CN107702594A - Guided missile decoy and guided missile truck - Google Patents
Guided missile decoy and guided missile truck Download PDFInfo
- Publication number
- CN107702594A CN107702594A CN201710999978.7A CN201710999978A CN107702594A CN 107702594 A CN107702594 A CN 107702594A CN 201710999978 A CN201710999978 A CN 201710999978A CN 107702594 A CN107702594 A CN 107702594A
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- Prior art keywords
- guided missile
- cylinder
- head
- decoy
- guided
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H3/00—Camouflage, i.e. means or methods for concealment or disguise
Abstract
The present invention relates to a kind of guided missile decoy and guided missile truck, wherein, guided missile decoy includes main body rack, main body rack includes guided missile head (1) and cylinder (2), guided missile head (1) is slidably disposed in one end of cylinder (2), it can outwards be drawn to predeterminated position from cylinder (2) when setting up guided missile, and be pushed back to needing to remove the time receiving in cylinder (2).Such a guided missile decoy, guided missile head can be drawn to predeterminated position when setting up guided missile from cylinder, reach the size and dimension close with true target, and fidelity is high, and be pushed back to when needing and removing receipts and transport in cylinder, be readily transported.Between such a guided missile decoy can save guided missile erection and remove the time receiving, mobility strong, neatly meet the operational requirements in military affairs；And the erection of guided missile can be achieved with by manpower and remove receipts, independent of hoisting equipment, logistic work task amount can be efficiently reduced；Such a guided missile decoy service life length, maintaining are convenient in addition.
Description
Technical field
The present invention relates to camouflage technical field, more particularly to a kind of guided missile decoy and guided missile truck.
Background technology
Camouflage technology: history is long, hidden true and show that vacation is to form indivisible two aspects of camouflage, at all times
The war of China and foreign countries proves to show that vacation advantageously ensures that the hidden of target, is advantageous to scattered and attracts enemy's notice and firepower, favorably
In raising military affairs and economic benefit.During the Second World War, because the high-altitude such as aircraft, dirigible reconnaissance equipment widely uses, to both sides at war
Huge pressure is brought, therefore, each belligerent state manufactures easy military mesh one after another in specific region using all kinds of cheap materials
Model is marked, for the military surveillance of confusing hostile, induction enemy carries out fire attack, reaches protection one's own side military target safety,
Consume the purpose of enemy's operating resources.Here it is the decoy of early stage.
Guided missile has developed the key member as attack and the weapons of system, missilize rapidly since World War II latter stage occurs
Change, auto-control is the main flow direction of world's military developments instantly.Guided missile truck as land-based missile delivery vehicle is guided missile
The motor-driven carrier with transmitting, and enemy attack important goal, are the military targets for needing key protection.Thus, the military produces
To the wilderness demand of guided missile truck decoy.For military surveillance at that time, earliest decoy is with wood or hard paper
Shell is simply process, and has been reached to lure the enemy in well and has been opened fire, confuses the enemy, hiding the purpose of oneself.
With the development of the basic industries such as material, machinery, various types of decoys continue to bring out, wherein inflatable vacation mesh
It is marked with it and manufactures and designs simple, cheap, skill station art function admirable and is promoted rapidly.At present, countries in the world active service decoy is still
It is based on inflatable, in addition, the guided missile decoy of the type such as skeleton covering type, rapid expanding formula, assembled also has a small amount of dress
It is standby.
The decoy of early stage designs, the phase of the outward appearance that only pursues a goal optical signature primarily directed to enemy's optical reconnaissance
Like property.As new Intelligence Technology is fast-developing, particularly radar, satellite technology come across application, microwave and infrared reconnaissance
Progressively turn into the main flow of modern Detection Techniques, traditional optical decoy is due to the difference of material, internal structure etc. and true target
Different, all there is significant difference in its Radar Cross Section and infrared emission feature, therefore, only pursue profile with true guided missile truck
The similitude of profile and visible light wave range, increasingly it is difficult in adapt to the demand of present war.
At present, some occurs in international market of military product can simulate radar, the infrared signature of true target in an extent and scope
Product.But these decoys are all using modified polymer material as main material, by adding associated materials to material matrix
Or equipment is set to simulate the radar reflection feature of decoy and infrared signature inside decoy.Because high polymer material improves
Technology or surface modification technology have some limitations, the performance in terms of material electromagnetism and the metal material used in true guided missile truck
Significant difference also be present, causing this new-type decoy, its verisimilitude also has certain defect compared with true guided missile truck.
Decoy typically requires that in light weight, sound construction is easy, is readily transported, sets up and removes receipts.Decoy is by making material
It is several that material and forming mode are divided into inflatable, assembled, foaming and intumescing formula and pioneer expedients model etc..Inflatable decoy be by
Plastics, rubber film or the gas-charging compound part by fabric and rubber form.It has certain profile fidelity, is advantageous to simulate mesh
The parts such as target pipe, curved surface, and in light weight, small volume.Assembled decoy is by parts such as timber, metal, fiberglass, plastics
Combined with fabric portion covering.There is higher profile fidelity, be easy to serve as entirety with partial component, be easy to and conveniently material
Material is used in combination, and is easy to repair after part breakage and is changed, is widely applied because obtained from.But major part fills at present
Overall dimensions with formula decoy are larger, carry out certain difficulty to setting up and removing take-up, and still deposited in terms of removing the transport after receiving
In larger problem.
The content of the invention
The purpose of the present invention is to propose to a kind of guided missile decoy and guided missile truck, can quickly realize the frame to guided missile decoy
And if remove receipts, neatly to meet use demand.
To achieve the above object, first aspect present invention provides a kind of guided missile decoy, including main body rack, the master
Body support frame includes guided missile head and cylinder, and length direction of the guided missile head along the cylinder is slidably disposed in one end of cylinder,
It can outwards be drawn to predeterminated position from the cylinder when setting up guided missile, and the cylinder is pushed back to needing to remove the time receiving
It is interior.
Further, the guided missile head can be pushed back to all in the cylinder.
Further, guiding mechanism is provided between the inwall of the outer wall of the guided missile head and the cylinder, for described
The motion of guided missile head is oriented to.
Further, the guiding mechanism includes channled rail and the vertical pulley in the channled rail, described
Length direction of the channled rail along the cylinder is located at the upper-lower position of cylinder inboard wall, and the vertical pulley is located at the guided missile head
The upper-lower position of outer wall.
Further, the guiding mechanism also includes horizontal guide rail and rides over the horizontal trolley on the horizontal guide rail, institute
The right position that length direction of the horizontal guide rail along the cylinder is located at cylinder inboard wall is stated, the horizontal trolley is located at the guided missile
The right position of head outer wall.
Further, the guiding mechanism includes horizontal trolley at least described in two groups, horizontal trolley point at least described in two groups
Wei Yu not the vertical both sides of the pulley along guided missile head length direction.
Further, the first position limiting structure is provided between the guided missile head and cylinder, is pushed back for limiting the guided missile head
Extreme position in the cylinder；And/or
The second position limiting structure is provided between the guided missile head and cylinder, for limiting the pole when guided missile head is outwards extracted out
Extreme position.
Further, the guided missile decoy also includes fixture, and is respectively equipped with the guided missile head and the cylinder
One hole and the second hole, the guided missile head are inwardly pushed back or pulled out to extreme position, first hole and second
The position in hole is corresponding, and the fixture can be located in first hole and the second hole and realize the guided missile head and cylinder
It is fixed.
Further, the free end of the guided missile head is in truncated cone shape, and the top center of the frustum of a cone is provided with
Screw rod, for connecting the guided missile cap of outside arranging, the guided missile cap is adapted with the frustum of a cone.
Further, the main body rack also includes missile tail, and the missile tail is detachably arranged in the cylinder
The other end, the missile tail can be inserted in the cylinder after pulling down.
Further, the main body rack also includes mounting seat, and the missile tail is connected to institute by the mounting seat
The other end of cylinder is stated, the mounting seat is provided with the support base for being used for being hinged with guided missile truck decoy.
Further, the guided missile decoy also includes decoration, and the decoration is detachably arranged on the cylinder,
The decoration can be inserted in the cylinder after pulling down.
Further, the cylinder includes retainer plate and multiple cylinder sections, by described between the adjacent cylinder section
Retainer plate connects.
Further, the guided missile decoy is also enclosed in the covering outside the main body rack, and the covering is adopted
With 5A05 aluminium-plastic panels；And/or the cylinder uses Q235 or Q345 steel.
To achieve the above object, second aspect of the present invention provides a kind of guided missile truck, including car body decoy and above-mentioned reality
Apply the guided missile decoy described in example.
Based on above-mentioned technical proposal, guided missile decoy of the invention, guided missile head can be taken out when setting up guided missile from cylinder
Go out to predeterminated position, reach the apparent size and shape, fidelity height close with true target, and push away when needing and removing receipts and transport
It is back in cylinder, is readily transported.Between such a guided missile decoy can save guided missile erection and remove the time receiving, mobility strong；And pass through
Manpower can be achieved with the erection of guided missile and remove receipts, without relying on hoisting equipment, can efficiently reduce logistic work task amount；In addition
Such a guided missile decoy service life length, maintaining are convenient.
Brief description of the drawings
Accompanying drawing described herein is used for providing a further understanding of the present invention, forms the part of the application, this hair
Bright schematic description and description is used to explain the present invention, does not form inappropriate limitation of the present invention.In the accompanying drawings：
Fig. 1 is the structural representation that guided missile decoy of the present invention is arranged on guided missile truck；
Fig. 2 is the appearance schematic diagram of one embodiment of guided missile decoy of the present invention；
Fig. 3 is the structural representation of one embodiment of cylinder；
Fig. 4 is the side view of cylinder shown in Fig. 3；
Fig. 5 is the structural representation of one embodiment of guided missile head；
Fig. 6 a and Fig. 6 b are respectively the mounting structure schematic diagram of vertical pulley and horizontal trolley, and wherein Fig. 6 b are the A in Fig. 5
Locate enlarged drawing；
Fig. 7 is the structural representation of one embodiment of guided missile head inner skeleton；
Fig. 8 is schematic enlarged-scale view at the B in Fig. 7；
Fig. 9 is the top view of guided missile head inner skeleton shown in Fig. 7；
Figure 10 is the C-C sectional views in Fig. 9.
Description of reference numerals
1st, guided missile head；2nd, cylinder；3rd, missile tail；4/5th, decoration；6th, mounting seat；7th, channled rail；8th, horizontal guide rail；
11st, skeleton；12nd, vertical pulley；13rd, horizontal trolley；14th, guided missile cap；15th, screw rod；16th, the first position limiting structure；17th, the first hole；
21st, cylinder section；22nd, retainer plate；61st, support base.
Embodiment
The present invention described further below.In the following paragraphs, the different aspect of embodiment is defined in more detail.So
The each side of restriction can combine with any other one side or many aspects, not can be combined unless explicitly stated otherwise.Especially,
It is considered as that preferable or favourable any feature can be considered as preferable or favourable feature group with other one or more
Close.
The term descriptions merely for convenience such as " first " that occurs in the present invention, " second ", there are same names to distinguish
Different building blocks, be not offered as successively or primary-slave relation.
In the description of the invention, it is to be understood that term " length ", " width ", " height ", " on ", " under ",
The orientation or position relationship of the instruction such as "left", "right", " preceding " and " rear " are based on orientation shown in the drawings or position relationship, are only
There must be specific orientation, for the ease of the description present invention, rather than the device of instruction or hint meaning with specific orientation
Construction and operation, therefore it is not intended that limiting the scope of the invention.
Referring to figs. 1 to Figure 10, the present invention proposes a kind of guided missile decoy, is assembled simulation model guided missile.At one
In schematical embodiment, the guided missile decoy includes main body rack, and main body rack includes guided missile head 1 and cylinder 2, guided missile head 1
It is independent module with cylinder 2, cylinder 2 uses hard hollow structure.Guided missile head 1 is slideably set along the length direction of cylinder 2
In one end of cylinder 2, guided missile head 1 can outwards be drawn to predeterminated position when needing and setting up guided missile from cylinder 2, and need
Removing the time receiving pushes back in cylinder 2.Preferably, the entire length of guided missile head 1 can be back into cylinder 2.As needed, also can be only
The partial-length of guided missile head 1 is pushed back in cylinder 2.
After guided missile head 1 is outwards drawn to predeterminated position, the appearance and size of guided missile decoy is high with true military products similarity, and
To make decoy true to nature, the set location of decoy is consistent with tactics, the technical requirements of true target, and keeps one with true target
Fixed safe distance.After guided missile head 1 inwardly pushes back to cylinder 2, guided missile overall appearance size is set to meet the model that traffic condition allows
Enclose, such as in can packing into the container, convenient transportation, mobility strong, and remove receipts with regard to that can be accomplished manually in a short time, without according to
Rely crane gear, the flexible transformation of tactics can be coordinated.Guided missile head 1 and cylinder 2 also allow for controlling each using modularized design
Module weight and operability, it is easy to maintain.
In order to make guided missile head 1 neatly slide in cylinder 2, prevent from that clamping stagnation occurs in motion process, raising is held
The reliability of guided missile decoy is set up during row tactics, guiding mechanism is provided between the outer wall of guided missile head 1 and the inwall of cylinder 2, is used
It is oriented in motion of the guided missile head 1 along the length direction of cylinder 2.Guiding mechanism can take various forms, such as interior outer guide
Coordinate, sliding bearing and line slideway coordinate, pulley and guide rail coordinate etc..
Preferably, guiding mechanism is symmetrically arranged at left and right and/or upper-lower position in the cross section of cylinder 2.Can integrally it rise
To load-bearing and the effect being oriented to, play balance and promote guiding, ensure that guided missile head 1 smoothly completes pulling motion, avoid guided missile
First 1 because inequality of exerting oneself glances off in draw process and interim card occurs in cylinder 2.
Here a kind of concrete structure of guiding mechanism setting is provided, as shown in figure 5, guiding mechanism includes two channled rails
7 and two vertical pulleys 12, with reference to figure 6a, for vertical pulley 12 in channled rail 7, two side walls of channled rail 7 can
The spacing effect in left and right is played to guided missile head 1, channled rail 7 is oriented to the sliding trace of vertical pulley 12.Two flute profiles
Length direction of the guide rail 7 along cylinder 2 is respectively provided at the upper-lower position of the inwall of cylinder 2, and the length of channled rail 7 is not less than guided missile head
1 whole movement travel, two vertical pulleys 12 are respectively provided at the upper-lower position of the outer wall of guided missile head 1 in same cross section.
Again referring to Fig. 5, guiding mechanism may also include two horizontal guide rails 8 and at least one set of horizontal trolley 13, horizontal trolley
13 are ridden on the horizontal part of horizontal guide rail 8, and horizontal guide rail 8 is played a supporting role to horizontal trolley 13, and horizontal trolley 13 can be
Slided on horizontal guide rail 8.With reference to figure 6b, horizontal trolley 13 is using the structure that guide sleeve is set in Bearing outer.Two levels are led
Rail 8 is located at the right position of the inwall of cylinder 2 along the length direction of cylinder 2 respectively, and two horizontal trolleys 13 are in same cross section
It is located at the right position of the outer wall of guided missile head 1.In Figure 5, for the ease of showing horizontal trolley 13 and vertical pulley 12 simultaneously, by water
Horizontal sliding wheel 13 is also shown in the section of vertical pulley 12, but actually horizontal trolley 13 is located at the left and right position of the outer wall of guided missile head 1
Put.
Preferably, as shown in figure 5, guiding mechanism includes at least two groups of horizontal trolleys 13, at least two groups of horizontal trolleys 13 divide
Not Wei Yu both sides of the vertical pulley 12 along the length direction of guided missile head 1, i.e. horizontal trolley 13 and vertical pulley 12 in the length of guided missile head 1
Direction on be arranged at intervals, to obtain stable support in the longitudinal direction, effective guide effect is provided to guided missile head 1.
Vertical pulley 12 and horizontal trolley 13 are applied in combination, the fortune of guided missile head 1 can be made by way of increasing and constraining
Dynamic more stable flexible, horizontal trolley 13 is used cooperatively with horizontal guide rail 8 can avoid producing Planar Mechanisms to pulley, prevent guided missile
First 1 not enough occurs catching phenomenon with the relative motion of cylinder 2 constraint.In guided missile head 1 connects the embodiment formed by skeleton 11,
Each pulley can be fixed on skeleton 11 by way of welding.
Further, guided missile head 1 can be carried out spacing during extracting out and pushing back.The is provided between guided missile head 1 and cylinder 2
One position limiting structure 16, the extreme position being forced back towards for limiting guided missile head 1 in cylinder 2.It is as shown in fig. 7, close in guided missile head 1
One end of cylinder 2 is provided with baffle plate, also correspondingly is provided with baffle plate (not shown) in the inner of the inside channel guide rail 7 of cylinder 2, when leading
When bullet 1 inwardly moves to two baffle plate contacts, guided missile head 1 just stops slid inward, prevents guided missile head 1 from slipping into cylinder 2 too
Extraction bad over long distances, and too many space in cylinder 2 is taken, to there is abundant space decoration etc. in cylinder 2.
On this basis, fixture, C-C as shown in Figure 10 figure, guided missile head 1 are also included in guided missile decoy of the invention
Side wall be provided with the first hole 17, the side wall of cylinder 2 is provided with the second hole, and guided missile head 1 pushes back to extreme position in cylinder 2
Under state, the position in the first hole 17 and the second hole is corresponding, and fixture, which can be located in, to be realized in the first hole 17 and the second hole and lead
The fixation of bullet 1 and cylinder 2, to prevent the guided missile phenomenon that guided missile head 1 is deviate from after receipts are removed, and avoid causing in transportation
Unnecessary damage.
Further, the second position limiting structure is provided between guided missile head 1 and cylinder 2, when outwards being extracted out for limiting guided missile head 1
Extreme position.For example, block piece is provided with close to one end of cylinder 2 in guided missile head 1, in cylinder 2 close to one end of guided missile head 1
Provided with block piece (not shown), when 1 outside pull of guided missile head contacts to two block pieces, guided missile head 1 just reaches in advance
If position, it can not now continue outside pull.
On the basis of guided missile head 1 is extracted out in place, it can be also fixed by the above-mentioned fixture provided, such as can be
It is located on the baffle plate of guided missile head 1 and opens up hole respectively on cylinder 2, fixture is located in the two holes, to ensure that guided missile exists
Complete the high similarity for during tactics required movement being not in guided missile head landing phenomenon and guided missile entirety.
2 adoptable concrete structure of guided missile head 1 and cylinder is provided herein.
Wherein, as shown in figure 5 and figure 7, guided missile head 1 is formed by skeleton 11, can reach higher strong while loss of weight
Degree, main part of the guided missile head 1 close to the one end of cylinder 2 enclose cylinder, from figure 7 it can be seen that can be with skeleton 11
Inclined bar is set to be strengthened.The free end of guided missile head 1 forms truncated cone shape, and the centre bit at the top of the frustum of a cone installs
There is screw rod 15, for connecting the guided missile cap 14 of outside arranging, guided missile cap 14 is adapted with the frustum of a cone.The frustum of a cone can make guided missile cap
14 are closely fit with guided missile head 1.
In Figure 5, the forward part skeleton 11 of guided missile head 1 is wrapped up by covering, and the part that rear part is not wrapped up by covering is embedding
Enter in cylinder 2, the part being connected as guided missile head 1 with cylinder 2, when being pushed into guided missile head 1 into cylinder 2, be enclosed with covering
Part also enters in cylinder 2.
As shown in figure 3, cylinder 2 is cylinder, including retainer plate 22 and multiple cylinder sections 21, between adjacent cylinder section 21
Connected by retainer plate 22, it is smaller unit that can dismantle guided missile decoy when traffic condition is limited, is locally damaged
Bad when, is conveniently replaceable.
On the basis of above-described embodiment, as shown in Fig. 2 main body rack also includes missile tail 3, missile tail 3 is removable
It is located at the other end of cylinder 2 with unloading, missile tail 3 can equally be pulled down when needing and removing receipts or transport and insert the hollow of cylinder 2
In cavity, or other positions are placed on, further to reduce the entire length of guided missile.
Further, as shown in figure 3, main body rack also includes mounting seat 6, missile tail 3 is connected to cylinder by mounting seat 6
The other end of body 2, mounting seat 6 are provided with the support base 61 for being used for being hinged with guided missile truck decoy.By being articulated and connected, guided missile is false
Target can flexibly between horizontality and vertical state area rotation, with the various tactics of flexible adaptation.
Again referring to Fig. 2, guided missile decoy may also include decoration 4,5, and decoration 4,5 is detachably arranged in main body rack
On, decoration 4,5 can be pulled down in decoy removes receipts or transportation and is placed into cylinder 2, so that volume shared by guided missile
It is smaller.
Outside main body rack, it can also be surrounded using covering, to improve the fidelity of guided missile.Covering can use metal
Aluminium makes with polyethylene composite aluminium plastic plate material, such as 5A05 aluminium-plastic panels etc., can not only reduce own wt, make full car gross weight
Amount is the 8% of true guided missile truck；And the verisimilitude of guided missile decoy appearance profile can also be improved, and make visible ray and radar reflection
Feature is consistent with true guided missile.The skeleton 11 and cylinder 2 of guided missile head 1 use Q235 or Q345 steel, such as seamless steel pipe, with
Ensure the intensity of missile mainbody structure, with larger or remain to keep the steadiness of self structure when external impact is larger in wind-force,
Convenient disassembly, significantly reduce logistics task amount.Material and process of surface treatment to produce used by such a guided missile decoy
Product are grown without easily worn part, service life, without short-term repeated construction, without often safeguarding.
It is described above, assembled simulation model guided missile of the invention flexibly the true target of simulation can be constructed actual and made
Industry time length, heat radiation characteristic, radio wave attenuation feature, acousto-optic feature and activity trail phase consistent with true target shape size
Seemingly.In addition, the guided missile decoy of the present invention main body rack and covering when enemy bombs can crush, to produce and true guided missile
The same fragment effect of car.
Next the detailed process that guided missile decoy shown in Fig. 2 set up and removed receipts is provided.
Needing to remove the time receiving, first removing missile-borne decoration 4,5；Then guided missile head 1 is promoted into cylinder 2,
Until the baffle plate on guided missile head 1 contacts with the baffle plate on the inside channel guide rail 7 of cylinder 2, then fixture is located in the of guided missile head 1
It is fixed in one hole 17 and the second hole of cylinder 2；Missile tail 3 is pulled down from cylinder 2 again, by decoration 4,5 from guided missile
The mating holes of afterbody 3 and cylinder 2 loads in cylinder 2, then missile tail 3 is loaded in cylinder 2, and this is that guided missile removes receipts or transport
State.
When needing to set up, missile tail 3 and decoration 4,5 are taken out out of cylinder 2, decoration 4,5 is arranged on respective
On missile-borne reserved location, missile tail 3 is arranged in mounting seat 6.Then will be taken for the fixture for fixing guided missile head 1
Under, outside pull guided missile head 1, until the block piece contact on guided missile head 1 and cylinder 2, illustrates that guided missile head 1 has moved default position to
Put, similarly, fixed the position of guided missile head 1 and cylinder 2 using fixture.Guided missile is holded up, the erection of guided missile is completed.
In addition, present invention also offers a kind of guided missile truck, as shown in figure 1, including guided missile truck decoy and above-mentioned each implementation
Guided missile decoy described in example.Such a guided missile truck has higher fidelity, can be according to the flexible simulation of military tactical demand
The tactical operation of true target, scene is conveniently withdrawn after use, is easy to safeguard.
A kind of guided missile decoy provided by the present invention and guided missile truck are described in detail above.It is used herein
Specific embodiment is set forth to the principle and embodiment of the present invention, and the explanation of above example is only intended to help and managed
Solve the method and its core concept of the present invention.It should be pointed out that for those skilled in the art, do not departing from
On the premise of the principle of the invention, some improvement and modification can also be carried out to the present invention, these are improved and modification also falls into this hair
In bright scope of the claims.
Claims (15)
1. a kind of guided missile decoy, it is characterised in that including main body rack, the main body rack includes guided missile head (1) and cylinder
(2), length direction of the guided missile head (1) along the cylinder (2) is slidably disposed in one end of cylinder (2), can set up
Outwards it is drawn to predeterminated position during guided missile from the cylinder (2), and is pushed back to needing to remove the time receiving in the cylinder (2).
2. guided missile decoy according to claim 1, it is characterised in that the guided missile head (1) can all push back to institute
State in cylinder (2).
3. guided missile decoy according to claim 1, it is characterised in that the outer wall of the guided missile head (1) and the cylinder
(2) guiding mechanism is provided between inwall, is oriented to for the motion to the guided missile head (1).
4. guided missile decoy according to claim 3, it is characterised in that the guiding mechanism include channled rail (7) and
Vertical pulley (12) in the channled rail (7), length direction of the channled rail (7) along the cylinder (2) are set
In the upper-lower position of cylinder (2) inwall, the vertical pulley (12) is located at the upper-lower position of the guided missile head (1) outer wall.
5. guided missile decoy according to claim 4, it is characterised in that the guiding mechanism also includes horizontal guide rail (8)
With the horizontal trolley (13) ridden on the horizontal guide rail (8), length direction of the horizontal guide rail (8) along the cylinder (2)
The right position of cylinder (2) inwall is located at, the horizontal trolley (13) is located at the right position of the guided missile head (1) outer wall.
6. guided missile decoy according to claim 5, it is characterised in that the guiding mechanism includes water at least described in two groups
Horizontal sliding wheel (13), horizontal trolley (13) is located at the vertical pulley (2) along guided missile head (1) length direction respectively at least described in two groups
Both sides.
7. guided missile decoy according to claim 4, it is characterised in that be provided between the guided missile head (1) and cylinder (2)
First position limiting structure (16), the extreme position pushed back to for limiting the guided missile head (1) in the cylinder (2)；And/or
The second position limiting structure is provided between the guided missile head (1) and cylinder (2), is outwards extracted out for limiting the guided missile head (1)
When extreme position.
8. guided missile decoy according to claim 1, it is characterised in that also including fixture, the guided missile head (1) and institute
State and the first hole (17) and the second hole are respectively equipped with cylinder (2), the guided missile head (1) is inwardly pushed back or pulled out to extremely spacing
In the state of putting, first hole (17) is corresponding with the position in the second hole, and the fixture can be located in first hole
(17) fixation of the guided missile head (1) and cylinder (2) and in the second hole is realized.
9. guided missile decoy according to claim 1, it is characterised in that the free end of the guided missile head (1) is in the frustum of a cone
Shape, the top center of the frustum of a cone are provided with screw rod (15), described to lead for connecting the guided missile cap (14) of outside arranging
Cap (14) is played to be adapted with the frustum of a cone.
10. guided missile decoy according to claim 1, it is characterised in that the main body rack also includes missile tail
(3), the missile tail (3) is detachably arranged in the other end of the cylinder (2), missile tail (3) energy after pulling down
Enough insert in the cylinder (2).
11. guided missile decoy according to claim 10, it is characterised in that the main body rack also includes mounting seat (6),
The missile tail (3) is connected to the other end of the cylinder (2) by the mounting seat (6), and the mounting seat (6) is provided with
For the support base (61) being hinged with guided missile truck decoy.
12. guided missile decoy according to claim 1, it is characterised in that also including decoration (4；5), the decoration
(4；5) it is detachably arranged on the cylinder (2), the decoration (4；5) can be inserted after pulling down in the cylinder (2).
13. guided missile decoy according to claim 1, it is characterised in that the cylinder (2) includes retainer plate (22) and more
Individual cylinder section (21), pass through the retainer plate (22) between the adjacent cylinder section (21) and connect.
14. guided missile decoy according to claim 1, it is characterised in that be also enclosed in outside the main body rack
Covering, the covering uses 5A05 aluminium-plastic panels；And/or the cylinder (2) uses Q235 or Q345 steel.
15. a kind of guided missile truck, it is characterised in that false including any described guided missile of guided missile truck decoy and claim 1~14
Target.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710999978.7A CN107702594B (en) | 2017-10-24 | 2017-10-24 | Missile decoy and missile vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710999978.7A CN107702594B (en) | 2017-10-24 | 2017-10-24 | Missile decoy and missile vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107702594A true CN107702594A (en) | 2018-02-16 |
| CN107702594B CN107702594B (en) | 2023-07-04 |
Family
ID=61182215
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710999978.7A Active CN107702594B (en) | 2017-10-24 | 2017-10-24 | Missile decoy and missile vehicle |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3386188A (en) * | 1965-08-23 | 1968-06-04 | Navy Usa | Missile launch simulator |
| CN1391648A (en) * | 1999-11-18 | 2003-01-15 | 斯托姆金属有限公司 | Decoy |
| US20030226771A1 (en) * | 2002-06-06 | 2003-12-11 | Corboy Grant W. | Inflatable restraint for missiles and missile canisters |
| CN103512428A (en) * | 2012-06-26 | 2014-01-15 | 北京元恒大通科技有限公司 | Hard shell type false missile vehicle target |
| CN205627067U (en) * | 2016-04-29 | 2016-10-12 | 汕头市乐飞科教有限公司 | Military car of interesting strong toy |
| CN106875806A (en) * | 2017-02-05 | 2017-06-20 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special respective-guide type guided cartridge vehicle model of teenager's research in defense-related science and technology |
| CN207570411U (en) * | 2017-10-24 | 2018-07-03 | 北京元恒大通科技有限公司 | Guided missile decoy and guided missile truck |
-
2017
- 2017-10-24 CN CN201710999978.7A patent/CN107702594B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3386188A (en) * | 1965-08-23 | 1968-06-04 | Navy Usa | Missile launch simulator |
| CN1391648A (en) * | 1999-11-18 | 2003-01-15 | 斯托姆金属有限公司 | Decoy |
| US20030226771A1 (en) * | 2002-06-06 | 2003-12-11 | Corboy Grant W. | Inflatable restraint for missiles and missile canisters |
| CN103512428A (en) * | 2012-06-26 | 2014-01-15 | 北京元恒大通科技有限公司 | Hard shell type false missile vehicle target |
| CN205627067U (en) * | 2016-04-29 | 2016-10-12 | 汕头市乐飞科教有限公司 | Military car of interesting strong toy |
| CN106875806A (en) * | 2017-02-05 | 2017-06-20 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special respective-guide type guided cartridge vehicle model of teenager's research in defense-related science and technology |
| CN207570411U (en) * | 2017-10-24 | 2018-07-03 | 北京元恒大通科技有限公司 | Guided missile decoy and guided missile truck |
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| CN107702594B (en) | 2023-07-04 |
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