CN108750085A - 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
- Publication number
- CN108750085A CN108750085A CN201810873600.7A CN201810873600A CN108750085A CN 108750085 A CN108750085 A CN 108750085A CN 201810873600 A CN201810873600 A CN 201810873600A CN 108750085 A CN108750085 A CN 108750085A
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- Prior art keywords
- rotor
- fuselage
- shell
- unmanned plane
- lower rotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000003814 drug Substances 0.000 title claims abstract description 13
- 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 3
- 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
- 239000000203 mixture Substances 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000003721 gunpowder Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C27/50—Blades foldable to facilitate stowage of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of attack unmanned planes using Terminal Sensitive Projectile medicine, including：Coaxial twin screw, fuselage and the shell being made of with lower rotor upper rotor, 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 is hinged with rotation axis with the lower rotor, 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, and the shell is covered in the fuselage outer surface.The present invention saves the power attenuation 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 present invention relates to air vehicle technique fields, and in particular to a kind of attack unmanned plane using Terminal Sensitive Projectile medicine.
Background technology
Terminal Sensitive Projectile medicine (referred to as " Terminal munition ") is one kind in Trajectory-terminal detection target location and distance and can make war
The sophisticated weapon that pan is exploded towards target direction.
In general, after the transmitting of Terminal munition mother's bullet or projectile, cast into the fuze actuation that is delayed when 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 will search for target with sensor system, confirm the current height of 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.
Invention content
In order to solve above-mentioned the deficiencies in the prior art, the present invention provides a kind of attack using Terminal Sensitive Projectile medicine nobody
Machine is laid out using coaxial anti-paddle, has foldable blade, can be Terminal munition be provided before discharge warhead certain movement and
Floating ability improves Operational Effectiveness Rat.
In order to achieve the above object, the technical solution adopted by the present invention is：
A kind of attack unmanned plane using Terminal Sensitive Projectile medicine, including：The coaxial double spiral shells being made of with lower rotor upper 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 are hinged with rotation axis, the fuselage be equipped with power with
Energy module, flight control modules and detection connect the coaxial double helix with fight module, the power with energy module
Paddle, the power is separately connected the flight control modules with energy module, the detection is 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 further description of the present invention, the shell is a kind of hollow shell case, by cambered surface shell one and cambered surface shell
Two connection compositions.
To further description of the present invention, the cambered surface shell one is equipped with micro fried with two junction of cambered surface shell
Medicine.
To further description of the present invention, attitude transducer and the connection detection are additionally provided in the flight control modules
With fight module.
Compared with prior art, advantages of the present invention：Coaxial twin screw is different from conventional single-blade disk helicopter, blade rotation
The torque meeting for changing the line of production raw is because upper and lower paddle disk being rotated backward and being cancelled out each other, therefore need not additionally configure tail-rotor to balance this
Torsional moment, meanwhile, it can also save the power attenuation that engine exports tail-rotor.In addition, because upper and lower two sets of paddle disks carry simultaneously
For lift, therefore rotor disk area required under same lift is much smaller than the area of single-blade disk, and aircraft overall dimensions are more compact, save
The coaxial twin-propeller blade in space is foldable, can also be unfolded in the air；The expansion of blade can be used and be not limited to use steering engine
The modes such as turning gear wheel disc or spring restoring force；In the unmanned plane initial velocity for giving blade folded state, smaller windward side
Product can reduce the loss of initial velocity, make unmanned plane can be with fast approaching target area.The unmanned plane exhibition close to after target area
Rotor blade is opened, the increase of one side rotor disk area can hold position when unmanned plane can be made to slow down to reach target area and be controlled
System flight or hovering, another aspect forward flight speed can make propeller spin generate certain initial lift, i.e. rotor at this time
Transmission can disconnect with engine or engine is only needed to provide a small amount of output.Power outputs power to two sets up and down with energy module
Propeller makes its rotation generate lift, ensures that unmanned plane can hover and fly；Attitude transducer built in flight control modules,
Unmanned plane during flying state can be adjusted according to the target information that attitude transducer and detection are provided with fight module；Detection and fight
Module may include one or more warheads, and when flight control system control unmanned plane reaches target overhead, release warhead is to target
It is attacked.Bullet shape shell is closed up by least two panels cambered surface shell to be formed, and is mutually fastened by engaging portion between each cambered surface shell.Knot
Conjunction portion can be used and be not limited to release the modes such as bolt limitation or the destruction of micro gunpowder using steering engine, release the fastening shape of engaging portion
State makes to detach between cambered surface shell, to release unmanned plane.Shell can be protected in initial acceleration and high-speed flight stage
Protect unmanned plane structure, reduce its contacted with emitter or high-speed flow and the loss or destruction that generate, in addition smooth shell
High-speed flight is improved with aerodynamic drag when shape shape can greatly reduce high-speed flight, reduction initial acceleration energy consumption is played in surface
Efficiency.Can be provided in a manner of it terrestrial gun can be used to penetrate or cast in the air etc. the initial flight speed of unmanned plane with close to target side
To trajectory.
Description of the drawings
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 sections.
Fig. 4 is application scenarios schematic diagram of the present invention in embodiment described herein.
Specific implementation mode
Below in conjunction with attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that is retouched
The embodiment stated is only a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, originally
The every other embodiment that field those of ordinary skill is obtained without creative efforts, belongs to the present invention
The range of protection.
Embodiment 1, as shown in Figures 1 to 4：
A kind of attack unmanned plane using Terminal Sensitive Projectile medicine, including：Coaxial pair be made of with lower rotor 2 upper rotor 1
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 is hinged with rotation axis with lower rotor 3, 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, unmanned plane is launched 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 detach, 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 one is obtained with propeller spin while unmanned plane reduces speed now
Part lift；Flight control modules 32 make unmanned plane hold position and subtract by rotor on active accommodation 1 and the rotation of 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 location 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 invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Profit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent requirements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.
Claims (4)
1. a kind of attack unmanned plane using Terminal Sensitive Projectile medicine, including：The coaxial double helix being made of with lower rotor upper 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 is hinged with rotation axis with the lower rotor, 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 is equipped with trace explosive with two junction of cambered surface shell.
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 |
|---|---|---|---|
| CN201810873600.7A CN108750085A (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 |
|---|---|---|---|
| CN201810873600.7A CN108750085A (en) | 2018-08-02 | 2018-08-02 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108750085A true CN108750085A (en) | 2018-11-06 |
Family
ID=63968816
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810873600.7A Withdrawn CN108750085A (en) | 2018-08-02 | 2018-08-02 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108750085A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109405649A (en) * | 2018-11-12 | 2019-03-01 | 彩虹无人机科技有限公司 | The foldable coaxial anti-paddle unmanned plane of one kind and striking method |
| CN109552596A (en) * | 2018-11-29 | 2019-04-02 | 江苏鸿鹄无人机应用科技有限公司 | It is a kind of can be with the unmanned plane of stabilized flight |
| CN110127037A (en) * | 2019-06-09 | 2019-08-16 | 西北工业大学 | A kind of cylindric vertically taking off and landing flyer using foldable single screw and grid fin |
| CN110889172A (en) * | 2019-12-04 | 2020-03-17 | 中国直升机设计研究所 | Method for prefabricating impact damage of helicopter rotor system |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2175626C2 (en) * | 1999-12-17 | 2001-11-10 | Кириллов Андрей Порфирьевич | Flying vehicle for destruction of object (versions) |
| US20140147277A1 (en) * | 2012-11-26 | 2014-05-29 | Tadashi Iwata | Rotor blade system for helicopter |
| CN104691748A (en) * | 2013-12-04 | 2015-06-10 | 中国直升机设计研究所 | Gun-launched unmanned helicopter and expansion method thereof |
| CN106864744A (en) * | 2015-12-11 | 2017-06-20 | 中国航空工业集团公司成都飞机设计研究所 | A kind of co-axial rotor variant vertically taking off and landing flyer |
| RU2628351C1 (en) * | 2016-04-14 | 2017-08-16 | Сергей Николаевич ПАВЛОВ | Anti-tank mine "strekosa-m" with possibility of spatial movement with hovering and reversibility in air, reconnaissance, neutralisation, and damage of mobile armoured targets |
| CN209396038U (en) * | 2018-08-02 | 2019-09-17 | 西安君晖航空科技有限公司 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
-
2018
- 2018-08-02 CN CN201810873600.7A patent/CN108750085A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2175626C2 (en) * | 1999-12-17 | 2001-11-10 | Кириллов Андрей Порфирьевич | Flying vehicle for destruction of object (versions) |
| US20140147277A1 (en) * | 2012-11-26 | 2014-05-29 | Tadashi Iwata | Rotor blade system for helicopter |
| CN104691748A (en) * | 2013-12-04 | 2015-06-10 | 中国直升机设计研究所 | Gun-launched unmanned helicopter and expansion method thereof |
| CN106864744A (en) * | 2015-12-11 | 2017-06-20 | 中国航空工业集团公司成都飞机设计研究所 | A kind of co-axial rotor variant vertically taking off and landing flyer |
| RU2628351C1 (en) * | 2016-04-14 | 2017-08-16 | Сергей Николаевич ПАВЛОВ | Anti-tank mine "strekosa-m" with possibility of spatial movement with hovering and reversibility in air, reconnaissance, neutralisation, and damage of mobile armoured targets |
| CN209396038U (en) * | 2018-08-02 | 2019-09-17 | 西安君晖航空科技有限公司 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109405649A (en) * | 2018-11-12 | 2019-03-01 | 彩虹无人机科技有限公司 | The foldable coaxial anti-paddle unmanned plane of one kind and striking method |
| CN109552596A (en) * | 2018-11-29 | 2019-04-02 | 江苏鸿鹄无人机应用科技有限公司 | It is a kind of can be with the unmanned plane of stabilized flight |
| CN110127037A (en) * | 2019-06-09 | 2019-08-16 | 西北工业大学 | A kind of cylindric vertically taking off and landing flyer using foldable single screw and grid fin |
| CN110889172A (en) * | 2019-12-04 | 2020-03-17 | 中国直升机设计研究所 | Method for prefabricating impact damage of helicopter rotor system |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181106 |