CN106515330B - High speed amphibious landing vehicle - Google Patents
High speed amphibious landing vehicle Download PDFInfo
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- CN106515330B CN106515330B CN201611174308.3A CN201611174308A CN106515330B CN 106515330 B CN106515330 B CN 106515330B CN 201611174308 A CN201611174308 A CN 201611174308A CN 106515330 B CN106515330 B CN 106515330B
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- Prior art keywords
- circular hole
- compartment
- axis
- fluted disc
- upper plate
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F3/00—Amphibious vehicles, i.e. vehicles capable of travelling both on land and on water; Land vehicles capable of travelling under water
- B60F3/0061—Amphibious vehicles specially adapted for particular purposes or of a particular type
Abstract
The present invention relates to a kind of high speed amphibious landing vehicles, are made of compartment (1), earthing or grounding means, and two airscrew engines (8) are mounted on compartment (1).It is big with the contact area on ground, and pressure is small, will not get deeply stuck in sand ground or miriness;Two airscrew engines (8), power is powerful, and speed high maneuver is flexible when logging in;Airscrew engine (8) rotatably, is easy to change direction of advance;Soldier, which logs in whole process, need not leave high speed amphibious landing vehicle, and from beginning to end under its protection, injures and deaths substantially reduce;Which employs provision for thermal insulation and Measure of reducing vibration, interior environment is preferable.In short, high speed amphibious landing vehicle energy effective protection soldier, firepower is powerful, can quickly log in, it is a kind of preferable landing equipment.
Description
Technical field
It is need not getting off the present invention relates to a kind of high speed amphibious landing vehicle, especially soldier, firepower is powerful, can quickly step on
The high speed amphibious landing vehicle in land.
Background technology
During landing operations, bank is not soft sand ground, is exactly the slob for hiding big finger stone, tank and plate armour
Vehicle is slow in action, and target is big in addition, is easy to be attacked by guided missile and rocket projectile;Soldier leaves ship or panzer, paddle on
Bank, action is slower, and without armoring protection, enemy occupies a commanding position, unless taking the enemy unaware, existing landing approach may cause sternly
Severe injury is died.
To reduce injures and deaths and loss, landing operations must be with lightning speed, and logging in soldier must adequately protect, and log in firepower
It is powerful neutralization must to be collected.
It confronts in the direction of effort, it is desirable to be able to realize early, this is the ardent hope of liberation army, and compatriots are duty-bound
It is duty-bound.
Invention content
It is need not getting off the technical problem to be solved in the present invention is to provide a kind of soldier, firepower is powerful, can quickly log in
High speed amphibious landing vehicle.Another will solve the problems, such as it is the method for implementing landing operations using high speed amphibious landing vehicle.
The technical issues of to solve above-mentioned high speed amphibious landing vehicle, the technical scheme is that:
A kind of high speed amphibious landing vehicle contains compartment and earthing or grounding means.
Compartment is surrounded by one piece of upper plate, one piece of bottom plate, one piece of foreboard, one piece of back plate, two blocks of side plates;The foreboard is from top to bottom
It gradually tilts backwards, lower end and the round and smooth fastening in front end of the bottom plate connect, and have multiple embrasures thereon;There is vehicle in the back plate
Door;Vertical clapboard is located at the rear portion in the compartment inner cavity, and the lower surface of end face and the upper plate, which fastens, thereon connects, lower face with
The upper surface of the bottom plate fastens connection, and both lateral sides face is solid with the interior lateral face of one of this two blocks of side plates of corresponding position respectively
It is close to and connects, there is division plate door thereon;Between the partition board and the back plate on the bottom plate of channel both sides, storage weapons and ammunitions, tool and
Engine fuel;The upper plate is rectangle, has rear circular hole and preceding circular hole on the longitudinal midline of upper surface, the rear circular hole again positioned at every
The surface of plate, the preceding circular hole are located at the front of the rear circular hole;Also there are multiple embrasures on the side plate.
Camera, display screen, gasket, seat, power and control system are installed on compartment.
Camera is located at the lateral center of compartment upper plate upper surface front end, is fixedly connected with the upper plate of corresponding position.
Display location is suspended in the dead astern of the preceding circular hole on compartment upper plate and close on this of corresponding position
On the lower surface of plate, the scene in the front that camera is shot on the compartment is shown on the display screen.
The diameter of circular gasket is less than the transverse width of compartment upper plate, the axis weight of axis and the rear circular hole on the upper plate
It closes, the upper surface of lower disc and the corresponding position upper plate, which fastens, to be connected;There are vertical gasket circular hole, the gasket in the center of the gasket
The internal diameter of circular hole is equal to or more than the internal diameter of the rear circular hole.
Multiple seats fasten on the upper surface of platform floor, and the seat positioned at display screen rear multiplies for driver
It sits, remaining seat supplies other soldiers rides.
Power and control system are made of airscrew engine, fagging, fluted disc, fluted disc axis, gear, gear shaft, steering wheel.
Connection propeller is fastened on the axis that one of two airscrew engines forward extend out.
The diameter of fluted disc is equal to the diameter of compartment Upper gasket, the axis weight of axis and the rear circular hole on the compartment upper plate
It closes, the upper disc movable contact of lower disc and the gasket;There is fluted disc circular hole at the center of the fluted disc, the axis of the fluted disc circular hole with
The axis of the fluted disc overlaps.
The vertical axial height of fluted disc axis is equal to the sum of the vertical thickness of fluted disc, gasket, compartment upper plate, and outer diameter is equal to should
The internal diameter of rear circular hole on upper plate is inserted in the fluted disc circular hole on the fluted disc, the gasket circular hole on the gasket, the rear circular hole,
It fastens with the upper plate and connects, and is fixed together with the fluted disc;Its corresponding position of the inner circumferential surface of the gasket circular hole
The fluted disc axis circumferential surface movable contact or mutually opposed.
One of two faggings are rectangular slab;This two fagging is symmetrically lived apart the both sides of fluted disc axis, the lower end of one of this two fagging
The upper surface of this of face and corresponding position fluted disc fastens connection;This two fagging is located at one of two airscrew engines center of gravity
The lower surface of the airscrew engine shell of underface, the upper surface of one of this two fagging and the surface of corresponding position, which fastens, to be connected
It connects;The axis of this two airscrew engine is parallel and vertical with the line of this two airscrew engines center of gravity;Mounted on the spiral
Propeller on paddle motor will not collide when rotating with the fluted disc.
The diameter of gear be less than fluted disc diameter, be located at fluted disc front and engage with the fluted disc, vertical axis and
The axis of preceding circular hole on compartment upper plate overlaps, the upper surface movable contact of the upper plate of lower disc and corresponding position;The tooth
The center of wheel has vertical gear circular hole, the axis of the gear circular hole to be overlapped with the axis of the gear.
The diameter of steering wheel is more than the diameter of gear, but less than the diameter of fluted disc, is located at the lower section of display screen on compartment
And close to the lower face of the display screen, there is steering wheel circular hole at center;The axis of the axis and direction disk of direction disk circular hole
It overlaps, internal diameter is equal to the internal diameter of the gear circular hole on gear.
The outer diameter of gear shaft is equal to the internal diameter of the gear circular hole on gear, is inserted in the gear circular hole, on compartment upper plate
In steering wheel circular hole on preceding circular hole, steering wheel, be fixedly connected with the upper plate, the external part upward from the preceding circular hole with should
Gear fastening links together, and the external part downward from the preceding circular hole links together with the fastening of corresponding position direction disk.
Earthing or grounding means is made of floor, cooling fin, heat-insulated column.
The tablet and wraping plate on floor are integral;The tablet is identical as the base plate configuration in compartment, area equation, and being located at should
The underface of bottom plate;The transverse width of the wraping plate is equal to the tablet transverse width, and front end upwarps, before lower end and the tablet
Hold round and smooth connect.
On the upper surface of the evenly dispersed tablet mounted on floor of polylith cooling fin;The cooling fin is strip piece, axis
Line is parallel with the axis of the tablet, and longitudinal length is equal to the longitudinal length of the tablet, thereafter the rear end face of end face and the tablet
It flushes, upper surface is opposed with the lower surface of the bottom plate on the compartment of corresponding position but does not contact, lower surface and corresponding position
The tablet upper surface fasten connection.
Multiple heat-insulated column dispersions are on the tablet on floor and the bottom plate in compartment;The heat-insulated column is short and small cylinder or more ribs
Column is manufactured with heat-insulating material, and vertical axial height is more than the vertical height of cooling fin, lower face and corresponding position it is flat
The upper surface of plate fastens connection, and the lower surface of the bottom plate of end face and corresponding position fastens connection thereon.
The soldier on compartment upper plate is lain concealed for protection, from top to bottom the lower face of gradual sweptback armour and vehicle
The front end of the upper surface of compartment upper plate fastens connection, from top to bottom gradually the lower face of intilted two pieces of armours respectively with this
The upper surface of one of upper plate front part sides fastens connection, has multiple vertical shooting notches on the armour.
To reinforce the firepower of high speed amphibious landing vehicle, on compartment in addition to having rifle, machine gun, rocket launcher, flame are also had
Injector.
Installation, which is fastened, to protect airscrew engine, on the upper surface of compartment upper plate starts machine protective cover, two propellers
Engine is hidden in it;This starts the front end of machine protective cover to have air admission hole, rear end open, by bullet front from top to bottom gradually to
Rear-inclined is gradually sloped inwardly from top to bottom by one of two sides are played.
The method for implementing landing operations using high speed amphibious landing vehicle is such:
After high speed amphibious landing vehicle is transported to debarkation point Its Adjacent Waters by large ship, go out before leaving the large ship,
While naval vessel and aircraft denial of the air are supported, and artillery fire coverage goal, the earth steps and trench in channel are scabbled, channel is destroyed
Barrier ignites the land mine on channel, eliminates channel both sides enemy;Then high speed amphibious landing vehicle drives towards behind debarkation point in high speed
Bank, to remaining unfriendly target come down in torrents bullet, launch a rocket shell, jet flames, rush at rapidly highland eliminate the remnants of the enemy force, it is too late with a sudden peal of thunder
The gesture for covering ear seizes position.
During traveling, the front situation that driver shows according to display screen selects travel path, adjusts driving side
To;When steering wheel rotationally clockwise when, band active toothed disk rotates in an anti-clockwise direction, and the rear end of corresponding airscrew engine is biased to
Right side makes high speed amphibious landing vehicle turn to the right;When steering wheel rotates in an anti-clockwise direction, band active toothed disk turns clockwise
Dynamic, left side is biased in the rear end of corresponding airscrew engine, and high speed amphibious landing vehicle is made to turn to the left;When the axis of airscrew engine
When line is parallel with the axis in compartment, the direction of advance of high speed amphibious landing vehicle is constant.
When more high speed amphibious landing vehicles log in simultaneously, advance in a triangle or laterally a line promotes, finally is needing to account for
Converge on the position of neck;Then large quantities of follow-up unit's follow-ups, consolidate a position, exploit success.
After such structure, since the contact area on floor and ground is big, pressure is small, and high speed amphibious landing vehicle will not
It gets deeply stuck in sand ground or miriness;Since the power of high speed amphibious landing vehicle comes from two airscrew engines, power is powerful, speed
More than panzer or tank;Since airscrew engine is rotatable, high speed amphibious landing vehicle is easy to change direction.In short, high speed
The speed and motor-driven of amphibious landing vehicle is more than tank and panzer.There is such landing equipment, injures and deaths subtract greatly when logging in.
After such structure, high speed amphibious landing vehicle is stepped on from the large ship for leaving carrying to beachhead is captured
Land battle scholar whole process need not leave high speed amphibious landing vehicle, debark and on foot in sand ground or muddy ground uplink into certainly without paddling
Begin to end under the protection in compartment, injures and deaths will substantially reduce.Its superiority is more than helicopter.Because helicopter closes on landing
Shi Sudu is small, is easy by missile attack;Because soldier will come out from helicopter eventually, out when being most dangerous
It carves.
After such structure, since the lower plate in compartment is not in direct contact with ground;Due to the floor contacted with ground
It is connect by heat-insulated column with lower plate, and heat-insulated column is manufactured with heat-insulating material, the heat that the friction on floor and ground generates seldom conducts
To compartment, and taken away by the air that cooling fin is flowed.Therefore temperature is normal in compartment, is not influenced on soldier in compartment.
After such structure, due between the fluted disc and compartment upper plate of installation airscrew engine across gasket, by
In the fluted disc axle position on fluted disc in the surface of partition board, the vibration of airscrew engine is passed to after being buffered by gasket by partition board
Then lower plate passes to floor by heat-insulated column, then passes to ground from floor, the vibration of airscrew engine is to soldier in compartment
Influence substantially reduces.
After such structure, charge with vehicle due to logging in soldier, can carry a large amount of weapons and ammunition on vehicle, individual soldier with
Its also energy band of motionless weapon, firepower concentrate it is fierce, it is as powerful as a thunderbolt irresistible, can effectively preserve oneself and disappear in time
It goes out enemy, moreover it is possible to lightning speed to seize beachhead.
Description of the drawings
Specific embodiments of the present invention will be described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is the schematic side view of high speed amphibious landing vehicle, but the side plate on compartment is detached from from compartment.
Fig. 2 is the schematic top plan view of earthing or grounding means.
Fig. 3 is the schematic top plan view of compartment upper plate.
Specific implementation mode
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of high speed amphibious landing vehicle contains compartment 1 and earthing or grounding means.
As shown in Figure 1, compartment 1 is by one piece of upper plate 1a, one piece of bottom plate 1b, one piece of foreboard 1c, one piece of back plate 1d, two blocks of side plates
It surrounds.Foreboard 1c is gradually tilted backwards from top to bottom, and lower end and the round and smooth fastening in front end of bottom plate 1b connect, and have thereon more
A embrasure 1h.There is car door 1e on back plate 1d.Vertical clapboard 1f is located at the rear portion in 1 inner cavity of compartment, thereon end face with should
The lower surface of upper plate 1a fastens connection, and the upper surface of lower face and bottom plate 1b, which fasten, to be connected, both lateral sides face respectively with
The interior lateral face of one of this two blocks of side plates of corresponding position fastens connection, there is division plate door 1g thereon.Partition board 1f and back plate 1d
Between channel both sides bottom plate 1b on, storage weapons and ammunitions, tool and engine fuel.Upper plate 1a is rectangle, upper table
There are rear circular hole 1i and preceding circular hole 1j on the longitudinal midline in face, which is located at the surface of partition board 1f, the preceding circular hole 1j again
Positioned at the front of the rear circular hole 1i.Also there are multiple embrasure 1h on the side plate.
As shown in Figure 1, being equipped with camera 2, display screen 3, gasket 15, seat 4, power and control system on compartment 1.
As shown in Figure 1, Figure 3, camera 2 is located at the lateral center of 1 upper surfaces upper plate 1a front end of compartment, with corresponding position
Upper plate 1a be fixedly connected.
As shown in Figure 1, display screen 3 is located at the dead astern of the preceding circular hole 1j on 1 upper plate 1a of compartment and close, suspension
On the lower surface of the upper plate 1a of corresponding position, the scene in the front that camera 2 is shot on the compartment 1 is shown in the display screen
On 3.
As shown in Figure 1, the diameter of circular gasket 15 is less than the transverse width of 1 upper plate 1a of compartment, axis and upper plate 1a
On the axis of rear circular hole 1i overlap, the upper surface of lower disc and corresponding position upper plate 1a fasten connection.The gasket 15
There is vertical gasket circular hole 15a at center, and the internal diameter of gasket circular hole 15a is equal to or more than the internal diameter of the rear circular hole 1i.
As shown in Figure 1, multiple seats 4 fasten on the upper surface of 1 bottom plate 1b of compartment, it is located at 3 rear of display screen
Seat 4 is taken for driver, remaining seat 4 supplies other soldiers rides.
As shown in Figure 1, Figure 3, power and control system are by airscrew engine 8, fagging 9, fluted disc 10, fluted disc axis 11, tooth
Wheel 12, gear shaft 13, steering wheel 14 form.
As shown in Figure 1, Figure 3, connection propeller is fastened on the axis that one of two airscrew engines 8 forward extend out.
As shown in Figure 1, Figure 3, the diameter of fluted disc 10 is equal to the diameter of 1 Upper gasket 15 of compartment, axis and 1 upper plate of compartment
The axis of rear circular hole 1i on 1a overlaps, the upper disc movable contact of lower disc and the gasket 15.The center of the fluted disc 10 has
The axis of fluted disc circular hole 10a, fluted disc circular hole 10a are overlapped with the axis of the fluted disc 10.
As shown in Figure 1, the vertical axial height of fluted disc axis 11 is equal to the vertical thickness of fluted disc 10, gasket 15,1 upper plate 1a of compartment
The sum of degree, outer diameter are equal to the internal diameter of the rear circular hole 1i on upper plate 1a, are inserted in fluted disc circular hole 10a on the fluted disc 10, should
In gasket circular hole 15a, the rear circular hole 1i on gasket 15, fastens and connect with upper plate 1a, and be fixedly connected with the fluted disc 10
Together.The circumferential surface movable contact of the fluted disc axis 11 of its corresponding position of inner circumferential surface of gasket circular hole 15a, or
It is mutually opposed.
As shown in Figure 1, one of two faggings 9 are rectangular slab;The both sides of symmetrical separation 10 axis of fluted disc of this two fagging 9, this two
The lower face of one of fagging 9 and the upper surface of the fluted disc 10 of corresponding position, which fasten, to be connected;This two fagging 9 is located at two spirals
The underface of one of paddle motor 8 center of gravity, the engine-propeller of the upper surface of one of this two fagging 9 and the surface of corresponding position
The lower surface of 8 shell of machine fastens connection.The axis of this two airscrew engine 8 it is parallel and with this two airscrew engines, 8 center of gravity
Line it is vertical.Propeller in the airscrew engine 8 will not collide when rotating with the fluted disc 10.
As shown in Figure 1, Figure 3, the diameter of gear 12 be less than fluted disc 10 diameter, be located at fluted disc 10 front and with the tooth
Disk 10 engages, and vertical axis overlaps with the axis of the preceding circular hole 1j on 1 upper plate 1a of compartment, lower disc and corresponding position this
The upper surface movable contact of upper plate 1a.There is a vertical gear circular hole 12a at the center of the gear 12, the axis of gear circular hole 12a with
The axis of the gear 12 overlaps.
As shown in Figure 1, the diameter of steering wheel 14 is more than the diameter of gear 12, but less than the diameter of fluted disc 10, it is located at vehicle
The lower section of display screen 3 and close to the lower face of the display screen 3 on compartment 1, there is steering wheel circular hole 14a at center.Direction disk circular hole
The axis of 14a is overlapped with the axis of direction disk 14, and internal diameter is equal to the internal diameter of the gear circular hole 12a on gear 12.
As shown in Figure 1, the outer diameter of gear shaft 13 is equal to the internal diameter of the gear circular hole 12a on gear 12, it is inserted in the gear
In circular hole 12a, the preceding circular hole 1j on 1 upper plate 1a of compartment, the steering wheel circular hole 14a on steering wheel 14, fixed with upper plate 1a
Connection, the external part upward from the preceding circular hole 1j link together with the gear 12 fastening, downward from the preceding circular hole 1j
External part links together with the fastening of corresponding position direction disk 14.
As shown in Figure 1 and Figure 2, earthing or grounding means is made of floor 5, cooling fin 6, heat-insulated column 7.
As shown in Figure 1 and Figure 2, the tablet 5a and wraping plate 5b on floor 5 are integral.The bottom plate 1b shapes of tablet 5a and compartment 1
Shape is identical, area equation, is located at the underface of bottom plate 1b.It is laterally wide that the transverse width of wraping plate 5b is equal to tablet 5a
Degree, front end upwarps, lower end with the front end of tablet 5a is round and smooth connects.
As shown in Figure 1 and Figure 2, on the upper surface of the evenly dispersed tablet 5a mounted on floor 5 of polylith cooling fin 6.The heat dissipation
Piece 6 is strip piece, and axis is parallel with the axis of tablet 5a, and longitudinal length is equal to the longitudinal length of tablet 5a,
Rear end face is flushed with the rear end face of tablet 5a, and upper surface is opposed with the lower surface of bottom plate 1b on the compartment 1 of corresponding position
But it does not contact, the upper surface of the tablet 5a of lower surface and corresponding position fastens connection.
As shown in Figure 1 and Figure 2, multiple dispersions of heat-insulated column 7 are on the tablet 5a on floor 5 and the bottom plate 1b in compartment 1.It should
Heat-insulated column 7 is short and small cylinder or polygon prism, is manufactured with heat-insulating material, and vertical axial height is more than the vertical height of cooling fin 6
The upper surface of the tablet 5a of degree, lower face and corresponding position, which fastens, to be connected, thereon under the bottom plate 1b of end face and corresponding position
Surface fastens connection.
The soldier on 1 upper plate 1a of compartment is lain concealed for protection, from top to bottom the lower face of gradual sweptback armour
It fastens and connects with the front end of the upper surface of 1 upper plate 1a of compartment, from top to bottom the lower face of gradual intilted two pieces of armours
It fastens and connects with the upper surface of one of upper plate 1a front part sides respectively, have multiple vertical shooting notches on the armour.
To reinforce the firepower of high speed amphibious landing vehicle, on compartment 1 in addition to having rifle, machine gun, rocket launcher, flame are also had
Injector.
Installation, which is fastened, to protect airscrew engine 8, on the upper surface of 1 upper plate 1a of compartment starts machine protective cover, two spiral shells
Rotation paddle motor 8 is hidden in it.This starts the front end of machine protective cover to have air admission hole, rear end open, from top to bottom by bullet front
It gradually tilts backwards, is gradually sloped inwardly from top to bottom by one of two sides are played.
The method for implementing landing operations using high speed amphibious landing vehicle is such:
After high speed amphibious landing vehicle is transported to debarkation point Its Adjacent Waters by large ship, go out before leaving the large ship,
While naval vessel and aircraft denial of the air are supported, and artillery fire coverage goal, the earth steps and trench in channel are scabbled, channel is destroyed
Barrier ignites the land mine on channel, eliminates channel both sides enemy.Then high speed amphibious landing vehicle drives towards behind debarkation point in high speed
Bank, to remaining unfriendly target come down in torrents bullet, launch a rocket shell, jet flames, rush at rapidly highland eliminate the remnants of the enemy force, it is too late with a sudden peal of thunder
The gesture for covering ear seizes position.
As shown in Figure 1, during traveling, the front situation that driver shows according to display screen 3 selects travel path,
Adjust direction of traffic.When steering wheel 14 rotationally clockwise when, band active toothed disk 10 rotates in an anti-clockwise direction, corresponding propeller hair
Right side is biased in the rear end of motivation 8, and high speed amphibious landing vehicle is made to turn to the right.When steering wheel 14 rotates in an anti-clockwise direction, drive
Rotationally clockwise, left side is biased in the rear end of corresponding airscrew engine 8 to fluted disc 10, and high speed amphibious landing vehicle is made to turn left
To.When the axis of airscrew engine 8 is parallel with the axis in compartment 1, the direction of advance of high speed amphibious landing vehicle is constant.
When more high speed amphibious landing vehicles log in simultaneously, advance in a triangle or laterally a line promotes, finally is needing to account for
Converge on the position of neck.Then large quantities of follow-up unit's follow-ups, consolidate a position, exploit success.
Embodiments of the present invention are explained in detail above in conjunction with attached drawing.The present invention is not limited to above-mentioned embodiment party
Formula, technical field those of ordinary skill within the scope of knowledge, can also be before not departing from present inventive concept
Put that various changes can be made.The various change made without departing from the purpose of the present invention, still falls within the scope of the present invention.
Claims (5)
1. a kind of high speed amphibious landing vehicle, (1) containing compartment;
It is characterized in that:
The high speed amphibious landing vehicle also contains earthing or grounding means;
It is enclosed by one piece of upper plate (1a), one piece of bottom plate (1b), one piece of foreboard (1c), one piece of back plate (1d), two blocks of side plates in compartment (1)
At;The foreboard (1c) gradually tilts backwards from top to bottom, and lower end and the round and smooth fastening in front end of the bottom plate (1b) connect,
On have multiple embrasures (1h);There is car door (1e) on the back plate (1d);Vertical clapboard (1f) is located in the compartment (1) inner cavity
Rear portion, the lower surface of end face and the upper plate (1a), which fastens, thereon connects, the upper surface of lower face and the bottom plate (1b)
Connection is fastened, both lateral sides face fastens with the interior lateral face of one of this two blocks of side plates of corresponding position connect respectively, has thereon
Division plate door (1g);Between the partition board (1f) and the back plate (1d) on the bottom plate (1b) of channel both sides, weapon bullet is stored
Medicine, tool and engine fuel;The upper plate (1a) is rectangle, has rear circular hole (1i) and preceding circle on the longitudinal midline of upper surface
Hole (1j), the rear circular hole (1i) and the surface positioned at partition board (1f), the preceding circular hole (1j) are located at the rear circular hole (1i)
Front;Also there are multiple embrasures (1h) on the side plate;
Camera (2), display screen (3), gasket (15), seat (4), power and control system are installed on compartment (1);
Camera (2) is located at the lateral center of the upper surface front end compartment (1) upper plate (1a), the upper plate with corresponding position
(1a) is fixedly connected;
Display screen (3) is located at the dead astern of the preceding circular hole (1j) on compartment (1) upper plate (1a) and close, is suspended on corresponding
On the lower surface of the upper plate (1a) of position, the scene in the front that camera (2) is shot on the compartment (1) is shown in this and shows
In display screen (3);
The diameter of circular gasket (15) is less than the transverse width of compartment (1) upper plate (1a), on axis and the upper plate (1a)
The axis of circular hole (1i) overlaps afterwards, and the upper surface of lower disc and upper plate (1a) described in corresponding position, which fastens, to be connected;The gasket
(15) center has vertical gasket circular hole (15a), the internal diameter of the gasket circular hole (15a) to be equal to or more than the rear circular hole (1i)
Internal diameter;
Multiple seats (4) fasten on the upper surface of compartment (1) bottom plate (1b), are located at the seat (4) at display screen (3) rear
It is taken for driver, remaining seat (4) supplies other soldiers rides;
Power and control system are by airscrew engine (8), fagging (9), fluted disc (10), fluted disc axis (11), gear (12), gear
Axis (13), steering wheel (14) composition;
Connection propeller is fastened on the axis that one of two airscrew engines (8) forward extend out;
The diameter of fluted disc (10) is equal to the diameter of compartment (1) Upper gasket (15), on axis and the compartment (1) upper plate (1a)
The axis of circular hole (1i) overlaps afterwards, the upper disc movable contact of lower disc and the gasket (15);In the fluted disc (10)
The heart has fluted disc circular hole (10a), the axis of the fluted disc circular hole (10a) to be overlapped with the axis of the fluted disc (10);
The vertical axial height of fluted disc axis (11) be equal to fluted disc (10), gasket (15), compartment (1) upper plate (1a) vertical thickness it
It is equal to the internal diameter of the rear circular hole (1i) on the upper plate (1a), the fluted disc circular hole being inserted on the fluted disc (10) with, outer diameter
In gasket circular hole (15a), the rear circular hole (1i) on (10a), the gasket (15), fastens and connect with the upper plate (1a)
It connects, and is fixed together with the fluted disc (10);The institute of its corresponding position of inner circumferential surface of the gasket circular hole (15a)
State the circumferential surface movable contact or mutually opposed of fluted disc axis (11);
One of two faggings (9) are rectangular slab;This two fagging (9) is symmetrically lived apart the both sides of fluted disc (10) axis, this two fagging (9) it
One lower face and the upper surface of the fluted disc (10) of corresponding position, which fasten, to be connected;This two fagging (9) is located at two spirals
The underface of one of paddle motor (8) center of gravity, the propeller of the upper surface of one of this two fagging (9) and the surface of corresponding position
The lower surface of engine (8) shell fastens connection;The axis of this two airscrew engine (8) it is parallel and with this two engine-propeller
The line of machine (8) center of gravity is vertical;Propeller in the airscrew engine (8) will not be with the fluted disc when rotating
(10) it collides;
The diameter of gear (12) is less than the diameter of fluted disc (10), is located at the front of fluted disc (10) and is nibbled with the fluted disc (10)
It closes, vertical axis is overlapped with the axis of the preceding circular hole (1j) on compartment (1) upper plate (1a), the institute of lower disc and corresponding position
State the upper surface movable contact of upper plate (1a);There are vertical gear circular hole (12a), the gear circular hole in the center of the gear (12)
The axis of (12a) is overlapped with the axis of the gear (12);
The diameter of steering wheel (14) is more than the diameter of gear (12), but less than the diameter of fluted disc (10), is located on compartment (1) and shows
The lower section of display screen (3) and close to the lower face of the display screen (3), there is steering wheel circular hole (14a) at center;The steering wheel circle
The axis in hole (14a) is overlapped with the axis of the steering wheel (14), and internal diameter is equal to the gear circular hole (12a) on gear (12)
Internal diameter;
The outer diameter of gear shaft (13) is equal to the internal diameter of the gear circular hole (12a) on gear (12), is inserted in the gear circular hole
It is and described in the steering wheel circular hole (14a) on preceding circular hole (1j), steering wheel (14) on (12a), compartment (1) upper plate (1a)
Upper plate (1a) is fixedly connected, and the external part upward from the preceding circular hole (1j) links together with the gear (12) fastening,
It links together from steering wheel (14) fastening described in the preceding circular hole (1j) downward external part and corresponding position;
Earthing or grounding means is made of floor (5), cooling fin (6), heat-insulated column (7);
The tablet (5a) and wraping plate (5b) on floor (5) are integral;Bottom plate (1b) shape phase of the tablet (5a) and compartment (1)
Same, area equation is located at the underface of the bottom plate (1b);The transverse width of the wraping plate (5b) is equal to the tablet (5a)
Transverse width, front end upwarp, lower end with the front end of the tablet (5a) is round and smooth connects;
On the upper surface of the evenly dispersed tablet (5a) mounted on floor (5) of polylith cooling fin (6);The cooling fin (6) is length
Strip piece, axis is parallel with the axis of the tablet (5a), and longitudinal length is equal to the longitudinal length of the tablet (5a),
Rear end face is flushed with the rear end face of the tablet (5a), under the bottom plate (1b) on the compartment (1) of upper surface and corresponding position
It opposing surface but does not contact, the upper surface of the tablet (5a) of lower surface and corresponding position fastens connection;
Multiple heat-insulated column (7) dispersions are on the tablet (5a) of floor (5) and the bottom plate (1b) of compartment (1);The heat-insulated column
(7) it is short and small cylinder or polygon prism, is manufactured with heat-insulating material, vertical axial height is more than the vertical height of cooling fin (6),
The upper surface of the tablet (5a) of its lower face and corresponding position fastens connection, thereon under the bottom plate (1b) of end face and corresponding position
Surface fastens connection.
2. according to high speed amphibious landing vehicle described in claim 1, it is characterised in that:
Gradually the front end of the upper surface of the lower face and compartment (1) upper plate (1a) of sweptback armour fastens company from top to bottom
It connects, gradually the lower face of intilted two pieces of armours is upper with one of the upper plate (1a) front part sides respectively from top to bottom
Surface fastens connection, has multiple vertical shooting notches on the armour.
3. according to high speed amphibious landing vehicle described in claim 1, it is characterised in that:
On compartment (1) in addition to having rifle, machine gun, rocket launcher, flame thrower are also had.
4. according to high speed amphibious landing vehicle described in claim 1, it is characterised in that:
Installation is fastened on the upper surface of compartment (1) upper plate (1a) starts machine protective cover, two airscrew engines (8) to hide it
It is interior;It is described that the front end of machine protective cover is started to have air admission hole, rear end open, it is gradually tilted backwards from top to bottom by bullet front,
Gradually sloped inwardly from top to bottom by one of two sides are played.
5. the method using high speed amphibious landing vehicle described in claim 1 is such:
After high speed amphibious landing vehicle is transported to debarkation point Its Adjacent Waters by large ship, go out before leaving the large ship, simultaneously
Support naval vessel and aircraft denial of the air, and artillery fire coverage goal, the earth steps and trench in channel are scabbled, the obstacle in channel is destroyed
Object ignites the land mine on channel, eliminates channel both sides enemy;Then high speed amphibious landing vehicle debarks at a high speed after driving towards debarkation point,
To remaining unfriendly target come down in torrents bullet, launch a rocket shell, jet flames, rush at highland rapidly and eliminate the remnants of the enemy force, with a sudden peal of thunder not as good as covering
The gesture of ear seizes position;
During traveling, the front situation that driver shows according to display screen (3) selects travel path, adjusts direction of traffic;
When steering wheel (14) rotationally clockwise when, band active toothed disk (10) rotate in an anti-clockwise direction, corresponding airscrew engine (8)
Right side is biased in rear end, and high speed amphibious landing vehicle is made to turn to the right;When steering wheel (14) rotates in an anti-clockwise direction, band active toothed disk
(10) rotationally clockwise, left side is biased in the rear end of corresponding airscrew engine (8), and high speed amphibious landing vehicle is made to turn left
To;When the axis of airscrew engine (8) is parallel with the axis of compartment (1), the direction of advance of high speed amphibious landing vehicle is constant;
When more high speed amphibious landing vehicles log in simultaneously, advance in a triangle or laterally a line promotes, is finally captured in needs
Converge on position;Then large quantities of follow-up unit's follow-ups, consolidate a position, exploit success.
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CN201611174308.3A CN106515330B (en) | 2016-12-12 | 2016-12-12 | High speed amphibious landing vehicle |
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CN201611174308.3A CN106515330B (en) | 2016-12-12 | 2016-12-12 | High speed amphibious landing vehicle |
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CN106515330B true CN106515330B (en) | 2018-11-06 |
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4407215A (en) * | 1981-12-14 | 1983-10-04 | Cyr Reno R J | Unique fan-powered water vessel |
CN85106060A (en) * | 1985-01-24 | 1986-07-23 | 昌维奥·简·克劳德 | Link assembled by combining two junk and make the device of land seagoing vessel |
US4669408A (en) * | 1985-07-29 | 1987-06-02 | Schad Robert D | Amphibious jet powered craft |
JPS63154411A (en) * | 1986-12-18 | 1988-06-27 | Mitsubishi Heavy Ind Ltd | Amphibious submarine boat |
CN103879251A (en) * | 2012-12-24 | 2014-06-25 | 孙学军 | Amphibious snow boat |
CN106004283A (en) * | 2016-07-13 | 2016-10-12 | 西藏长源动力科技有限公司 | Offensive fire-support unmanned ship for amphibious landing operation |
CN106081038A (en) * | 2016-08-19 | 2016-11-09 | 抚顺抚运安仪救生装备有限公司 | A kind of double double oar air ships |
-
2016
- 2016-12-12 CN CN201611174308.3A patent/CN106515330B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4407215A (en) * | 1981-12-14 | 1983-10-04 | Cyr Reno R J | Unique fan-powered water vessel |
CN85106060A (en) * | 1985-01-24 | 1986-07-23 | 昌维奥·简·克劳德 | Link assembled by combining two junk and make the device of land seagoing vessel |
US4669408A (en) * | 1985-07-29 | 1987-06-02 | Schad Robert D | Amphibious jet powered craft |
JPS63154411A (en) * | 1986-12-18 | 1988-06-27 | Mitsubishi Heavy Ind Ltd | Amphibious submarine boat |
CN103879251A (en) * | 2012-12-24 | 2014-06-25 | 孙学军 | Amphibious snow boat |
CN106004283A (en) * | 2016-07-13 | 2016-10-12 | 西藏长源动力科技有限公司 | Offensive fire-support unmanned ship for amphibious landing operation |
CN106081038A (en) * | 2016-08-19 | 2016-11-09 | 抚顺抚运安仪救生装备有限公司 | A kind of double double oar air ships |
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Effective date of registration: 20201127 Address after: Block b-1-5-2, chonglan Industrial Park, Dongxing City, Fangchenggang City, Guangxi Zhuang Autonomous Region Patentee after: Guangxi Dongxing Jianye kitchenware Manufacturing Co., Ltd Address before: Seven road 528437 in Guangdong Province, Zhongshan Torch Development Zone No. 113 fraternity homes 1 building 1407 room Lily Patentee before: Li Xinya |
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