CN206087272U - A lot of aircraft that descends in area of planting - Google Patents
A lot of aircraft that descends in area of planting Download PDFInfo
- Publication number
- CN206087272U CN206087272U CN201621051388.9U CN201621051388U CN206087272U CN 206087272 U CN206087272 U CN 206087272U CN 201621051388 U CN201621051388 U CN 201621051388U CN 206087272 U CN206087272 U CN 206087272U
- Authority
- CN
- China
- Prior art keywords
- aircushion vehicle
- air cushion
- propeller
- undercarriage
- aircraft
- 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 lot of aircraft that descends in area of planting, including fin screw, organism, screw, safe seat, control system, undercarriage system, aircushion vehicle system and engine, the aircushion vehicle system includes aircushion vehicle front portion, aircushion vehicle rear portion, turbofan and motor. The device is small, and the safety in utilization goes with operating stability, the device can be arranged in the ground that the general aircraft of topographic reconnaissance and disaster area rescue can not descend, and the device passes through the all -round stop of the multiple environment of aircushion vehicle system implementation, and the device adopts the undercarriage that can adjust, solves to survey the slope and berth, is applicable to the multiple ground including the surface of water, the device's aircushion vehicle system is adjust the posture by oneself, guarantees that the aircraft normally takes off, has solved the volume problem the when aircushion vehicle is out of work, puts into among the the device to add scalable stretcher, realizes emergency rescue and disaster relief, wounded's transportation and baby plane and selects, is fit for that the disaster area is reconnoitered and the wounded transport.
Description
Technical field
This utility model is related to a kind of aircraft, specifically it is a kind of can various area landing aircrafts.
Background technology
Aircraft refers to that the power set with a tool or many tool electromotors produce the thrust or pulling force advanced, consolidating by fuselage
Determine wing and produce lift, in the airborne vehicle for overweighting air of endoatmosphere flight, aircraft is a kind of modal fixed-wing aviation
Device.According to its using engine type can be divided into jet airplane and propeller aeroplane again.Helicopter is exactly the one of aircraft
Kind, current helicopter when rescue is realized is looked for a suitable landing place to become a difficult problem, considers net during landing
Landforms around landing field and object height are all required by empty condition.And the mountain valley vacant lot in disaster area is often by soft farmland
Occupy, helicopter can not be dropped on the inadequate soil of these hardness.Sometimes it is also required at sea or marsh is rescued,
This just need helicopter as close to or stop, existing helicopter can not meet above-mentioned requirements, and this is just brought for rescue
Inconvenience.
Utility model content
The purpose of this utility model be provide it is a kind of can it is various area landing aircrafts, to solve in above-mentioned background technology
The problem of proposition.
For achieving the above object, this utility model provides following technical scheme：
It is a kind of can it is various area landing aircrafts, including empennage propeller, body, propeller, safety seat, control system
System, Landing Gear System, air cushion boat system and electromotor, the empennage propeller, propeller, safety seat, control system, rise and fall
Frame system and electromotor are installed on body, and safety seat and control system are installed in internal body and control system position
In the side of safety seat, Landing Gear System is arranged on the lower section of body, and air cushion boat system is arranged on the inside of Landing Gear System,
Electromotor is arranged on the top of body, and the top of body is provided with propeller, and the side of body is provided with empennage propeller, air cushion
Boat system includes air cushion forward quarter, aircushion vehicle rear portion, turbofan and motor, and turbofan is arranged on air cushion by turbo shelf
The air outlet of ship rear portion and turbofan is provided with air port baffle plate and air outlet support, the gentle pad ship rear portion in air cushion forward quarter
It is mounted on motor.
As further program of the utility model：Landing Gear System includes undercarriage, hydraulic cylinder and guide rail, and undercarriage is adopted
It is arranged on guide rail with the mode being slidably connected, guide rail adopts line slideway, and range sensor is additionally provided with undercarriage.
As further program of the utility model：Hydraulic cylinder is arranged on undercarriage by hydraulic cylinder leg, turbine wind
Machine adopts high-pressure turbine blower fan.
As further program of the utility model：Warning lamp is additionally provided with body, after the gentle pad ship in air cushion forward quarter
Portion is made using highstrenghtpiston, and air port baffle plate and turbo shelf are made using aluminum alloy materials.
Compared with prior art, the beneficial effects of the utility model are：The device is reasonable in design, and fault rate is low, small volume,
Safety in utilization and good operation stability；The device can be used for general aircraft in topographic(al) reconnaissance and disaster area rescue and can not land
Ground, the device realizes the comprehensive stop of various environment by air cushion boat system, and what the device employing can be adjusted rises and falls
Frame, solves to survey slope stop, it is adaptable to including the multiple types of floors including the water surface；The air cushion boat system of the device can voluntarily adjust appearance
Gesture, it is ensured that aircraft normally takes off, solves capacity issue when aircushion vehicle does not work, and is put into plus scalable load in the device
Frame, realizes that rescue and relief work, wounded's transport and baby plane are selected, and is adapted to disaster area and scouts and wounded's transhipment.
Description of the drawings
Fig. 1 be can it is various area landing aircrafts axonometric chart.
Fig. 2 be can it is various area landing aircrafts front view.
Fig. 3 be can it is various area landing aircrafts side view.
Fig. 4 be can it is various area landing aircrafts top view.
Fig. 5 be can it is various area landing aircrafts in air cushion boat system and Landing Gear System front view.
Fig. 6 be can it is various area landing aircrafts in air cushion boat system and Landing Gear System top view.
Wherein：1- empennage propellers, 2- bodies, 3- propellers, 4- safety seats, 5- control systems, 6- Landing Gear Systems,
7- air cushion boat systems, 8- electromotors, 9- warning lamps, 10- guide rails, 11- aircushion vehicles rear portion, 12- turbofans, 13- air ports baffle plate,
14- turbo shelfs, 15- hydraulic cylinders, 16- air cushions forward quarter, 17- air outlet supports, 18- motors, 19- undercarriages.
Specific embodiment
The technical scheme of this patent is described in more detail with reference to specific embodiment.
Refer to Fig. 1-6, it is a kind of can various area landing aircrafts, including empennage propeller 1, body 2, propeller 3, peace
Full seat 4, control system 5, Landing Gear System 6, air cushion boat system 7 and electromotor 8, the empennage propeller 1, propeller 3, peace
Full seat 4, control system 5, Landing Gear System 6 and electromotor 8 are installed on body 2, and safety seat 4 and control system 5 are equal
Inside body 2 and control system 5 be located at safety seat 4 side, Landing Gear System 6 be arranged on body 2 lower section,
Air cushion boat system 7 is arranged on the inside of Landing Gear System 6, and electromotor 8 is arranged on the top of body 2, and the top of body 2 is provided with
Propeller 3, the side of body 2 are provided with empennage propeller 1, and air cushion boat system 7 includes air cushion forward quarter 16, aircushion vehicle rear portion
11st, turbofan 12 and motor 18, turbofan 12 are arranged on aircushion vehicle rear portion 11 and turbofan by turbo shelf 14
12 air outlet is provided with air port baffle plate 13 and air outlet support 17, and air cushion forward quarter 16 and aircushion vehicle rear portion 11 are mounted on
Motor 18.Landing Gear System 6 includes undercarriage 19, hydraulic cylinder 15 and guide rail 10, and undercarriage 19 is pacified by the way of being slidably connected
It is mounted on guide rail 10, guide rail 10 adopts line slideway, is additionally provided with range sensor on undercarriage 19.Hydraulic cylinder 15 passes through hydraulic pressure
Jar support is arranged on undercarriage 19, and turbofan 12 adopts high-pressure turbine blower fan.Warning lamp 9, air cushion are additionally provided with body 2
Forward quarter 16 and aircushion vehicle rear portion 11 are made using highstrenghtpiston, and air port baffle plate 13 and turbo shelf 14 adopt aluminium alloy
Material makes.
Operation principle of the present utility model is：The aircraft quotes the configuration design of zero ° of aircraft by increasing flexible air cushion
Boat system 7 and Landing Gear System 6 realize that full landform is stopped, and 7 longitudinal direction of air cushion boat system is launched, and turbofan 12 is supplied for aircushion vehicle
Gas, realizes that many landform of aircraft are stopped, and taking off needs certain angle, when the angle of aircraft landing air cushion boat system 7 is improper,
Posture can voluntarily be adjusted, it is ensured that helicopter take-off angle.Air cushion boat system 7 shrinks, and undercarriage 19 puts down, and realizes aircraft good
The stop of good landform, energy saving.Landing Gear System 6 adopts hydraulic control, realizes that aircraft landing is steady by range sensor
Stop；Body 2 adopts baby plane, is suitably executed and reconnoitres the condition of a disaster, scouts the tasks such as the condition of a fire in mountain area.Air cushion boat system 7 is rising
The inside of the frame system 6 that falls, more can protect the air cushion boat system 7 when not working, and air cushion boat system 7 lift well,
Enough spaces are left between airframe 2 and air cushion boat system 7, retractable litter can be opened the transport for realizing the wounded.Gas
Air is sent into the bottom of air cushion, realizes the work of aircushion vehicle by high-pressure turbine blower fan 12 by pad boat system 7.Air cushion boat system 7
Be using pressure-air alow and the water surface（Or ground）Between form air cushion, make hull completely or partially hover, aircushion vehicle be use
High-power turbo blower fan 12 is pressed into air under hull bottom, is limited by air seal sets such as the flexible skirts or rigid sidewalls around hull bottom
Its effusion and soaring for being formed, the advantage of air cushion boat system 7 are that it can be in sandy beach, marsh, the water surface, ice face and appropriate recessed
Travel where convex injustice.Air cushion boat system 7 is reached air cushion boat system 7 and is occupied less when not in use using elastic
Space, reduces the flight resistance of helicopter.
The device is reasonable in design, and fault rate is low, small volume, safety in utilization and good operation stability；The device can be used
The ground that general aircraft can not land in topographic(al) reconnaissance and disaster area rescue, the device is realized various by air cushion boat system 7
The comprehensive stop of environment, the undercarriage 19 that the device employing can be adjusted solve to survey slope stop, it is adaptable to including including the water surface
Multiple types of floors；The air cushion boat system 7 of the device can voluntarily adjust posture, it is ensured that aircraft normally takes off, and solves aircushion vehicle
Capacity issue when not working, is put in the device plus Telescopic stretcher, realizes rescue and relief work, wounded's transport and baby plane
Select, be adapted to disaster area and scout and wounded's transhipment.
It is obvious to a person skilled in the art that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type is by claims rather than described above is limited, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in this utility model.Any reference in claim should not be considered as restriction
Involved claim.
Moreover, it will be appreciated that although this specification is been described by according to embodiment, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of description is only that those skilled in the art should for clarity
Using description as an entirety, the technical scheme in each embodiment can also Jing it is appropriately combined, form those skilled in the art
Understandable other embodiment.
Claims (4)
1. it is a kind of can it is various area landing aircrafts, it is characterised in that including empennage propeller, body, propeller, emergency seat
Chair, control system, Landing Gear System, air cushion boat system and electromotor, the empennage propeller, propeller, safety seat, control
System, Landing Gear System and electromotor are installed on body, safety seat and control system be installed in internal body and
Control system is located at the side of safety seat, and Landing Gear System is arranged on the lower section of body, and air cushion boat system is arranged on undercarriage
The inside of system, electromotor are arranged on the top of body, and the top of body is provided with propeller, and the side of body is provided with empennage
Propeller, air cushion boat system include air cushion forward quarter, aircushion vehicle rear portion, turbofan and motor, and turbofan is by turbine
Frame is arranged on aircushion vehicle rear portion and the air outlet of turbofan is provided with air port baffle plate and air outlet support, air cushion forward quarter
Motor is mounted on aircushion vehicle rear portion.
2. it is according to claim 1 can it is various area landing aircrafts, it is characterised in that the Landing Gear System has included
Fall frame, hydraulic cylinder and guide rail, and undercarriage is arranged on guide rail by the way of being slidably connected, and guide rail adopts line slideway, rises and falls
Range sensor is additionally provided with frame.
3. it is according to claim 2 can it is various area landing aircrafts, it is characterised in that the hydraulic cylinder pass through hydraulic cylinder
Support is arranged on undercarriage, and turbofan adopts high-pressure turbine blower fan.
4. it is according to claim 1 can it is various area landing aircrafts, it is characterised in that be additionally provided with police on the body
Show lamp, the gentle pad ship rear portion in air cushion forward quarter is made using highstrenghtpiston, and air port baffle plate and turbo shelf are closed using aluminum
Golden material makes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621051388.9U CN206087272U (en) | 2016-09-13 | 2016-09-13 | A lot of aircraft that descends in area of planting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621051388.9U CN206087272U (en) | 2016-09-13 | 2016-09-13 | A lot of aircraft that descends in area of planting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206087272U true CN206087272U (en) | 2017-04-12 |
Family
ID=58476580
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621051388.9U Expired - Fee Related CN206087272U (en) | 2016-09-13 | 2016-09-13 | A lot of aircraft that descends in area of planting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206087272U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184724A (en) * | 2016-09-13 | 2016-12-07 | 胡宇晗 | A kind of can multiple area landing aircraft |
-
2016
- 2016-09-13 CN CN201621051388.9U patent/CN206087272U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184724A (en) * | 2016-09-13 | 2016-12-07 | 胡宇晗 | A kind of can multiple area landing aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8453963B2 (en) | Amphibious large aircraft without airstairs | |
| CN107933914B (en) | Water-air amphibious sightseeing electric rotor aircraft | |
| CN203528804U (en) | Large-size rescue amphibious aircraft | |
| RU2721030C1 (en) | Multipurpose aircraft | |
| CN105270620A (en) | Integrated general-purpose vertical take-off and landing aircraft based on lifting and floating force | |
| WO2018209428A1 (en) | Amphibious, pressurizable and low noise twin-engine aircraft configuration | |
| CN106005394A (en) | Rescue aircraft | |
| US20210171189A1 (en) | High-speed take-off and landing anti-falling airplane | |
| US20200354050A1 (en) | Convertiplane | |
| CN206087272U (en) | A lot of aircraft that descends in area of planting | |
| CN105109694A (en) | Novel anti-falling airplane and anti-falling control method | |
| CN104787306A (en) | Low-speed safety aircraft capable of controlling flight attitude by aerodynamic force | |
| CN201086825Y (en) | Wing shaped airplane | |
| CN102424110A (en) | Variable wing miniature amphibious aircraft | |
| WO2013137915A1 (en) | Mid-wing airplane | |
| AU2006100241A4 (en) | An aircraft buoyancy augmentation device | |
| CA2507280A1 (en) | Auxiliary, rotatable, independent jet engines on plane fuselage | |
| CN109250117A (en) | A kind of civilian manned aircraft | |
| RU173780U1 (en) | PLANE AMPHIBIA | |
| RU2532658C2 (en) | Ram wing sea plane | |
| CN1618698A (en) | Life saving scheme of airplane and verticraft | |
| CN106184724A (en) | A kind of can multiple area landing aircraft | |
| CN108725772A (en) | A kind of band is without the rear single-screw paddle composite wing aircraft for pushing away the compound auxiliary wing | |
| CN205273454U (en) | Hover platform ships of dwelling more | |
| RU112154U1 (en) | MULTI-PURPOSE PLANE |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 Termination date: 20170913 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |