jump ring 18 of the manned capsule 8 of the bottom of guide-track groove 16 and guide rail 17.
5, deliver troops' system and device fast according to claim 1 or 2 described battlefields, it is characterized in that: the soldier who takes in the described manned capsule 8 bears parachute 15, wears the helmet 32, earplug 35, anti-high wind face shield 24, oxygen unit 20.
6, a kind ofly troops' system and device is delivered in claim 1 to 5 described battlefield fast be modified into and be used for the system and device that military material is delivered in the battlefield fast, it is characterized in that: the front portion of described rocket Casting device 5 is become a diameter 600mm by the partial reequipping of adorning manned capsule 8, the cylindrical shape cargo hold 25 of long 2.5m to 3m, and at interface 28 places of cargo hold 25 and the fuel compartment 7 of rocket engine 6 by the fixing jump ring 29 of dress, also herein by the blast separator 26 that cargo hold 25 is housed, and with lead be connected as microcomputer chip 10 and power supply 9 in the preceding cone-shaped hood 21 of the hatchcover of cargo hold 25, cargo hold 25 and preceding cone-shaped hood 21 as this hatchcover are secured together with the screw rod drift bolt 32 of the band nut of a perforation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510132498 CN101013017A (en) | 2005-12-28 | 2005-12-28 | Troops and munitions battlefield rapid transportation system device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510132498 CN101013017A (en) | 2005-12-28 | 2005-12-28 | Troops and munitions battlefield rapid transportation system device |
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| Publication Number | Publication Date |
|---|---|
| CN101013017A true CN101013017A (en) | 2007-08-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200510132498 Pending CN101013017A (en) | 2005-12-28 | 2005-12-28 | Troops and munitions battlefield rapid transportation system device |
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| CN (1) | CN101013017A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102442526A (en) * | 2010-10-12 | 2012-05-09 | 杨礼诚 | Potential energy transporting system |
| CN104751613A (en) * | 2013-12-30 | 2015-07-01 | 华为技术有限公司 | Method, terminal and system for life detection, control center and wireless transceiver station |
| CN105627838A (en) * | 2016-02-22 | 2016-06-01 | 许昌义 | Express delivery missile |
-
2005
- 2005-12-28 CN CN 200510132498 patent/CN101013017A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102442526A (en) * | 2010-10-12 | 2012-05-09 | 杨礼诚 | Potential energy transporting system |
| CN104751613A (en) * | 2013-12-30 | 2015-07-01 | 华为技术有限公司 | Method, terminal and system for life detection, control center and wireless transceiver station |
| WO2015100875A1 (en) * | 2013-12-30 | 2015-07-09 | 华为技术有限公司 | Life detection method, terminal and system, control center and wireless transmission/reception station |
| CN105627838A (en) * | 2016-02-22 | 2016-06-01 | 许昌义 | Express delivery missile |
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Open date: 20070808 |