CN106184724A - A kind of can multiple area landing aircraft - Google Patents
A kind of can multiple area landing aircraft Download PDFInfo
- Publication number
- CN106184724A CN106184724A CN201610818520.2A CN201610818520A CN106184724A CN 106184724 A CN106184724 A CN 106184724A CN 201610818520 A CN201610818520 A CN 201610818520A CN 106184724 A CN106184724 A CN 106184724A
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- CN
- China
- Prior art keywords
- aircushion vehicle
- propeller
- aircraft
- aircushion
- turbofan
- 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.)
- Pending
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
- B64C25/56—Floats inflatable
Abstract
The invention discloses a kind of can multiple area landing aircraft, including empennage propeller, body, propeller, safety seat, control system, Landing Gear System, aircushion vehicle system and electromotor, described aircushion vehicle system includes aircushion vehicle front portion, aircushion vehicle rear portion, turbofan and motor.This device volume is little, safety in utilization and good operation stability；This device may be used for the ground that in topographic(al) reconnaissance and disaster area rescue, general aircraft can not land, this device realizes the comprehensive stop of multiple environment by aircushion vehicle system, this device uses the undercarriage that can regulate, and solves to survey slope and stops, it is adaptable to the multiple types of floors including the water surface；The aircushion vehicle system of this device can be from Row sum-equal matrix posture, ensure that aircraft normally takes off, solve capacity issue when aircushion vehicle does not works, this device is put into and adds Telescopic stretcher, realize rescue and relief work, wounded's transport and baby plane to select, be suitable for disaster area and scout and wounded's transhipment.
Description
Technical field
The present invention relates to a kind of aircraft, a kind of can the aircraft of multiple area landing.
Background technology
Aircraft refers to that the power set with a tool or many tool electromotors produce the thrust or pulling force, consolidating by fuselage advanced
Determining wing and produce lift, at the airborne vehicle overweighting air of endoatmosphere flight, aircraft is modal a kind of fixed-wing aviation
Device.Jet airplane and propeller aeroplane can be divided into again according to its engine type used.Helicopter is exactly the one of aircraft
Kind, current helicopter, realizing rescue when, looks for a suitable landing place to become a difficult problem, considers clean during landing
Landforms around landing field and object height are all required by empty condition.And the vacant lot, mountain valley in disaster area is often by soft farmland
Occupying, helicopter can not drop on the soil that these hardness are inadequate.Sometimes it is also required at sea or marsh is rescued,
This just needs helicopter close as far as possible or stops, and existing helicopter can not meet above-mentioned requirements, and this just brings for rescue
Inconvenience.
Summary of the invention
It is an object of the invention to provide a kind of can multiple area landing aircraft, with solve in above-mentioned background technology propose
Problem.
For achieving the above object, the present invention provides following technical scheme:
A kind of can multiple area landing aircraft, including empennage propeller, body, propeller, safety seat, control system, rise
Fall frame system, aircushion vehicle system and electromotor, described empennage propeller, propeller, safety seat, control system, undercarriage system
System and electromotor are installed on body, and safety seat and control system are installed in internal body and control system is positioned at peace
The side of full seat, Landing Gear System is arranged on the lower section of body, and aircushion vehicle system is arranged on the inside of Landing Gear System, starts
Machine 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, aircushion vehicle system
System includes aircushion vehicle front portion, aircushion vehicle rear portion, turbofan and motor, after turbofan is arranged on aircushion vehicle by turbo shelf
Being provided with air port baffle plate and air outlet support at the air outlet of portion and turbofan, aircushion vehicle is anterior and aircushion vehicle rear portion is all pacified
Equipped with motor.
As the further scheme of the present invention: Landing Gear System includes undercarriage, hydraulic cylinder and guide rail, undercarriage uses sliding
The mode being dynamically connected is arranged on guide rail, and guide rail uses line slideway, and undercarriage is additionally provided with range sensor.
As the further scheme of the present invention: hydraulic cylinder is arranged on undercarriage by hydraulic cylinder leg, and turbofan is adopted
Use high-pressure turbine blower fan.
As the further scheme of the present invention: be additionally provided with warning lamp on body, aircushion vehicle is anterior and aircushion vehicle rear portion is equal
Using highstrenghtpiston to make, air port baffle plate and turbo shelf all use aluminum alloy materials to make.
Compared with prior art, the invention has the beneficial effects as follows: this device is reasonable in design, failure rate is low, volume is little, uses
Safety and good operation stability；This device may be used for the ground that in topographic(al) reconnaissance and disaster area rescue, general aircraft can not land
Face, this device realizes the comprehensive stop of multiple environment by aircushion vehicle system, and this device uses the undercarriage that can regulate, and solves
Certainly survey slope to stop, it is adaptable to the multiple types of floors including the water surface；The aircushion vehicle system of this device can be protected from Row sum-equal matrix posture
Card aircraft normally take off, solve when aircushion vehicle does not works capacity issue, this device is put into and adds Telescopic stretcher, it is achieved
Rescue and relief work, wounded's transport and baby plane select, and are suitable for disaster area and scout and wounded's transhipment.
Accompanying drawing explanation
Fig. 1 is can the axonometric chart of aircraft of multiple area landing.
Fig. 2 is can the front view of aircraft of multiple area landing.
Fig. 3 is can the side view of aircraft of multiple area landing.
Fig. 4 is can the top view of aircraft of multiple area landing.
Fig. 5 be can multiple area landing aircraft in aircushion vehicle system and the front view of Landing Gear System.
Fig. 6 be can multiple area landing aircraft in aircushion vehicle system and the top view of Landing Gear System.
Wherein: 1-empennage propeller, 2-body, 3-propeller, 4-safety seat, 5-control system, 6-Landing Gear System,
7-aircushion vehicle system, 8-electromotor, 9-warning lamp, 10-guide rail, 11-aircushion vehicle rear portion, 12-turbofan, 13-air port baffle plate,
14-turbo shelf, 15-hydraulic cylinder, 16-aircushion vehicle is anterior, 17-air outlet support, 18-motor, 19-undercarriage.
Detailed description of the invention
Below in conjunction with detailed description of the invention, the technical scheme of this patent is described in more detail.
Refer to Fig. 1-6, a kind of can the aircraft of multiple area landing, including empennage propeller 1, body 2, propeller 3, peace
Full seat 4, control system 5, Landing Gear System 6, aircushion vehicle system 7 and electromotor 8, described 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
Being arranged on inside body 2 and control system 5 is positioned at the side of safety seat 4, Landing Gear System 6 is arranged on the lower section of body 2,
Aircushion vehicle 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 is provided with empennage propeller 1, and aircushion vehicle system 7 includes aircushion vehicle front portion 16, aircushion vehicle rear portion
11, turbofan 12 and motor 18, turbofan 12 is arranged on aircushion vehicle rear portion 11 and turbofan by turbo shelf 14
Being provided with air port baffle plate 13 and air outlet support 17 at the air outlet of 12, aircushion vehicle anterior 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 uses the mode being slidably connected to pacify
Being contained on guide rail 10, guide rail 10 uses line slideway, and undercarriage 19 is additionally provided with range sensor.Hydraulic cylinder 15 passes through hydraulic pressure
Jar support is arranged on undercarriage 19, and turbofan 12 uses high-pressure turbine blower fan.Warning lamp 9, air cushion it is additionally provided with on body 2
Forward quarter 16 and aircushion vehicle rear portion 11 all use highstrenghtpiston to make, and air port baffle plate 13 and turbo shelf 14 all use aluminium alloy
Material makes.
The operation principle of the present invention is: this aircraft quotes the configuration design of zero ° of aircraft by increasing flexible aircushion vehicle system
System 7 and Landing Gear System 6 realize full landform and stop, and aircushion vehicle system 7 is longitudinally launched, and turbofan 12 supplies for aircushion vehicle, real
Many landform of existing aircraft are stopped, and take off and need certain angle, when the angle of aircraft landing aircushion vehicle system 7 is improper, permissible
From Row sum-equal matrix posture, it is ensured that helicopter take-off angle.Aircushion vehicle system 7 is shunk, and undercarriage 19 puts down, it is achieved aircraft is well
The stop of shape, saves the energy.Landing Gear System 6 uses hydraulic control, realizes aircraft landing by range sensor and steadily stops；
Body 2 uses baby plane, is suitably executed and reconnoitres the condition of a disaster in mountain area, scouts the tasks such as the condition of a fire.Aircushion vehicle system 7 is in undercarriage system
The inside of system 6, more can well protect the aircushion vehicle system 7 when not working, and aircushion vehicle system 7 can lift, aircraft machine
Leave enough spaces between body 2 and aircushion vehicle system 7, retractable litter can be opened the transport realizing the wounded.Aircushion vehicle system
Air, by high-pressure turbine blower fan 12, is sent into the bottom of air cushion, it is achieved the work of aircushion vehicle by system 7.Aircushion vehicle system 7 is to utilize
Pressure-air alow and forms air cushion between the water surface (or ground), make hull completely or partially hover, and aircushion vehicle is with high-power
Air is pressed under hull bottom by turbofan 12, the air seal sets such as the flexible skirt around hull bottom or rigid sidewalls limit its effusion
And soaring of being formed, the advantage of aircushion vehicle system 7 be it can at sandy beach, marsh, the water surface, ice face and the most uneven
Local traveling.Aircushion vehicle system 7 uses elastic, reaches aircushion vehicle system 7 and occupies less space when not in use, subtracts
The flight resistance of few helicopter.
This device is reasonable in design, failure rate is low, and volume is little, safety in utilization and good operation stability；This device can be used
The ground that general aircraft can not land in topographic(al) reconnaissance and disaster area are rescued, this device realizes multiple by aircushion vehicle system 7
The comprehensive stop of environment, this device uses the undercarriage 19 that can regulate, and solves to survey slope and stops, it is adaptable to including the water surface
Multiple types of floors；The aircushion vehicle system 7 of this device can be from Row sum-equal matrix posture, it is ensured that aircraft normally takes off, and solves aircushion vehicle
When not working capacity issue, this device is put into and adds Telescopic stretcher, it is achieved rescue and relief work, the wounded transport and baby plane
Select, be suitable for disaster area and scout and wounded's transhipment.
It is obvious to a person skilled in the art that the invention is not restricted to the details of above-mentioned one exemplary embodiment, Er Qie
In the case of the spirit or essential attributes of the present invention, it is possible to realize the present invention in other specific forms.Therefore, no matter
From the point of view of which point, all should regard embodiment as exemplary, and be nonrestrictive, the scope of the present invention is by appended power
Profit requires rather than described above limits, it is intended that all by fall in the implication of equivalency and scope of claim
Change is included in the present invention.Should not be considered as limiting involved claim by any reference in claim.
Although moreover, it will be appreciated that this specification is been described by according to embodiment, but the most each embodiment only wraps
Containing an independent technical scheme, this narrating mode of description is only that for clarity sake those skilled in the art should
Description can also be formed those skilled in the art through appropriately combined as an entirety, the technical scheme in each embodiment
May be appreciated other embodiments.
Claims (4)
1. one kind can multiple area landing aircraft, it is characterised in that include empennage propeller, body, propeller, emergency seat
Chair, control system, Landing Gear System, aircushion vehicle system and electromotor, described 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 positioned at the side of safety seat, and Landing Gear System is arranged on the lower section of body, and aircushion vehicle system is arranged on undercarriage
The inside of 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, aircushion vehicle system includes aircushion vehicle front portion, aircushion vehicle rear portion, turbofan and motor, and turbofan is propped up by turbine
Frame is arranged at the air outlet of aircushion vehicle rear portion and turbofan and is provided with air port baffle plate and air outlet support, and aircushion vehicle is anterior
It is mounted on motor with aircushion vehicle rear portion.
The most according to claim 1 can multiple area landing aircraft, it is characterised in that described Landing Gear System has included
Fall frame, hydraulic cylinder and guide rail, and undercarriage uses the mode being slidably connected to be arranged on guide rail, and guide rail uses line slideway, rises and falls
Range sensor it is additionally provided with on frame.
The most according to claim 2 can multiple area landing aircraft, it is characterised in that described hydraulic cylinder passes through hydraulic cylinder
Support is arranged on undercarriage, and turbofan uses high-pressure turbine blower fan.
The most according to claim 1 can multiple area landing aircraft, it is characterised in that be additionally provided with police on described body
Showing lamp, aircushion vehicle is anterior and aircushion vehicle rear portion all uses highstrenghtpiston to make, and air port baffle plate and turbo shelf all use aluminum to close
Gold copper-base alloy makes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610818520.2A CN106184724A (en) | 2016-09-13 | 2016-09-13 | A kind of can multiple area landing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610818520.2A CN106184724A (en) | 2016-09-13 | 2016-09-13 | A kind of can multiple area landing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184724A true CN106184724A (en) | 2016-12-07 |
Family
ID=58068161
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610818520.2A Pending CN106184724A (en) | 2016-09-13 | 2016-09-13 | A kind of can multiple area landing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184724A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1069209A (en) * | 1964-09-16 | 1967-05-17 | Fiat Spa | Air cushion vehicle |
| FR2272872A1 (en) * | 1975-03-10 | 1975-12-26 | Dobb Herbert | Helicopter propelled air cushion vehicle - has load carrying nacelle movable on rails between twin pontoons with skirts |
| US4984754A (en) * | 1986-07-28 | 1991-01-15 | Arthur Yarrington | Heli-hover amphibious surface effect vehicle |
| GB2423971A (en) * | 2005-03-12 | 2006-09-13 | George W Davis | Autogyro hovercraft |
| CN104619591A (en) * | 2012-10-04 | 2015-05-13 | 波音公司 | Configuring landing supports for landing on uneven terrain |
| CN206087272U (en) * | 2016-09-13 | 2017-04-12 | 胡宇晗 | A lot of aircraft that descends in area of planting |
-
2016
- 2016-09-13 CN CN201610818520.2A patent/CN106184724A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1069209A (en) * | 1964-09-16 | 1967-05-17 | Fiat Spa | Air cushion vehicle |
| FR2272872A1 (en) * | 1975-03-10 | 1975-12-26 | Dobb Herbert | Helicopter propelled air cushion vehicle - has load carrying nacelle movable on rails between twin pontoons with skirts |
| US4984754A (en) * | 1986-07-28 | 1991-01-15 | Arthur Yarrington | Heli-hover amphibious surface effect vehicle |
| GB2423971A (en) * | 2005-03-12 | 2006-09-13 | George W Davis | Autogyro hovercraft |
| CN104619591A (en) * | 2012-10-04 | 2015-05-13 | 波音公司 | Configuring landing supports for landing on uneven terrain |
| CN206087272U (en) * | 2016-09-13 | 2017-04-12 | 胡宇晗 | A lot of aircraft that descends in area of planting |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161207 |
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| WD01 | Invention patent application deemed withdrawn after publication |