CN206954516U - Air flow system and gyroplane inside gyroplane - Google Patents
Air flow system and gyroplane inside gyroplane Download PDFInfo
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- CN206954516U CN206954516U CN201720543518.9U CN201720543518U CN206954516U CN 206954516 U CN206954516 U CN 206954516U CN 201720543518 U CN201720543518 U CN 201720543518U CN 206954516 U CN206954516 U CN 206954516U
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- gyroplane
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model provides the air flow system and gyroplane inside a kind of gyroplane, is related to air material technical field, removes to get up to waste time and energy after solving the front windshield frosting of gyroplane, fogging, causes the technical problem of huge potential safety hazard.Air flow system inside gyroplane includes cooling air unit, cooling air unit includes air inlet, air outlet and gas channel, air inlet is arranged on the outer surface of the fuselage of gyroplane, air outlet is arranged at the inner surface of gyroplane fuselage, gas channel connects air inlet and air outlet, and the cold wind flowed out by air outlet can flow along front windshield.Extraneous cold wind is introduced in gyroplane cabin by cooling air unit, to the air cooling-down in gyroplane cabin, the temperature difference after air cooling-down containing steam with glass outside air reduces, steam is not easy condensation and forms mist or frost, driver's seat is clear, has ensured the security in traveling way, and introduces outside air and cool to cabin atmosphere, without extra energy expenditure, energy-conservation environmental protection again.
Description
Technical field
The utility model is related to air material technical field, more particularly, to the air flow system inside a kind of gyroplane and
Gyroplane.
Background technology
Gyroplane is that relative wind when flying before a kind of utilization blows autorotation to produce the rotary wing aircraft of lift.It
Thrust directly provided by driven by engine propeller.It is a kind of aircraft between helicopter and aircraft, equipped with rotation
The wing and fixed aerofoil.Have the characteristics that landing apart from it is short, low speed low-latitude flying can be made, it is simple light and handy, be easy to hidden, but can not hang down
Straight landing, it can not hover.Available for take photo in the sky, arm discharge, battlefield scout etc..
Gyroplane and helicopter are simply the same from profile, and substantially gyroplane and helicopter are two kinds complete
Different aircraft.
Gyroplane is actually a kind of aircraft between helicopter and aircraft, and it is removed outside rotor, also with one
The propeller that pair is disposed vertically typically is also equipped with less wing and awing provides part lift to provide the power of advance.
The maximum difference of gyroplane and helicopter is that the rotor of gyroplane is not connected with engine driving system, and engine is not to drive
Dynamic rotor provides lift for gyroplane, but during gyroplane flies, rotor wing rotation is blown by front air-flow and produces liter
Power, as a windmill, rotor system is only driven when starting by self power, is referred to as prewhirl (prerotate), after taking off
Driven by air effect power；And the rotor of helicopter is connected with engine driving system, lift can be produced, and can provides flight
Power, as an electric fan.Because rotor is rotation type, the moment of torsion very little being delivered on fuselage, therefore gyroplane is without picture
Tail-rotor as single-rotor helicopter, but empennage is generally equipped with, to control flight.
Awing, gyroplane with helicopter be most significantly respectively helicopter rotor towards top rake, and gyroplane
Rotor be then sweptback.
Applicants have discovered that at least there is following technical problem in prior art：
Every winter, or always occur that the front windshield frosting of gyroplane, fogging show when cabin internal-external temperature difference is larger
As removing gets up to waste time and energy, and influences driver's seat, causes huge potential safety hazard.Existing frost removal is mostly adopted
Defrosted with mode of heating demisting, but a part of thermal source needed for defrosting is dispersed into extraneous wasting in vain, therefore in order to save
The about energy, mode of heating frost removal are usually just to start working after fogging frosting, do not have preventive effect.
In addition, supply warm wind is needed to reach comfortable temperature when winter or relatively low temperature in gyroplane cabin, if installed additional
Air-conditioning, certainly will increase energy resource consumption, and complete machine cost can also increase；On the other hand, the engine of gyroplane is in the course of work
In can distribute substantial amounts of heat and not be used and just dissipate in vain to surrounding environment, these heats, cause certain
Waste and loss.
Utility model content
The purpose of this utility model is to provide the air flow system and gyroplane inside a kind of gyroplane, existing to solve
Remove to get up to waste time and energy after the front windshield frosting of gyroplane present in technology, fogging, and influence driver's seat,
Cause the technical problem of huge potential safety hazard.
To achieve the above object, the utility model provides following technical scheme：
Air flow system inside a kind of gyroplane provided by the utility model, including cooling air unit, the cooling air unit bag
Air inlet, air outlet and gas channel are included, the air inlet is arranged on the outer surface of the fuselage of gyroplane, and the air outlet is set
The inner surface of gyroplane fuselage is placed in, the gas channel connects the air inlet and the air outlet, by the air outlet
The cold wind of outflow can flow along front windshield.
Frost is that in-car hot steam condenses formation to the cold, by setting cooling air unit that extraneous cold wind is introduced into gyroplane machine
In cabin, to the air cooling-down in gyroplane cabin, the temperature difference after the air cooling-down containing steam with glass outside air reduces, and steams
Vapour is not easy condensation and forms mist or frost, and driver's seat is clear, has ensured the security in traveling way, and introduces outside air and give
Cabin atmosphere cools, without extra energy expenditure, energy-conservation environmental protection again.
Further, the air outlet is arranged at the position of the close front windshield of gyroplane instrument board.
To the air cooling-down near front windshield, this targetedly local cooling mode ensures front windshield glass in cabin
Air themperature near glass reduces with the extraneous temperature difference of windshield, the steam in cabin in air be not easy condensation formed mist or
Frost, driver's seat is clear, has ensured the security in traveling way；And due to being local cooling, engine room inside bulk temperature
It will not be greatly affected, driver and passenger are unlikely to feel cold because temperature declines excessive.
Further, the gas channel passes through the inside of the instrument board of gyroplane.
The inside of the gas channel through the instrument board of gyroplane is directly communicated to instrument board close to front windshield
Air outlet.
The quantity of air outlet is multiple, and multiple air outlets are distributed in the front side of instrument board, and air outlet is close to front windshield glass
Glass；The cold wind of air outlet outflow flows upwards, backward along front windshield, to the air cooling-down near front windshield.
Further, the quantity of the air inlet is two, and two air inlets are arranged at the two of the boat lamp of gyroplane
Side.
Air inlet direction is consistent with blower fan heading, air-flow can with the traveling automatic stream air inlet of gyroplane,
And air outlet is circulated to by air inlet, it is convenient easily to realize and simple in construction without extra power set.
Further, in addition to heater, the warm wind, which is put, collects the heat dissipation capacity of gyroplane engine to adjust rotor
Temperature in machine cabin.
Further, the heater includes delivery pipe and the heat collection being arranged at below engine radiator
Box, the arrival end of the delivery pipe connect with the heat collection box, and the port of export of the delivery pipe connects with the inside of cabin.
Compared with traditional installation heating apparatus, the radiating for recycling engine not only saves come the mode to be heated up to cabin
About energy consumption, and realize that cost is also cheap by simple structure.
Further, the heat collection box is fixedly connected with engine radiator.
Heat collection box is directly fixedly connected with engine radiator, and intermediate link is few, and thermal losses is few, efficiency high.
Further, the delivery pipe is flexible pipe.
Heat is conveyed using flexible pipe, easy for installation, without changing original structure, Path selection is versatile and flexible, also can be more
Supernumerary segment material saving.
Further, the port of export of the delivery pipe is arranged at the rear side of gyroplane front passenger's seat chair back.
A kind of air flow system inside gyroplane, including above-mentioned gyroplane.
By setting cooling air unit to introduce extraneous cold wind in gyroplane cabin, to the air cooling-down in gyroplane cabin,
The temperature difference after air cooling-down containing steam with glass outside air reduces, and steam is not easy condensation and forms mist or frost, and driver regards
It is wild clear, the security in traveling way has been ensured, and introduce outside air and cool to cabin atmosphere, disappear without extra energy
Consumption, energy-conservation environmental protection again；The radiating for recycling engine not only saves energy consumption come the mode to be heated up to cabin, and by simple
Structure realize that cost is also cheap.
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 required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is a kind of structural representation of gyroplane of the air flow system inside the utility model is set；
Fig. 2 is the structural representation of cooling air unit outlet；
Fig. 3 gives the schematic diagram of gyroplane front windshield, in figure arrow it is signified be cooling air unit air-flow flowing side
To；
Fig. 4 is the structural representation of heater；
Fig. 5 is the connection diagram of heater and engine radiator.
1- air outlets in figure；2- front windshields；3- instrument boards；4- delivery pipes；5- engine radiators；6- heat collections
Box；7- air inlets.
Embodiment
, below will be to technology of the present utility model to make the purpose of this utility model, technical scheme and advantage clearer
Scheme is described in detail.Obviously, described embodiment is only the utility model part of the embodiment, rather than all
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not before creative work is made
Resulting all other embodiment is put, belongs to the scope that the utility model is protected.
As shown in Fig. 2 the utility model provides the air flow system inside a kind of gyroplane, including cooling air unit, it is described
Cooling air unit includes air inlet 7, air outlet 1 and gas channel, and the air inlet 7 is arranged at the outer surface of the fuselage of gyroplane
On, the air outlet 1 is arranged at the inner surface of gyroplane fuselage, and the gas channel connects the air inlet 7 and the air-out
Mouth 1, the cold wind flowed out by the air outlet 1 can flow along front windshield 2, and flow direction is as shown in Figure 3.
Frost is that in-car hot steam condenses formation to the cold, by setting cooling air unit that extraneous cold wind is introduced into gyroplane machine
In cabin, to the air cooling-down in gyroplane cabin, the temperature difference after the air cooling-down containing steam with glass outside air reduces, and steams
Vapour is not easy condensation and forms mist or frost, and driver's seat is clear, has ensured the security in traveling way, and introduces outside air and give
Cabin atmosphere cools, without extra energy expenditure, energy-conservation environmental protection again.
Optionally embodiment, the air outlet 1 are arranged at the close front windshield 2 of gyroplane instrument board 3
Position.
To the air cooling-down near front windshield 2, this targetedly local cooling mode ensures front windshield in cabin
Air themperature near glass 2 reduces with the extraneous temperature difference of windshield, and the steam in cabin in air is not easy condensation and forms mist
Or frost, driver's seat is clear, has ensured the security in traveling way；And due to being local cooling, the overall temperature of engine room inside
Degree will not be greatly affected, and driver and passenger are unlikely to feel cold because temperature declines excessive.
Optionally embodiment, the gas channel pass through the inside of the instrument board 3 of gyroplane.
The inside of the gas channel through the instrument board 3 of gyroplane is directly communicated to instrument board 3 close to front windshield 2
Air outlet 1.
The quantity of air outlet 1 is multiple, and multiple air outlets 1 are distributed in the front side of instrument board 3, and air outlet 1 is close to front
Wind glass 2；The cold wind that air outlet 1 flows out flows upwards, backward along front windshield 2, to the air near front windshield 2
Cooling.
Optionally embodiment, the quantity of the air inlet 7 is two, and two air inlets 7 are arranged at rotor
The both sides of the boat lamp of machine.
The direction of air inlet 7 is consistent with blower fan heading, and air-flow can be with the traveling automatic stream air inlet of gyroplane
7, and air outlet 1 is circulated to by air inlet 7, it is convenient easily to realize and simple in construction without extra power set.
As shown in Figure 4 and Figure 5, optionally embodiment, the air flow system inside gyroplane also include heater,
The warm wind, which is put, to be collected the heat dissipation capacity of gyroplane engine and adjusts the temperature in gyroplane cabin.
Optionally embodiment, the heater include delivery pipe 4 and are arranged at the lower section of engine radiator 5
Heat collection box 6, the arrival end of the delivery pipe 4 connects with the heat collection box 6, the port of export of the delivery pipe 4 with
The inside connection of cabin.
Compared with traditional installation heating apparatus, the radiating for recycling engine not only saves come the mode to be heated up to cabin
About energy consumption, and realize that cost is also cheap by simple structure.
Optionally embodiment, the heat collection box 6 are fixedly connected with engine radiator 5.
Heat collection box 6 is directly fixedly connected with engine radiator 5, and intermediate link is few, and thermal losses is few, efficiency high.
Optionally embodiment, the delivery pipe 4 are flexible pipe.
Heat is conveyed using flexible pipe, easy for installation, without changing original structure, Path selection is versatile and flexible, also can be more
Supernumerary segment material saving.
Optionally embodiment, after the port of export of the delivery pipe 4 is arranged at gyroplane front passenger's seat chair back
Side.
As shown in figure 1, the utility model provides the air flow system inside a kind of gyroplane, including above-mentioned gyroplane.
By setting cooling air unit to introduce extraneous cold wind in gyroplane cabin, to the air cooling-down in gyroplane cabin, contain steam
Air cooling-down after reduce with the temperature difference of glass outside air, steam is not easy condensation and forms mist or frost, and driver's seat is clear, protects
The security in traveling way is hindered, and has introduced outside air and cool to cabin atmosphere, without extra energy expenditure, energy-conservation is again
Environmental protection；The radiating for recycling engine not only saves energy consumption come the mode to be heated up to cabin, and real by simple structure
Existing, cost is also cheap.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art can readily occur in change in the technical scope that the utility model discloses
Or replace, it should all cover within the scope of protection of the utility model.Therefore, the scope of protection of the utility model should be with the power
The protection domain that profit requires is defined.
Claims (10)
1. the air flow system inside a kind of gyroplane, it is characterised in that including cooling air unit, the cooling air unit includes air inlet
(7), air outlet (1) and gas channel, the air inlet are arranged on the outer surface of the fuselage of gyroplane, the air outlet (1)
The inner surface of gyroplane fuselage is arranged at, the gas channel connects the air inlet and the air outlet, by the air-out
The cold wind of mouth (1) outflow can flow along front windshield (2).
2. the air flow system inside gyroplane according to claim 1, it is characterised in that the air outlet (1) is arranged at
The position of the close front windshield (2) of gyroplane instrument board (3).
3. the air flow system inside gyroplane according to claim 2, it is characterised in that the gas channel passes through rotor
The inside of the instrument board (3) of machine.
4. the air flow system inside gyroplane according to claim 1, it is characterised in that the quantity of the air inlet is two
Individual, two air inlets are arranged at the both sides of the boat lamp of gyroplane.
5. the air flow system inside gyroplane according to any one of Claims 1-4, it is characterised in that also including warm wind
Device, the warm wind, which is put, to be collected the heat dissipation capacity of gyroplane engine and adjusts the temperature in gyroplane cabin.
6. the air flow system inside gyroplane according to claim 5, it is characterised in that the heater includes conveying
Pipe (4) and the heat collection box (6) that is arranged at below engine radiator (5), the arrival end of the delivery pipe (4) with it is described
Heat collection box (6) connects, and the port of export of the delivery pipe (4) connects with the inside of cabin.
7. the air flow system inside gyroplane according to claim 6, it is characterised in that the heat collection box (6) with
Engine radiator (5) is fixedly connected.
8. the air flow system inside gyroplane according to claim 7, it is characterised in that the delivery pipe (4) is flexibility
Pipe.
9. the air flow system inside gyroplane according to claim 8, it is characterised in that the outlet of the delivery pipe (4)
End is arranged at the rear side of gyroplane front passenger's seat chair back.
10. gyroplane, it is characterised in that including the air flow system inside the gyroplane described in claim any one of 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720543518.9U CN206954516U (en) | 2017-05-15 | 2017-05-15 | Air flow system and gyroplane inside gyroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720543518.9U CN206954516U (en) | 2017-05-15 | 2017-05-15 | Air flow system and gyroplane inside gyroplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206954516U true CN206954516U (en) | 2018-02-02 |
Family
ID=61376072
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720543518.9U Active CN206954516U (en) | 2017-05-15 | 2017-05-15 | Air flow system and gyroplane inside gyroplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206954516U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107416211A (en) * | 2017-05-15 | 2017-12-01 | 河北天启通宇航空器材科技发展有限公司 | Air flow system and gyroplane inside gyroplane |
-
2017
- 2017-05-15 CN CN201720543518.9U patent/CN206954516U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107416211A (en) * | 2017-05-15 | 2017-12-01 | 河北天启通宇航空器材科技发展有限公司 | Air flow system and gyroplane inside gyroplane |
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