CN206344997U - A kind of low latitude investigation depopulated helicopter - Google Patents
A kind of low latitude investigation depopulated helicopter Download PDFInfo
- Publication number
- CN206344997U CN206344997U CN201621234365.1U CN201621234365U CN206344997U CN 206344997 U CN206344997 U CN 206344997U CN 201621234365 U CN201621234365 U CN 201621234365U CN 206344997 U CN206344997 U CN 206344997U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- tail
- oar
- nylon
- deck store
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model discloses a kind of low latitude investigation depopulated helicopter, including nose shell, undercarriage, electronic jamming device, nylon oar, wing drop device, high-definition camera, tailplane, vertical tail, tail-rotor, tail rotor driving shafts, deck store, searchlight, fuselage；It is provided with before the fuselage below nose shell, fuselage and is connected with undercarriage, fuselage left surface has even been provided with electronic jamming device, fuselage right flank, which is provided with above searchlight, fuselage, is provided with nylon oar, and high-definition camera is provided with above nylon oar；It is provided with behind the fuselage inside deck store, deck store and is provided with tail rotor driving shafts, deck store side is connected with tailplane, and deck store afterbody is connected with vertical tail, and tail-rotor.Pneumatic efficiency height during the utility model flight, flight safety are stable.
Description
Technical field
The utility model is related to helicopter field, and in particular to a kind of low latitude investigation depopulated helicopter.
Background technology
Reconnaissance helicopter is as reconnaissance plane, to serve as information and the military machine of gather material.Reconnaissance helicopter is served as
Closely the either information gathering work of infighting Performance Area, as Tactical Reconnaissance Aircraft, mainly serves as military's support
Zhen Search roles.Information and gather material, reconnaissance helicopter are carried out because helicopter can hover over the undetectable place of enemy
It is still one of main information and the military machine of gather material now.
Utility model content
In view of the shortcomings of the prior art, pneumatic efficiency when the purpose of this utility model is to provide a kind of flight is high, winged
The low latitude investigation depopulated helicopter of row safety and stability.
In order to realize above-mentioned purpose, the technical solution adopted in the utility model：A kind of low latitude investigation depopulated helicopter, bag
Include nose shell, undercarriage, electronic jamming device, nylon oar, wing drop device, high-definition camera, tailplane, vertical tail,
Tail-rotor, tail rotor driving shafts, deck store, searchlight, fuselage；It is provided with before the fuselage below nose shell, fuselage and is connected with undercarriage,
Fuselage left surface has even been provided with electronic jamming device, and fuselage right flank, which is provided with above searchlight, fuselage, is provided with nylon oar, Buddhist nun
High-definition camera is provided with above imperial oar；Deck store is provided with behind the fuselage, tail rotor driving shafts are provided with inside deck store, deck store side with
Tailplane is connected, and deck store afterbody is connected with vertical tail, and tail-rotor.
Further, wing drop device is provided with above the fuselage, wing drop device is connected with nylon oar；
Further, the undercarriage is damping undercarriage；
Further, the nylon oar is glass fiber reinforced nylon oar.
The beneficial effects of the utility model are:
The utility model is provided with damping undercarriage, and aircraft, be with ground sharp impacts in touchdown；Taking off,
In landing, because ground is uneven, also can with ground collision, by provided with damping undercarriage, it is possible to reduce four axle unmanned vehicles
The impact being subject to during landing, it is to avoid produce strong bounce of jolting, this is all extremely advantageous to aircaft configuration and flight safety；Glass
Fiber reinforced nylon tensile strength of material is high, extending small, coefficient of elasticity, high, rigidity is good, therefore apparatus with shock absorbing is big.Glass is tieed up
Inorfil, with noninflammability, chemical resistance is good, yardstick stability, heat resistance are good, good insulating, and corrosion resistance is good, resistance to fall
Ability is strong, high-speed deformation is small, efficiency high, fast response time the advantages of, blade use glass fiber net nylon blade, can effectively improve winged
Pneumatic efficiency during row；The instruction of flight control assemblies can be converted to rotor blade controlled motion by wing drop device, because
Rotor is rotation, and the instruction that auto-bank unit be used to send flight control assemblies is delivered to rotation from non-rotary fuselage
Blade, the flight of aircraft is more stablized.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the accompanying drawing used required in description of the prior art is briefly described：
Fig. 1 is structural representation of the present utility model.
Drawing reference numeral is：1- nose shells；2- undercarriages；3- electronic jamming devices；4- nylon oars；5- wing drop devices；
6- high-definition cameras；7- tailplanes；8- vertical tail,s；9- tail-rotors；10- tail rotor driving shafts；11- deck stores；12- searchlights；13- machines
Body.
Embodiment
Refering to a kind of low latitude investigation depopulated helicopter shown in the drawings, including nose shell 1, undercarriage 2, electronic jamming device
3rd, nylon oar 4, wing drop device 5, high-definition camera 6, tailplane 7, vertical tail, 8, tail-rotor 9, tail rotor driving shafts 10, deck store
11st, searchlight 12, fuselage 13；The fuselage 13 is above provided with nose shell 1, and fuselage 13 is connected with undercarriage 2 below, and fuselage 13 is left
Side, which connects, is provided with electronic jamming device 3, and the right flank of fuselage 13 is provided with searchlight 12, and fuselage 13 is provided with nylon oar 4, Buddhist nun above
Imperial oar 4 is provided with high-definition camera 6 above；The fuselage 13 is provided with deck store 11 below, and the inside of deck store 11 is provided with tail rotor driving shafts 10,
The side of deck store 11 is connected with tailplane 7, and the afterbody of deck store 11 is connected with vertical tail, 8 and tail-rotor 9.
On above-described embodiment preferably, the fuselage 13 is provided with wing drop device 5, wing drop device 5 and Buddhist nun above
Imperial oar 4 is connected；
On above-described embodiment preferably, the undercarriage 2 is damping undercarriage；
On above-described embodiment preferably, the nylon oar 4 is glass fiber reinforced nylon oar.
Using such scheme, obtaining the beneficial effects of the utility model is:The utility model is provided with damping undercarriage, flight
Device, be with ground sharp impacts in touchdown；In taking off, landing, because ground is uneven, it can also lead to ground collision
Cross provided with damping undercarriage, it is possible to reduce the impact that four axle unmanned vehicles are subject to when landing, it is to avoid produce strong jolt
Bounce, this is all extremely advantageous to aircaft configuration and flight safety；Glass fiber reinforcement nylon material tensile strength is high, extend small, bullet
Property coefficient is high, rigidity is good, therefore apparatus with shock absorbing is big.Glass dimension is inorfil, and with noninflammability, chemical resistance is good, yardstick
Stability, heat resistance are good, good insulating, and corrosion resistance is good, and the resistance to ability of falling is strong, high-speed deformation is small, efficiency high, fast response time
The advantages of, blade uses glass fiber net nylon blade, can effectively improve pneumatic efficiency during flight；Wing drop device will can fly
The instruction of control device is converted to rotor blade controlled motion, because rotor is rotation, auto-bank unit be used to fly
The instruction that control device is sent is delivered to the blade of rotation from non-rotary fuselage, the flight of aircraft is more stablized.
It is described above, embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Therefore, protection domain of the present utility model should be determined by the scope of protection defined in the claims.
Claims (4)
1. a kind of low latitude investigation depopulated helicopter, including nose shell, undercarriage, electronic jamming device, nylon oar, wing drop dress
Put, high-definition camera, tailplane, vertical tail, tail-rotor, tail rotor driving shafts, deck store, searchlight, fuselage；It is characterized in that：Institute
State to be provided with below nose shell, fuselage before fuselage and be connected with undercarriage, fuselage left surface has even been provided with electronic jamming device, machine
Body right flank, which is provided with above searchlight, fuselage, is provided with nylon oar, and high-definition camera is provided with above nylon oar；Behind the fuselage
Provided with deck store, tail rotor driving shafts are provided with inside deck store, deck store side be connected with tailplane, deck store afterbody be connected with vertical tail, with
Tail-rotor.
2. a kind of low latitude investigation depopulated helicopter according to claim 1, it is characterised in that：It is provided with certainly above the fuselage
Dynamic tilting gearing, wing drop device is connected with nylon oar.
3. a kind of low latitude investigation depopulated helicopter according to claim 1, it is characterised in that：The undercarriage rises for damping
Fall frame.
4. a kind of low latitude investigation depopulated helicopter according to claim 1, it is characterised in that：The nylon oar is tieed up for glass
Strengthen nylon oar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621234365.1U CN206344997U (en) | 2016-11-17 | 2016-11-17 | A kind of low latitude investigation depopulated helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621234365.1U CN206344997U (en) | 2016-11-17 | 2016-11-17 | A kind of low latitude investigation depopulated helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206344997U true CN206344997U (en) | 2017-07-21 |
Family
ID=59320706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621234365.1U Expired - Fee Related CN206344997U (en) | 2016-11-17 | 2016-11-17 | A kind of low latitude investigation depopulated helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206344997U (en) |
-
2016
- 2016-11-17 CN CN201621234365.1U patent/CN206344997U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170721 Termination date: 20201117 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |