CN202481308U

CN202481308U - Air energy aircraft

Info

Publication number: CN202481308U
Application number: CN2012200217927U
Authority: CN
Inventors: 刘新广
Original assignee: Individual
Current assignee: Individual
Priority date: 2012-01-18
Filing date: 2012-01-18
Publication date: 2012-10-10
Anticipated expiration: 2022-01-18

Abstract

The utility model discloses an air energy aircraft. A sealing shell is provided with a compressed air inlet and supporting legs; a cabin is attached to the sealing shell; a left valve and a right valve are arranged on the sealing shell, each valve is communicated with the sealing shell, outlets of the valves are forward opened along the horizontal direction, a hollow propeller is connected to the front ends of the valves, air injection holes are formed at two ends of the propeller, and the propeller can rotate around the front ends of the valves; or a left valve and a right valve which are communicated with the sealing shell are arranged on the sealing shell, an outlet of each valve is backward opened along the horizontal direction; the air injection holes are formed at two ends of the hollow propeller, the propeller is connected to the upper end of a vertical hollow shaft, the inner cavity of the propeller is communicated with that of the vertical hollow shaft, the propeller can rotate around the vertical hollow shaft, a locking device is arranged on the vertical hollow shaft, the lower end of the vertical hollow shaft is connected with an upper valve, and the upper valve is communicated with the sealing shell; a controller and a storage battery are arranged in the cabin; and the controller is connected with the storage battery, and an air pressure sensor, a temperature sensor and a humidity sensor which are arranged in a detection shell, the locking devices and the valves through leads.

Description

Air can aircraft

Technical field

The utility model relates to the aviation aircraft technology, and particularly a kind of air can aircraft.。

Background technology

Existing aircraft is an engine with hot machine (turbine engine, turboaxle motor, piston engine) or electric device, and hot machine is the energy with fuel, and electric device is the energy with the electric energy of battery.Because with hot machine or electric device be the Flight Vehicle Structure of engine complicated, than great, so existing aircraft load ratio (quality of material that aircraft carries and the ratio of vehicle mass) little (quality of material that existing aircraft carries be about aircraft own wt 25%), energy consumption are big.With turbine or screw propeller that hot machine or electric device drive, the vibration of generation is big.

Summary of the invention

In order to overcome the above-mentioned defective of existing aircraft, the utility model designs a kind of air ability aircraft, is power with pressurized air and solar power, and this FLIGHT VEHICLE VIBRATION is little, flight is flexible, load ratio is big, energy consumption is little, environmental protection.

The utility model is realized through following technical proposals.

Make a seal casinghousing, the sealing housing is towards several supporting legs of ground side protrusion, and the inner chamber of supporting leg is the cavity part of seal casinghousing, on said seal casinghousing, has pressurized air to advance mouth; The cabin is attached on the seal casinghousing, and the cabin does to drive the chamber, (like electron camera, navigating instrument etc.) equipment or manned or lade and equipment usefulness install instruments.Flying activation configuration before the said air ability aircraft is: a left valve, a right valve are set on said seal casinghousing; The import of each valve directly or with managing communicates with the cavity of seal casinghousing, the outlet along continuous straight runs of each valve forward, the outlet of each valve all is horizontal hollow tubulars; Revolve oar in the front end contact one of each horizontal hollow tubular respectively; It is hollow revolving oar, have and revolve the fumarole of the hollow UNICOM of oar in the two ends end sides of revolving oar, and it is in the opposite direction to revolve the fumarole of two ends end sides of oar; Revolve the hollow UNICOM of the hollow and horizontal hollow tubular of oar, revolving oar can be around horizontal hollow tubular rotation; No. two left valves, No. two right valves perhaps are set on said seal casinghousing, and the import of each valve communicates with the cavity of seal casinghousing with pipe, and the outlet of each valve is as the spout outside seal casinghousing, and said spout along continuous straight runs backward.On the top of seal casinghousing main rotor mechanism is set; Its rotor is hollow, and end sides has the fumarole with the hollow UNICOM of rotor at the two ends of rotor, and the jet aperture of the two ends end sides of rotor is in the opposite direction; Its rotor contact is in the upper end of vertical hollow shaft; The hollow UNICOM of the hollow and vertical hollow shaft of rotor, rotor can be around the rotation of vertical hollow shaft, only locks device and is installed on the vertical hollow shaft and near the rotor downside; The lower end of vertical hollow shaft connects with the suitable for reading of last valve, the end opening of last valve connect with seal casinghousing and with its cavity UNICOM; Controller, storage battery are set in said cabin; BARO sensor, temperature sensor, humidity sensor penetrate said seal casinghousing from said cabin respectively and probe in it, BARO sensor, temperature sensor, humidity sensor all with the seal casinghousing sealed attachment; Controller respectively with storage battery, BARO sensor, temperature sensor, humidity sensor, only lock device, valve is connected with lead.

Said air can be taken advantage of the direct beam riding of people by aircraft, also can pass through remotely pilotless beam riding, and people's beam riding and remotely pilotless beam riding all realize through controller.Advance the mouth injecting compressed air from pressurized air.BARO sensor, temperature sensor, humidity sensor be pressure, temperature, the humidity of the interior gas of perception seal casinghousing respectively, and deliver to controller and monitor, and controls controller and controller come control cock according to pressure, temperature, the humidity of gas aperture.Left valve of controller control, a right valve output pressurized air when pressurized air outwards sprays from the fumarole that revolves oar, are revolved oar choosing commentaries on classics because antagonistic force makes, and also can make air fly, to turn before the aircraft.Controller is controlled No. two left valves, No. two right valves are jet, can make air fly, to turn to before the aircraft.Current degree at full speed acquires a certain degree, and closes to close valve, and rotor rotates freely generation lift, and current degree at full speed is increased to another degree again, and the locked rotor of controlled prevention lock device becomes fixed-wing.Valve output pressurized air is gone up in controller control, and pressurized air because antagonistic force makes the rotor rotation produce upper pulling force, makes air can aircraft rise or hover when the fumarole of rotor outwards sprays.Valve opening is gone up in controller control can make air descend with gravity by aircraft.Control the aperture of each valve of controller control, can obtain various flying speeds.

Tasks such as air can aircraft can carry out scouting, monitor, patrol, search and rescue, sow.

The effect that the utility model is useful:

1, air ability Flight Vehicle Structure is extremely simple, and cost is very little.

2, the quality of the seal casinghousing of air ability aircraft; Can accomplish suitable even little with the casing and the alighting gear quality of existing aircraft; But air can aircraft all valves, to revolve oar, rotor total mass little more than the total mass of the driving engine of existing aircraft and transmission device; It is much little that the compressed air quality that it carries carries fuel mass than existing aircraft, and the proportion of air ability aircraft is more than having the little of aircraft now, so the existing aircraft of its load ratio is much bigger, energy consumption is little in a word.

3, existing aircraft run up time is at 1-10 minute, and air can be short to and can take off immediately by aircraft run up time, and this gives power to carrying out an urgent task very much, and existing aircraft can't be reached.

4, the driving engine of existing aircraft is turbine engine or turboaxle motor or piston engine, thereby vibration, noise are big, and air can FLIGHT VEHICLE VIBRATION, and noise is compared less.

When 5, can aircraft annotating pressurized air for air, the room temperature environment of being everlasting, after the completion, air can aircraft if to outdoor, the heat that its can absorbing environmental or the heat of sunshine make its internal compression atmosphere temperature rising and produce pressure excess, this is equivalent to energization.So air can gratis utilize solar power or environment thermal energy by aircraft in passing.This is its another outstanding advantage.

6, control simply, flight flexibly.

7, the structure and the principle of work of said air ability aircraft have determined it longer than existing aircraft reliable operation, life-span.

8, manufacturing process, use, scrap the back almost non-toxic evil, so environmental protection.

9, owing to above-mentioned advantage, so said air ability aircraft cost performance is high.

Description of drawings

Fig. 1 is the structural representation of embodiment 1;

Fig. 2 is the birds-eye view of Fig. 1;

Fig. 3 is the A-A cutaway view of Fig. 2;

Fig. 4 is the structural representation of embodiment 2;

Fig. 5 is the B-B section-drawing of Fig. 4.

The specific embodiment

Embodiment 1:

Show like Fig. 1 to Fig. 3.Make seal casinghousing 1, seal casinghousing 1 protrudes several supporting legs 2 towards ground side, and the inner chamber of supporting leg 2 is communicated with the cavity of seal casinghousing 1; Seal casinghousing 1 left and right sides is stretched out port wing 5, starboard wing 12 respectively, and port wing 5, starboard wing 12 inner chambers all are communicated with the cavity of seal casinghousing 1; On seal casinghousing 1, there is a pressurized air to advance mouth 3; Cover plate 15 connects with the upper forepart of seal casinghousing 1 forms do

driving chambers

21,21, numbers cabins, a cabin, the equipment that installs instruments (like electron camera, navigating instrument etc.) or manned or lade and equipment usefulness; Controller 19, a storage battery 20 are set in a cabin 21; BARO sensor 22, temperature sensor 23, a humidity sensor 24 penetrate seal casinghousing 1 from a cabin 21 respectively and probe in it, they and seal casinghousing 1 sealed attachment; On the top of seal casinghousing 1 main rotor mechanism is set; One of which rotor 7 is hollow; End sides has and a fumarole of the hollow UNICOM of rotor 8, No. two fumaroles 11 at the two ends of a rotor 7; And a fumarole 8 and No. two fumarole 11 apertures is in the opposite direction, and one of which rotor 7 is got in touch in the upper end of a vertical hollow shaft 10, the hollow UNICOM of a hollow and vertical hollow shaft 10 of a rotor 7; No. one rotor 7 can be around vertical hollow shaft 10 rotations; Only lock device 7-1 for No. one and be installed on the vertical hollow shaft 10 and near rotor 7 downsides, the lower end of a vertical hollow shaft 10 with go up the suitable for reading of valve 9 No. one and connect, go up for No. one valve 9 end opening and seal casinghousing 1 and with its cavity UNICOM; Flying activation configuration before said air is can aircraft a kind of is: left valve 18, a right valve 16 are set respectively on port wing 5, starboard wing 12; The import 14 of the import 4 of a left valve 18, a right valve 16 communicates with the inner chamber of port wing 5, starboard wing 12 respectively; The equal along continuous straight runs of outlet of left valve 18, a right valve 16 forward, the outlet of left valve 18, a right valve 16 all is horizontal hollow tubulars; Front end contact at the horizontal hollow tubular of a left valve 18 is revolved oar 6 No. one; No. one revolves oar 6 is hollow; Have and revolve No. three fumarole 6-1 of the hollow UNICOM of oar 6, No. four fumarole 6-2 No. one in the two ends end sides of revolving oar 6 for No.; The direction of No. three fumarole 6-1 and No. four fumarole 6-2's is opposite, revolves the hollow UNICOM of the hollow of oar 6 and the horizontal hollow tubular of a left valve 18 for No. one, and revolving oar 6 No. one can be around the horizontal hollow tubular rotation of a left valve 18; Front end contact at the horizontal hollow tubular of a right valve 16 is revolved oar 13 No. two; No. two revolve oar 13 is hollow; Have and revolve No. five fumarole 13-1 of the hollow UNICOM of oar 13, No. six fumarole 13-2 No. two in the two ends end sides of revolving oar 13 for No. two; The direction of No. five fumarole 13-1 and No. six fumarole 13-2's is opposite, revolves the hollow UNICOM of the hollow of oar 13 and the horizontal hollow tubular of a right valve 16 for No. two, and revolving oar 13 No. two can be around the horizontal hollow tubular rotation of a right valve 16; Controller 19 respectively with storage battery 20, BARO sensor 22, temperature sensor 23, humidity sensor 24, go up the right valve of the left valve of valve 9, No. one 18, No. one 16 for No. one, only lock device 7-1 and be connected for No. one with lead.

Advance mouth 3 injecting compressed airs from a pressurized air.BARO sensor 22, temperature sensor 23, humidity sensor 24 be pressure, temperature, the humidity of gas in the perception seal casinghousings 1 respectively, and deliver to a controller 19 and monitor.Control controller 19 No. one, and controller 19 is according to pressure, temperature, the humidity of gas and control instruction and control each valve opening.Open and go up valve 9 for No. one, pressurized air is from a fumarole of a rotor 78, No. two fumarole 11 ejections, thereby causes rotor 7 rotations to produce lift; If close all the other valves; Air can vertically be risen by aircraft,, air can be hovered by aircraft through controlling the upward aperture of valve 9 No. one; Control left valve 18, a right valve 16; Pressurized air is from said fumarole ejection of revolving oar, saidly revolves the oar rotation and produces pulling force forward thereby cause, and air is flown before can the aircraft level or turns to (if the right valve of No. one, left valve 18 opening ratio 16 is big; Right-hand turning then, otherwise also anti-); Current degree at full speed acquires a certain degree, and closes last 9, numbers rotors 7 of valve and rotates freely generation lift, and current degree at full speed is increased to another degree again, and may command is only locked 7 one-tenth fixed-wings of the locked rotor of device 7-1 for No. one.Control controller 19 No. one, control the aperture that goes up valve 9 for No., close all the other valves simultaneously, can make air can aircraft at the uniform velocity or quicken (leaning on gravity) vertical landing.Control each valve aperture, can make air can aircraft obtain the flying speed of various flights.

This air can be prone to control owing to valve is few by aircraft, and proportion is littler.Flight is imitated on the most suitable near-earth of this aircraft ground, can reduce energy consumption greatly, can promote to be used for individual's flight.

Embodiment 2:

Show like Fig. 4, Fig. 5.Making one has the spherical seal casinghousing 25 of a depression, and spherical seal casinghousing 25 protrudes several supporting legs 28 towards ground side, and the inner chamber of supporting leg 28 is communicated with the cavity of spherical seal casinghousing 25, on spherical seal casinghousing 25, has No. two pressurized airs to advance mouth 34; Curved cover plate 26 covers the depression of spherical seal casinghousing 25; And curved cover plate 26 lids connect with spherical seal casinghousing 25; Curved cover plate 26 is formed 27, No. two cabins, No. two cabins 27 with the depression of spherical seal casinghousing 25 and is made to drive chamber, the equipment that installs instruments (like electron camera, navigating instrument etc.) or manned or lade and equipment usefulness; No. two controllers 29, No. two storage batterys 30 are set in No. two cabins 27; No. two BARO sensors 31, No. two temperature sensors 32, No. two humidity sensors 33 penetrate spherical seal casinghousing 25 from No. two cabins 27 respectively and probe in it, No. two BARO sensors 31, No. two temperature sensors 32, No. two humidity sensors 33 all with spherical seal casinghousing 25 sealed attachment; The another kind of structure that said air flies actuator before can aircraft is: in left rear side, the right lateral side of spherical seal casinghousing 25 No. two left valves 42, No. two right valves 35 are set respectively; The outlet of No. two left valves 42, No. two right valves 35 is outside spherical seal casinghousing 25 and be in horizontal direction; No. two left valves 42, No. two right valves 35 connect with the UNICOM of spherical seal casinghousing 25 with left levelling pipe 43, right levelling pipe 44 respectively, and the outlet of No. two left valves 42, No. two right valves 35 is respectively as the left back spout of level, the right back spout of level outside spherical seal casinghousing 25; On the top of spherical seal casinghousing 25 main rotor mechanism is set; Its No. two rotors 40 are hollow; End sides has and No. seven fumaroles of the hollow UNICOM of rotor 38, No. eight fumaroles 39 at the two ends of No. two rotors 40; And No. seven fumaroles 38 and No. eight fumarole 39 apertures is in the opposite direction, and its No. two rotors 40 are got in touch in the upper end of No. two vertical hollow shafts 41 the hollow UNICOM of the hollow and No. two vertical hollow shafts 41 of No. two rotors 40; No. two rotor 40 can be around No. two vertical hollow shaft 41 rotations; Only lock device 40-1 for No. two and be installed on No. two vertical hollow shafts 41 and near No. two rotor 40 downsides, the lower end of No. two vertical hollow shafts 41 with go up the suitable for reading of valve 37 No. two and connect, the end opening of going up valves 37 for No. two connects with spherical seal casinghousing 25 and with its cavity UNICOM; No. two controllers 29 respectively with No. two storage batterys 30, No. two BARO sensors 31, No. two temperature sensors 32, No. two humidity sensors 33, go up the right valve of the left valve of valve 37, No. two 42, No. two 35 for No. two, only lock device 40-1 and be connected for No. two with lead.

Advance mouth 34 injecting compressed airs from No. two pressurized airs.No. two BARO sensors 31, No. two temperature sensors 32, No. two humidity sensors 33 be pressure, temperature, the humidity of gas in the spherical seal casinghousings 25 of perception respectively, and deliver to No. two controllers 29 and monitor.Control controller 29 No. two, and No. two controllers 29 are according to pressure, temperature, the humidity of gas and control instruction and control each valve opening.Open No. two and go up valve 37; Pressurized air is from No. seven fumaroles of No. two rotors 40 38, No. eight fumarole 39 ejections; Thereby cause No. two rotor 40 rotations to produce lift,, air can vertically be risen by aircraft if close all the other valves; Through controlling the upward aperture of valve 37 No. two, air can be hovered by aircraft.Control the left valve of No. 29, two, No. two controllers 42, No. two right valves 35 are jet backward, and air can be flown before the aircraft level; Control the aperture of No. two left valves 42, No. two right valves 35; Can make air can aircraft turn to (if the right valve of No. two, No. two left valve 42 opening ratios 35 is big, right-hand turning then, otherwise also anti-); Current degree at full speed acquires a certain degree, and closes No. two last 37, No. two rotors 40 of valve and rotates freely generation lift, and current degree at full speed is increased to another degree again, and may command is only locked 40 one-tenth fixed-wings of locked No. two rotors of device 40-1 for No. two.Control controller 29 No. two, control the aperture that goes up valves 37 for No. two, close all the other valves simultaneously, can make air can aircraft at the uniform velocity or quicken (leaning on gravity) vertical landing.Control each valve aperture, can make air can aircraft obtain the flying speed of various flights.

This air can be suitable for carrying out the less demanding task of flying speed by aircraft.

Claims

1. air can aircraft, it is characterized in that:

Make a seal casinghousing, the sealing housing is towards several supporting legs of ground side protrusion, and the inner chamber of supporting leg is the cavity part of seal casinghousing, on said seal casinghousing, has pressurized air to advance mouth; The cabin is attached on the seal casinghousing; Flying activation configuration before the said air ability aircraft is: a left valve, a right valve are set on said seal casinghousing; The import of each valve directly or with managing communicates with the cavity of seal casinghousing, the outlet along continuous straight runs of each valve forward, the outlet of each valve all is horizontal hollow tubulars; Revolve oar in the front end contact one of each horizontal hollow tubular respectively; It is hollow revolving oar, have and revolve the fumarole of the hollow UNICOM of oar in the two ends end sides of revolving oar, and it is in the opposite direction to revolve the fumarole of two ends end sides of oar; Revolve the hollow UNICOM of the hollow and horizontal hollow tubular of oar, revolving oar can be around horizontal hollow tubular rotation; No. two left valves, No. two right valves perhaps are set on said seal casinghousing, and the import of each valve communicates with the cavity of seal casinghousing with pipe, and the outlet of each valve is as the spout outside seal casinghousing, and said spout along continuous straight runs backward; On the top of seal casinghousing main rotor mechanism is set; Its rotor is hollow, and end sides has the fumarole with the hollow UNICOM of rotor at the two ends of rotor, and the jet aperture of the two ends end sides of rotor is in the opposite direction; Its rotor contact is in the upper end of vertical hollow shaft; The hollow UNICOM of the hollow and vertical hollow shaft of rotor, rotor can be around the rotation of vertical hollow shaft, only locks device and is installed on the vertical hollow shaft and near the rotor downside; The lower end of vertical hollow shaft connects with the suitable for reading of last valve, the end opening of last valve connect with seal casinghousing and with its cavity UNICOM; Controller, storage battery are set in said cabin; BARO sensor, temperature sensor, humidity sensor penetrate said seal casinghousing from said cabin respectively and probe in it, BARO sensor, temperature sensor, humidity sensor all with the seal casinghousing sealed attachment; Controller respectively with storage battery, BARO sensor, temperature sensor, humidity sensor, only lock device, valve is connected with lead.

2. according to the said air ability of claim 1 aircraft, it is characterized in that: make seal casinghousing (1), seal casinghousing (1) protrudes several supporting legs (2) towards ground side, and the inner chamber of supporting leg (2) is communicated with the cavity of seal casinghousing (1); Seal casinghousing (1) left and right sides is stretched out port wing (5), starboard wing (12) respectively, and port wing (5), starboard wing (12) inner chamber all are communicated with the cavity of seal casinghousing (1); On seal casinghousing (1), there is a pressurized air to advance mouth (3); Cover plate (15) connects with the upper forepart of seal casinghousing 1 forms a cabin (21); A controller (19), a storage battery (20) are set in a cabin (21); A BARO sensor (22), a temperature sensor (23), a humidity sensor (24) penetrate seal casinghousing (1) from a cabin (21) respectively and probe in it, they and seal casinghousing (1) sealed attachment; Top at seal casinghousing (1) is provided with main rotor mechanism; One of which rotor (7) is hollow; In the two ends end sides of a rotor (7) a fumarole (8), No. two fumaroles (11) with the hollow UNICOM of rotor are arranged; And a fumarole (8) is in the opposite direction with No. two fumaroles (11) aperture, and one of which rotor (7) is got in touch in the upper end of a vertical hollow shaft (10), the hollow UNICOM of a hollow and vertical hollow shaft (10) of a rotor (7); A rotor (7) can rotate around a vertical hollow shaft (10); Only lock that device (7-1) is installed in that vertical hollow shaft (10) is gone up for No. one and near a rotor (7) downside, the lower end of a vertical hollow shaft (10) and suitable for reading connection of going up valve (9) No., on No. one the end opening of valve (9) and seal casinghousing (1) and with its cavity UNICOM; Flying activation configuration before said air ability aircraft is a kind of is: a left valve (18), a right valve (16) are set respectively on port wing (5), starboard wing (12); The import (4) of a left valve (18), the import (14) of a right valve (16) communicate with the inner chamber of port wing (5), starboard wing (12) respectively; The equal along continuous straight runs of outlet of a left valve (18), a right valve (16) forward, the outlet of a left valve (18), a right valve (16) all is horizontal hollow tubulars; Front end contact at the horizontal hollow tubular of a left valve (18) is revolved oar (6) No. one; It is hollow revolving oar (6) for No. one; Have and revolve No. three fumaroles (6-1), No. four fumaroles (6-2) of the hollow UNICOM of oar (6) No. one in the two ends end sides of revolving oar (6) for No.; The direction of No. three fumaroles (6-1) and No. four fumaroles (6-2) opposite, the hollow UNICOM of revolving the hollow of oar (6) and the horizontal hollow tubular of a left valve (18) for No., revolving oar (6) No. one can be around the horizontal hollow tubular rotation of a left valve (18); Front end contact at the horizontal hollow tubular of a right valve (16) is revolved oar (13) No. two; It is hollow revolving oar (13) for No. two; Have and revolve No. five fumaroles (13-1), No. six fumaroles (13-2) of the hollow UNICOM of oar (13) No. two in the two ends end sides of revolving oar (13) for No. two; The direction of No. five fumaroles (13-1) and No. six fumaroles (13-2) opposite; Revolve the hollow UNICOM of the horizontal hollow tubular of the hollow of oar (13) and a right valve (16) for No. two, revolving oar (13) No. two can be around the horizontal hollow tubular rotation of a right valve (16); A controller (19) goes up valve (9), a left valve (18), a right valve (16) with a storage battery (20), a BARO sensor (22), a temperature sensor (23), a humidity sensor (24), No. one respectively, only lock device (7-1) for No. one is connected with lead.

3. according to the said air ability of claim 1 aircraft; It is characterized in that: making one has the spherical seal casinghousing (25) of a depression; Spherical seal casinghousing (25) protrudes several supporting legs (28) towards ground side; The inner chamber of supporting leg (28) is communicated with the cavity of spherical seal casinghousing (25), on spherical seal casinghousing (25), has No. two pressurized airs to advance mouth (34); Curved cover plate (26) covers the depression of spherical seal casinghousing (25), and curved cover plate (26) lid connects depression composition No. two cabins (27) of curved cover plate (26) and spherical seal casinghousing (25) with spherical seal casinghousing (25); No. two controllers (29), No. two storage batterys (30) are set in No. two cabins (27); No. two BARO sensors (31), No. two temperature sensors (32), No. two humidity sensors (33) penetrate spherical seal casinghousing (25) from No. two cabins (27) respectively and probe in it, No. two BARO sensors (31), No. two temperature sensors (32), No. two humidity sensors (33) all with spherical seal casinghousing (25) sealed attachment; The another kind of structure that flies actuator before the said air ability aircraft is: left rear side, the right lateral side in spherical seal casinghousing (25) is provided with No. two left valves (42), No. two right valves (35) respectively; The outlet of No. two left valves (42), No. two right valves (35) is outside spherical seal casinghousing (25) and be in horizontal direction; No. two left valves (42), No. two right valves (35) use left levelling pipe (43), right levelling pipe (44) to connect with the UNICOM of spherical seal casinghousing (25) respectively, and the outlet of No. two left valves (42), No. two right valves (35) is respectively as the left back spout of level, the right back spout of level outside spherical seal casinghousing (25); Top at spherical seal casinghousing (25) is provided with main rotor mechanism; Its No. two rotors (40) are hollow; In the two ends end sides of No. two rotors (40) No. seven fumaroles (38), No. eight fumaroles (39) with the hollow UNICOM of rotor are arranged; And No. seven fumaroles (38) are in the opposite direction with No. eight fumaroles (39) aperture, and its No. two rotors (40) are got in touch in the upper end of No. two vertical hollow shafts (41), the hollow UNICOM of the hollow and No. two vertical hollow shafts (41) of No. two rotors (40); No. two rotors (40) can rotate around No. two vertical hollow shafts (41); Only lock device (40-1) for No. two and be installed on No. two vertical hollow shafts (41) and near No. two rotors (40) downside, the lower end of No. two vertical hollow shafts (41) and suitable for reading connection of going up valves (37) No. two, the end opening of No. two last valves (37) connects with spherical seal casinghousing (25) and with its cavity UNICOM; No. two controllers (29) go up valve (37), No. two left valves (42), No. two right valves (35) with No. two storage batterys (30), No. two BARO sensors (31), No. two temperature sensors (32), No. two humidity sensors (33), No. two respectively, only lock device (40-1) for No. two is connected with lead.