CN209396038U - A kind of attack unmanned plane using Terminal Sensitive Projectile medicine - Google Patents
A kind of attack unmanned plane using Terminal Sensitive Projectile medicine Download PDFInfo
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- CN209396038U CN209396038U CN201821240997.8U CN201821240997U CN209396038U CN 209396038 U CN209396038 U CN 209396038U CN 201821240997 U CN201821240997 U CN 201821240997U CN 209396038 U CN209396038 U CN 209396038U
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- rotor
- fuselage
- shell
- unmanned plane
- lower rotor
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- 239000003814 drug Substances 0.000 title claims abstract description 12
- 238000001514 detection method Methods 0.000 claims abstract description 13
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000002360 explosive Substances 0.000 claims description 4
- 230000001133 acceleration Effects 0.000 abstract description 3
- 238000005265 energy consumption Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000006378 damage Effects 0.000 description 3
- 238000005266 casting Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000003721 gunpowder Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses a kind of attack unmanned planes using Terminal Sensitive Projectile medicine, it include: the coaxial twin screw being made of upper rotor with lower rotor, fuselage and shell, the upper rotor is connect by rotation axis with the fuselage with the lower rotor, the upper rotor is opposite with the lower rotor rotation direction, the upper rotor and the lower rotor and rotation axis are hinged, the fuselage is equipped with power and energy module, flight control modules and detection and fight module, the upper rotor is folded to fuselage side by rotary shaft, the lower rotor is folded to the fuselage other side by rotary shaft, the shell is covered in the fuselage outer surface.The utility model saves the power loss that engine exports tail-rotor, reduces the loss of initial velocity, makes unmanned plane that can be reduced initial acceleration energy consumption with fast approaching target area, be improved high-speed flight efficiency.
Description
Technical field
The utility model relates to air vehicle technique fields, and in particular to a kind of attack using Terminal Sensitive Projectile medicine nobody
Machine.
Background technique
Terminal Sensitive Projectile medicine (referred to as " Terminal munition ") be it is a kind of Trajectory-terminal detection target position with apart from and can make to fight
The sophisticated weapon that pan is exploded towards target direction.
In general, Terminal munition mother's bullet transmitting or after casting, delay fuze actuation is cast when into uncontrolled Trajectory-terminal
Device casts out Terminal munition bullet, and Terminal munition bullet itself slows down and subtracts cyclone start-up operation, it is made to hold position and direction
To fall vertically, while the scanning of Terminal munition bullet and sensor system will search for the current height of target, confirmation bullet
And at a distance from target, reached a certain level when bullet height and at a distance from target, bullet warhead, which will explode, to carry out pair
The attack of target.
Terminal munition is lower compared to missile cost, has many advantages, such as that hit probability is high, damage effectiveness is good, but Terminal munition bullet is certainly
Body locomotivity is limited, needs female bullet to cast a large amount of bullet and is scanned attack within the scope of one, is not casting covering model
It encloses or just target can not effectively be attacked not in bullet scanning range.
Utility model content
In order to solve above-mentioned the deficiencies in the prior art, the utility model provides a kind of attack using Terminal Sensitive Projectile medicine
Unmanned plane is laid out using coaxial anti-paddle, has foldable blade, can provide certain shifting before discharging warhead for Terminal munition
Dynamic and floating ability improves Operational Effectiveness Rat.
In order to achieve the above object, the technical solution adopted in the utility model are as follows:
A kind of attack unmanned plane using Terminal Sensitive Projectile medicine, comprising: the coaxial double spiral shells being made of upper rotor with lower rotor
Rotation paddle, fuselage and shell, the upper rotor are connect by rotation axis with the fuselage with the lower rotor, the upper rotor and
The lower rotor rotation direction on the contrary, the upper rotor and the lower rotor and rotation axis are hinged, the fuselage be equipped with power with
Energy module, flight control modules and detection connect the coaxial double helix with energy module with fight module, the power
Paddle, the power are separately connected the flight control modules, the detection with energy module and connect with fight module, the upper rotation
The wing is folded to fuselage side by rotary shaft, and the lower rotor is folded to the fuselage other side, the shell by rotary shaft
It is covered in the fuselage outer surface.
To the utility model further description, the shell is a kind of hollow shell case, by cambered surface shell one and cambered surface
The connection composition of shell two.
To the utility model further description, the cambered surface shell one is equipped with micro with two junction of cambered surface shell
Explosive.
To the utility model further description, it is additionally provided in the flight control modules described in attitude transducer and connection
Detection and fight module.
Compared with prior art, the advantages of the utility model: coaxial twin screw is different from conventional single-blade disk helicopter, paddle
The torque that leaf rotation generates can not need additionally to configure tail-rotor because upper and lower paddle disk is rotated backward and cancelled out each other with flat
Weigh the torsional moment, meanwhile, the power loss that engine exports tail-rotor can also be saved.In addition, because upper and lower two sets of paddle disks are same
When lift is provided, therefore under same lift needed for rotor disk area be much smaller than the area of single-blade disk, aircraft overall dimensions are more compact,
It is foldable to save the coaxial twin-propeller blade in space, can also be unfolded in the sky；The expansion of blade can be used and be not limited to using
The modes such as steering engine turning gear wheel disc or spring restoring force；It is lesser to meet in the unmanned plane initial velocity for giving blade folded state
Wind area can reduce the loss of initial velocity, make unmanned plane can be with fast approaching target area.Close to after target area nobody
Machine be unfolded rotor blade, the increase of one side rotor disk area can hold position when unmanned plane can be made to slow down to reach target area into
Row control flight or hovering, another aspect forward flight speed can make propeller spin generate certain initial lift, i.e., revolve at this time
The transmission of the wing can disconnect with engine or engine is only needed to provide a small amount of output.Power and energy module output power to up and down
Two sets of propellers make its rotation generate lift, guarantee that unmanned plane can hover and fly；Posture built in flight control modules senses
Device can adjust unmanned plane during flying state according to the target information that attitude transducer and detection are provided with fight module；Detection with
Module of fighting may include one or more warheads, discharge warhead pair when flight control system control unmanned plane reaches target overhead
Target is attacked.Bullet shape shell is closed up by least two panels cambered surface shell to be formed, mutually tight by engaging portion between each cambered surface shell
Gu.Engaging portion can be used and be not limited to be released the modes such as bolt limitation or the destruction of micro gunpowder using steering engine, and engaging portion is released
Tightening state makes to separate between cambered surface shell, so that unmanned plane be released.Shell can be in initial acceleration and high-speed flight
Stage protects unmanned plane structure, reduces its loss or destruction for contacting and generating with emitter or high-speed flow, in addition smooth
Case surface and the aerodynamic drag that plays shape shape when can greatly reduce high-speed flight, reduce initial acceleration energy consumption, improve it is high
Fast flight efficiency.The initial flight speed of unmanned plane and close can be provided in a manner of it terrestrial gun can be used to penetrate or cast in the air etc.
The trajectory of target direction.
Detailed description of the invention
Fig. 1 is that unmanned plane of the present invention constitutes schematic diagram.
Fig. 2 is that unmanned plane of the present invention folding blade is placed in the schematic diagram in shell.
Fig. 3 is partial schematic diagram of the shell engaging portion of the present invention under A-A section.
Fig. 4 is application scenarios schematic diagram of the present invention in embodiment described herein.
Specific embodiment
Below in conjunction with attached drawing, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that
The described embodiments are only a part of the embodiments of the utility model, instead of all the embodiments.Based on the utility model
In embodiment, every other implementation obtained by those of ordinary skill in the art without making creative efforts
Example, fall within the protection scope of the utility model.
Embodiment 1, as shown in Figures 1 to 4:
A kind of attack unmanned plane using Terminal Sensitive Projectile medicine, comprising: coaxial pair be made of upper rotor 1 with lower rotor 2
The coaxial twin screw of propeller, fuselage 3 and shell 4, upper rotor 1 are connect by rotation axis with fuselage 3 with lower rotor 2, upper rotation
For the wing 1 with lower 2 rotation direction of rotor on the contrary, upper rotor 1 and lower rotor 3 and rotation axis are hinged, fuselage 3 is equipped with power and energy module
31, flight control modules 32 and detection and fight module 33, power and energy module 31 connect coaxial twin screw, power and
Energy module 31 is separately connected flight control modules 32, detection is connect with fight module 33, and upper rotor 1 is folded to by rotary shaft
3 side of fuselage, lower rotor 2 are folded to 3 other side of fuselage by rotary shaft, and shell 4 is covered in 3 outer surface of fuselage.
A kind of optimal technical scheme of the present embodiment, shell is a kind of hollow shell case, by cambered surface shell 1 and cambered surface
The connection composition of shell 2 42.
A kind of optimal technical scheme of the present embodiment, cambered surface shell 1 are micro equipped with 43 with 2 42 junction of cambered surface shell
Explosive.
A kind of optimal technical scheme of the present embodiment is additionally provided with attitude transducer and connection detection in flight control modules 32
With fight module 33.
In the present embodiment, aircraft carrying lift-off is played by taking, launches unmanned plane when close to target area；Unmanned plane via
It is uncontrolled jettisoning trajectory approaching target overhead when, time-delay fuze start shell 4 built in trace explosive 43 detonate, destroy cambered surface
Engaging portion between shell 1 and cambered surface shell 42, shell 4 separate, and discharge unmanned plane, and subsequent unmanned plane rotor 1 and 2 is unfolded,
Unmanned plane entirety front face area increases, and suffered resistance increases, and obtains one with propeller spin while unmanned plane reduces speed now
Part lift；Flight control modules 32 make unmanned plane hold position and subtract by the rotation of rotor 1 on active accommodation and lower rotor 2
Speed to hovering flight state, detection starts with fight module 33, retrieves the target on periphery；Unmanned plane retrieves the position letter of target
Breath or through preset track flight to target position overhead, confirm the height of unmanned plane and at a distance from target after, release fight
Portion attacks target.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model
Protection scope within.
Claims (4)
1. a kind of attack unmanned plane using Terminal Sensitive Projectile medicine, comprising: the coaxial double helix being made of upper rotor with lower rotor
The coaxial twin screw of paddle, fuselage and shell, which is characterized in that the coaxial twin screw is made of upper rotor and lower rotor,
The upper rotor is connect by rotation axis with the fuselage with the lower rotor, the upper rotor and the lower rotor rotation direction
On the contrary, the upper rotor and the lower rotor and rotation axis are hinged, the fuselage is equipped with power and energy module, flight control mould
Block and detection and fight module, the power connect the coaxial twin screw, the power and energy mould with energy module
Block is separately connected the flight control modules, the detection is connect with fight module, and the upper rotor is folded to by rotary shaft
Fuselage side, the lower rotor are folded to the fuselage other side by rotary shaft, and the shell is covered in the fuselage appearance
Face.
2. a kind of attack unmanned plane using Terminal Sensitive Projectile medicine according to claim 1, which is characterized in that the shell
It is a kind of hollow shell case, is connect and formed with cambered surface shell two by cambered surface shell one.
3. a kind of attack unmanned plane using Terminal Sensitive Projectile medicine according to claim 2, which is characterized in that the cambered surface
Shell one and two junction of cambered surface shell are equipped with trace explosive.
4. a kind of attack unmanned plane using Terminal Sensitive Projectile medicine according to claim 2, which is characterized in that the flight
Attitude transducer and the connection module that detects and fight are additionally provided in control module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821240997.8U CN209396038U (en) | 2018-08-02 | 2018-08-02 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821240997.8U CN209396038U (en) | 2018-08-02 | 2018-08-02 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209396038U true CN209396038U (en) | 2019-09-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821240997.8U Active CN209396038U (en) | 2018-08-02 | 2018-08-02 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
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| CN (1) | CN209396038U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750085A (en) * | 2018-08-02 | 2018-11-06 | 西安君晖航空科技有限公司 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
| CN111156865A (en) * | 2020-01-07 | 2020-05-15 | 北京理工大学 | Coaxial multi-rotor patrol missile |
| CN113086170A (en) * | 2021-04-23 | 2021-07-09 | 北京航空航天大学 | Distributed coaxial ducted power system and aircraft comprising same |
-
2018
- 2018-08-02 CN CN201821240997.8U patent/CN209396038U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750085A (en) * | 2018-08-02 | 2018-11-06 | 西安君晖航空科技有限公司 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
| CN111156865A (en) * | 2020-01-07 | 2020-05-15 | 北京理工大学 | Coaxial multi-rotor patrol missile |
| CN113086170A (en) * | 2021-04-23 | 2021-07-09 | 北京航空航天大学 | Distributed coaxial ducted power system and aircraft comprising same |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: An attack UAV using terminal sensitive ammunition Effective date of registration: 20211108 Granted publication date: 20190917 Pledgee: Xi'an investment and financing Company limited by guarantee Pledgor: XI'AN JUNHUI AVIATION TECHNOLOGY CO.,LTD. Registration number: Y2021610000312 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20221205 Granted publication date: 20190917 Pledgee: Xi'an investment and financing Company limited by guarantee Pledgor: XI'AN JUNHUI AVIATION TECHNOLOGY CO.,LTD. Registration number: Y2021610000312 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: An attack drone using terminal sensitive ammunition Effective date of registration: 20231020 Granted publication date: 20190917 Pledgee: Pudong Development Bank of Shanghai Limited by Share Ltd. Xi'an branch Pledgor: XI'AN JUNHUI AVIATION TECHNOLOGY CO.,LTD. Registration number: Y2023980062077 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |