CN204916153U - Formula aircraft is put to gaseous pressure - Google Patents
Formula aircraft is put to gaseous pressure Download PDFInfo
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- CN204916153U CN204916153U CN201520661477.4U CN201520661477U CN204916153U CN 204916153 U CN204916153 U CN 204916153U CN 201520661477 U CN201520661477 U CN 201520661477U CN 204916153 U CN204916153 U CN 204916153U
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- pressure relief
- gas pressure
- balloon
- relief type
- gas
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Abstract
The utility model provides a formula aircraft is put to gaseous pressure, include: main rise balloon (1), aerify balloon (2), gas storage unit (3), gas compression unit (4), the control unit (5), balloon cover physically and connecting device (11), radio signal receiving unit (6) and power (15) etc. This formula aircraft is put to gaseous pressure has increased on the basis of inert gas balloon and has aerifyd balloon, gas compression unit, the balloon cover body and connecting device, through realizing this formula aircraft is put to gaseous pressure's rising, suspension, decline, landing to aerifing balloon volume change. Simultaneously, can also charge in order to guarantee the long -time flight aloft of this formula aircraft is put to gaseous pressure through the solar cell panel who sets up on with this formula aircraft is put to gaseous pressure, belong to the green design with this formula aircraft is put to gaseous pressure, the security is high, convenient operation, can be used for fields such as amusement, air traffic, scientific investigation, military affairs, has wide application space.
Description
Technical field
The utility model relates to a kind of gas pressure relief type aircraft.
Background technology
The enforcement the earliest of balloon flighter can be traced back to 1784, and the manual feed fish shape of Frenchman Robert brother fills taking a flight test of hydrogen HIKOUSEN.French engineer Ji Faer in 1852 has manufactured and designed that air bag is 2500 cubic meters, to promote screw propeller be onward impulse operates and fill hydrogen dirigible with steam engine.
At present, unreactable gas balloon in the world in realization lift operations time need balloon inflation, need when realizing step-down operation balloon venting, its shortcoming is to consuming time relatively long during balloon inflation, causes expensive unreactable gas to waste when exit to balloon.
Utility model content
In order to solve the above-mentioned shortcoming that balloon exists when inflating and exit, the utility model provides a kind of gas pressure relief type aircraft, this gas pressure relief type aircraft adds aerating ballon and gas compressing apparatus on the basis of unreactable gas balloon, by realizing the rising of this gas pressure relief type aircraft, suspension, decline, landing to aerating ballon volume change, in addition, the airflight that rotor driver realizes this gas pressure relief type aircraft is equipped with.
The utility model solves the technical scheme that its technical matters adopts: a kind of gas pressure relief type aircraft, comprising:
Mainly rise balloon, completely quantitative helium can be filled, provide predetermined lift can to this gas pressure relief type aircraft;
Aerating ballon, can be charged helium and discharge helium, realizing the rising of this gas pressure relief type aircraft, decline, suspension, landing;
Gas storage unit, is filled with this aerating ballon for stores compression gas by this pressure gas;
Gas compression unit, stores for sending into this gas storage unit after the gas compression of being discharged by this aerating ballon;
Control unit, can control gas that aerating ballon discharges and send into this gas compression unit and carry out compressing and the gas of compression is sent into gas storage unit, can also control this gas compression unit and inflate this aerating ballon;
Wireless signal Transmit-Receive Unit, can realize this gas pressure relief type aircraft and the external world contacts;
Power supply, powers for giving this gas pressure relief type aircraft.
Described gas pressure relief type aircraft also comprises aircraft device body, and gas storage unit, gas compression unit and control unit are all arranged in aircraft device body.
This is main rises balloon and aerating ballon adjoins up and down, and aircraft device body is positioned at this main below rising balloon and aerating ballon; Or, this is main rise balloon and aerating ballon about adjacent, aircraft device body is positioned at this main below rising balloon and aerating ballon.
The main balloon that rises is connected with aircraft device body by balloon cover body and connecting device with aerating ballon, and balloon cover body covers on and mainly rises outside balloon and aerating ballon, and connecting device is arranged on balloon cover body lower end, and balloon cover body is connected with aircraft device body by connecting device.
Balloon cover body is connected with connecting device, and connecting device is for connecting tightrope.
Gas storage unit, gas compression unit and control unit are all arranged in aircraft device body, and wireless signal Transmit-Receive Unit is arranged on outside the surface of aircraft device body.
Described gas pressure relief type aircraft also comprises for the solar panel of this power source charges, and this solar panel is arranged at outside the outer and/or aircraft device body of balloon cover body.
Described gas pressure relief type aircraft also comprises testing and alarm unit, and this testing and alarm unit is connected with control unit, and this testing and alarm unit can send alerting signal when this gas pressure relief type aircraft occurs abnormal.
Aircraft device is provided with the rotor driver for driving flight and change of flight direction with it, the bottom of aircraft device body is provided with the running gear that this gas pressure relief type aircraft can be made to walk on the ground, and described gas pressure relief type aircraft also comprises the remote controller for this gas pressure relief type aircraft of remote control.
The quantity of aerating ballon is no more than 2.
The beneficial effects of the utility model are, this gas pressure relief type aircraft adds aerating ballon and gas compression unit on the basis of unreactable gas balloon, by realizing the rising of this gas pressure relief type aircraft, suspension, decline, landing to aerating ballon volume change.Meanwhile, can also by the solar panel that this gas pressure relief type aircraft is arranged being carried out charge to ensure the skyborne flying for long time of this gas pressure relief type aircraft; This gas pressure relief type aircraft is belonged to environmental protection design, safety is high, easy to operate, may be used for the fields such as amusement, air communication, scientific investigation, military affairs, has wide application space.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described in further detail.
Fig. 1 is the schematic front view of the first gas pressure relief type aircraft.
Fig. 2 is the schematic rear view of the first gas pressure relief type aircraft.
Fig. 3 is the principle schematic of gas pressure relief type aircraft.
Fig. 4 is the schematic diagram of the second gas pressure relief type aircraft.
Fig. 5 is the schematic diagram of the third gas pressure relief type aircraft.
1. mainly rise balloon, 2. aerating ballon, 3. gas storage unit, 4. gas compression unit, 5. control unit, 6. wireless signal Transmit-Receive Unit, 7. rotor driver, 8. running gear, 9. pipeline system, 10. aircraft device body, 11. connecting devices, 12. balloon cover bodies, 13. valves, 14. testing and alarm unit, 15. power supplys.
Detailed description of the invention
It should be noted that, when not conflicting, the embodiment in the application and the feature in embodiment can combine mutually.Below with reference to the accompanying drawings and describe the utility model in detail in conjunction with the embodiments.
A kind of gas pressure relief type aircraft, comprising:
Mainly rise balloon 1, the helium that interior filling is completely quantitative, provide lift can to this gas pressure relief type aircraft;
Aerating ballon 2, can be charged helium and discharge helium, realizing the rising of this gas pressure relief type aircraft, decline, suspension, landing;
Gas storage unit 3, is filled with this aerating ballon 2 for stores compression gas by this pressure gas;
Gas compression unit 4, sends into this gas storage unit 3 for after the gas compression of being discharged by this aerating ballon 2;
Control unit 5, gas that aerating ballon 2 discharges can be controlled send into this gas compression unit 4 and carry out compressing and the gas of compression is sent into gas storage unit 3, this gas compression unit 4 can also be controlled inflate this aerating ballon 2, to realize the rising of this gas pressure relief type aircraft, decline, suspension, landing;
Wireless signal Transmit-Receive Unit 6, for contacting with the external world;
Power supply 15, for powering to this gas pressure relief type aircraft, as shown in Figure 1 to Figure 3.
In the present embodiment, the main constancy of volume rising balloon 1, namely in use, main rise in balloon 1 fill full quantitative helium after generally no longer carry out being filled with helium or discharging helium, mainly rise the helium being filled with setting weight in balloon 1, the volume of aerating ballon 2 can change, namely when aerating ballon 2 is filled with helium, the volume of aerating ballon 2 increases, when aerating ballon 2 discharges helium, and the smaller volume of aerating ballon 2.The gas that aerating ballon 2 is discharged enters gas storage unit 3 after the compression of gas compression unit 4, when aerating ballon 2 needs inflation, gas storage unit 3 is inflated aerating ballon 2 again, and the helium of such aerating ballon 2 in the process of whole inflation and venting in aerating ballon 2 can not be revealed but recycle.In addition, by regulating the overall lift of this gas pressure relief type aircraft of stereomutation of aerating ballon 2, operate simple and quick.
Concrete, the main volume rising balloon 1 arranges according to the own wt of this gas pressure relief type aircraft, makes the main balloon 1 that rises possess certain lift; Aerating ballon 2 be according to occupant, carry this gas pressure relief type aircraft that goods and materials weight is arranged lifting balloon, guarantee that this gas pressure relief type aircraft skybornely can rise when load-carrying, declines, if the lift that rise balloon 1 provides main is 1000N, and the lift that aerating ballon 2 provides can be 100N ~ 1000N.The rising of this gas pressure relief type aircraft, the inflation of the main dependence aerating ballon 2 that declines, venting realize.During the work of this gas pressure relief type aircraft, the main balloon 1 that rises is in the state that unreactable gas is full of, the unreactable gas (helium) stored is filled in aerating ballon 2 by pipeline system 9 by gas storage unit 3, realized rising and the suspension of this gas pressure relief type aircraft by the cubic expansion of aerating ballon 2, the unreactable gas in aerating ballon 2 to be compressed in gas storage unit 3 by pipeline system by gas compression unit 4 and the volume reducing aerating ballon 2 realizes decline and the suspension of this gas pressure relief type aircraft.The main design rising balloon 1 and aerating ballon 2 belongs to modularization and seriation structure design, and flexible, the main position rising balloon 1 and aerating ballon 2 of its array mode is determined according to actual conditions.
Main balloon 1 can be elastomeric material with the material of aerating ballon 2, or elastomeric material composite material.For the ease of gas compression, can also be provided with exhaust unit between gas compression unit 4 and aerating ballon 2, this exhaust unit escapes and enter gas compression unit 4 for making the gas in aerating ballon 2.
In the present embodiment, described gas pressure relief type aircraft also comprises aircraft device body 10, aircraft device body 10 be framing member as crew department, goods and materials storage chamber, aircraft mechanical room, gas storage unit 3, gas compression unit 4 and control unit 5 are all arranged in aircraft device body 10.Gas storage unit 3, gas compression unit 4 and control unit 5 are all arranged in aircraft device body 10, gas storage unit 3 and gas compression unit 4 are separated with the balance ensureing aircraft device body 10 in aircraft device body 10, control unit 5 is positioned at aircraft device body 10, wireless signal Transmit-Receive Unit 6 is arranged on outside aircraft device body 10 surface, as shown in Figure 1.
This gas pressure relief type aircraft mainly can rise balloon 1 and multiple aerating ballon 2 containing multiple, and its array mode can be flexible and changeable, and the main position rising balloon 1 and aerating ballon 2 also can be determined according to actual conditions.In the present embodiment, described gas pressure relief type aircraft mainly can rise balloon 1 and 1 aerating ballon 2 containing 1, this is main rises balloon 1 and aerating ballon about 2 adjacent (contact), and aircraft device body 10 is positioned at this main below rising balloon 1 and aerating ballon 2, as depicted in figs. 1 and 2; Or described gas pressure relief type aircraft contains 1 and mainly rises balloon 1 and 2 aerating ballons 2, this is main rises balloon 1 and aerating ballon about 2 adjoins, and aircraft device body 10 is positioned at this main below rising balloon 1 and aerating ballon 2, as shown in Figure 4; Or described gas pressure relief type aircraft contains 1 and mainly rises balloon 1 and 1 aerating ballon 2, this is main rises balloon 1 and aerating ballon about 2 adjoins, and aircraft device body 10 is positioned at this main below rising balloon 1 and aerating ballon 2, as shown in Figure 5.
In the present embodiment, the main balloon 1 that rises is connected with aircraft device body 10 by balloon cover body 12 and connecting device 11 with aerating ballon 2, balloon cover body 12 is the cryptomere closed, containing spatial accommodation in balloon cover body 12, balloon cover body 12 covers on and mainly rises outside balloon 1 and aerating ballon 2, namely mainly rise balloon 1 and aerating ballon 2 is wrapped in balloon cover body 12, connecting device 11 is arranged on balloon cover body 12 lower end, and balloon cover body 12 is connected with aircraft device body 10 by connecting device 11.Balloon cover body 12 both can prevent from mainly rising balloon 1 and aerating ballon 2 departs from described gas pressure relief type aircraft, can restrain and control again the main volume rising balloon 1, aerating ballon 2, especially be unlikely to damage because pressure variation makes balloon volume change expand in high-altitude lost efficacy and produced safety problem.Preferably, balloon cover body 12 is connected with connecting device 11, and namely balloon cover body 12 and connecting device 11 are integral type structure, and balloon cover body 12 can not be separated with between connecting device, and wherein, connecting device 11 is for connecting tightrope.
In order to extend the airborne hours that this states gas pressure relief type aircraft, described gas pressure relief type aircraft can arrange and comprise for the solar panel of this power source charges, this solar panel is arranged at outside balloon cover body 12 and/or outside aircraft device body 10, namely this solar panel is arranged at outside balloon cover body 12, or this solar panel is arranged at outside aircraft device body 10, or this solar panel is arranged at outside balloon cover body 12 and aircraft device body 10.
In this enforcement, described gas pressure relief type aircraft also comprises testing and alarm unit 14, and this testing and alarm unit 14 is connected with control unit 5, and this testing and alarm unit 14 can send alerting signal when this gas pressure relief type aircraft occurs abnormal.This testing and alarm unit 14 contains and aerating ballon 2, gas storage unit 3, gas compression unit 4, control unit 5, the sensor that wireless signal Transmit-Receive Unit 6 is connected with power supply 15, when wherein any one unit module et out of order, this testing and alarm unit 14 can send alerting signal to control unit 5, alerting signal is sent again by wireless signal Transmit-Receive Unit 6 remote controller earthward, thus make control gas pressure relief type aircraft landing described in this, or automatic landing procedure is set in control unit 5, when this testing and alarm unit 14 sends alerting signal to control unit 5, control unit 5 operates this gas pressure relief type aircraft and automatically lands, as shown in Figure 3.This testing and alarm unit 14 makes this gas pressure relief type flying balloon under precarious position, play warning, warning, contact, communication effect.
In this enforcement, aircraft device body 10 is provided with the rotor driver 7 for driving flight and change of flight direction, rotor driver 7 can advance, retreat and change direction by driving gas pressure relief type aircraft, the bottom of aircraft device body 10 is provided with running gear 8, and running gear 8 can so that the taking off and land and walking on the ground of described gas pressure relief type aircraft.Described gas pressure relief type aircraft also comprises the remote controller for this gas pressure relief type aircraft of remote control, the transmission of wireless signal is carried out between this remote controller and wireless signal Transmit-Receive Unit 6, such user by the rising of described gas pressure relief type aircraft, decline and suspension just can be operated at terrestrial operation remote controller, as shown in Figure 2.
This gas pressure relief type aircraft adds aerating ballon 2 and gas compression unit 4 on the basis of unreactable gas balloon, by realizing the rising of this gas pressure relief type aircraft, suspension, decline, landing to the change of aerating ballon 2 volume.Meanwhile, can also by the solar panel that this gas pressure relief type aircraft is arranged being carried out charge to ensure the skyborne flying for long time of this gas pressure relief type aircraft; This gas pressure relief type aircraft is belonged to environmental protection design, safety is high, easy to operate, may be used for the fields such as amusement, air communication, scientific investigation, military affairs, has wide application space.
The above; be only specific embodiment of the utility model, the scope of utility model enforcement can not be limited with it, so the displacement of its equivalent assemblies; or the equivalent variations to do according to the utility model scope of patent protection and modification, all still should belong to the category that this patent is contained.In addition, the technical characteristic in the utility model and all can using by independent assortment between technical characteristic, between technical characteristic and technical scheme, between technical scheme and technical scheme.
Claims (10)
1. a gas pressure relief type aircraft, is characterized in that, described gas pressure relief type aircraft comprises:
Mainly rise balloon (1), completely quantitative helium can be filled, provide predetermined lift can to this gas pressure relief type aircraft;
Aerating ballon (2), can be charged helium and discharge helium, realizing the rising of this gas pressure relief type aircraft, decline, suspension, landing;
Gas storage unit (3), is filled with this aerating ballon (2) for stores compression gas by this pressure gas;
Gas compression unit (4), stores for sending into this gas storage unit (3) after the gas compression of being discharged by this aerating ballon (2);
Control unit (5), gas that aerating ballon (2) discharges can be controlled send into this gas compression unit (4) and carry out compressing and the gas of compression is sent into gas storage unit (3), this gas compression unit (4) can also be controlled this aerating ballon (2) is inflated;
Wireless signal Transmit-Receive Unit (6), can realize this gas pressure relief type aircraft and the external world contacts;
Power supply (15), powers for giving this gas pressure relief type aircraft.
2. gas pressure relief type aircraft according to claim 1, it is characterized in that, described gas pressure relief type aircraft also comprises aircraft device body (10), and gas storage unit (3), gas compression unit (4) and control unit (5) are all arranged in aircraft device body (10).
3. gas pressure relief type aircraft according to claim 2, it is characterized in that, this is main rises balloon (1) and aerating ballon (2) adjoins up and down, and aircraft device body (10) is positioned at this main below rising balloon (1) and aerating ballon (2);
Or this is main rises balloon (1) and aerating ballon (2) left and right is adjacent, and aircraft device body (10) is positioned at this main below rising balloon (1) and aerating ballon (2).
4. gas pressure relief type aircraft according to claim 2, it is characterized in that, the main balloon (1) that rises is connected with aircraft device body (10) by balloon cover body (12) and connecting device (11) with aerating ballon (2), balloon cover body (12) covers on and mainly rises balloon (1) and aerating ballon (2) outward, connecting device (11) is arranged on balloon cover body (12) lower end, and balloon cover body (12) is connected with aircraft device body (10) by connecting device (11).
5. gas pressure relief type aircraft according to claim 4, is characterized in that, balloon cover body (12) is connected with connecting device (11), and connecting device (11) is for connecting tightrope.
6. gas pressure relief type aircraft according to claim 2, it is characterized in that, gas storage unit (3), gas compression unit (4) and control unit (5) are all arranged in aircraft device body (10), and wireless signal Transmit-Receive Unit (6) is arranged on outside the surface of aircraft device body (10).
7. gas pressure relief type aircraft according to claim 4, it is characterized in that, described gas pressure relief type aircraft also comprises for the solar panel of this power source charges, this solar panel be arranged at balloon cover body (12) outward and/or aircraft device body (10) outward.
8. gas pressure relief type aircraft according to claim 1, it is characterized in that, described gas pressure relief type aircraft also comprises testing and alarm unit (14), this testing and alarm unit (14) is connected with control unit (5), and this testing and alarm unit (14) can send alerting signal when this gas pressure relief type aircraft occurs abnormal.
9. gas pressure relief type aircraft according to claim 2, it is characterized in that, aircraft device body (10) is provided with the rotor driver (7) for driving flight and change of flight direction, the bottom of aircraft device body (10) is provided with the running gear (8) that this gas pressure relief type aircraft can be made to walk on the ground, and described gas pressure relief type aircraft also comprises the remote controller for this gas pressure relief type aircraft of remote control.
10. gas pressure relief type aircraft according to claim 1, is characterized in that, the quantity of aerating ballon (2) is no more than 2.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520661477.4U CN204916153U (en) | 2015-08-28 | 2015-08-28 | Formula aircraft is put to gaseous pressure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520661477.4U CN204916153U (en) | 2015-08-28 | 2015-08-28 | Formula aircraft is put to gaseous pressure |
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| Publication Number | Publication Date |
|---|---|
| CN204916153U true CN204916153U (en) | 2015-12-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520661477.4U Expired - Fee Related CN204916153U (en) | 2015-08-28 | 2015-08-28 | Formula aircraft is put to gaseous pressure |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828861A (en) * | 2017-01-13 | 2017-06-13 | 中国地质大学（武汉） | A kind of hydrogen helium mixture aerostatics |
| CN112304354A (en) * | 2020-10-19 | 2021-02-02 | 湖南广播电视大学（湖南网络工程职业学院） | Forest site monitoring device and monitoring system based on wireless sensor network |
| CN115301079A (en) * | 2022-08-10 | 2022-11-08 | 湖北工业大学 | A purifier for atmosphere is administered |
-
2015
- 2015-08-28 CN CN201520661477.4U patent/CN204916153U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828861A (en) * | 2017-01-13 | 2017-06-13 | 中国地质大学（武汉） | A kind of hydrogen helium mixture aerostatics |
| CN112304354A (en) * | 2020-10-19 | 2021-02-02 | 湖南广播电视大学（湖南网络工程职业学院） | Forest site monitoring device and monitoring system based on wireless sensor network |
| CN115301079A (en) * | 2022-08-10 | 2022-11-08 | 湖北工业大学 | A purifier for atmosphere is administered |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151230 Termination date: 20160828 |
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| CF01 | Termination of patent right due to non-payment of annual fee |