CN202529148U

CN202529148U - Air energy and solar energy composite aircraft

Info

Publication number: CN202529148U
Application number: CN2011205347104U
Authority: CN
Inventors: 刘新广
Original assignee: Individual
Current assignee: Individual
Priority date: 2011-12-20
Filing date: 2011-12-20
Publication date: 2012-11-14
Anticipated expiration: 2021-12-20

Abstract

The utility model discloses an air energy and solar energy composite aircraft which comprises a sealed shell. A plurality of support legs of the sealed shell project towards the ground, an inner cavity of each support leg is a part of a cavity of the sealed shell, the sealed shell is provided with a compressed air inlet nozzle and a plurality of valves, a cabin is attached onto the sealed shell and is used as a driving room and for installing instruments and loading goods or equipment, an inlet of each valve is communicated with the cavity of the sealed shell directly or by the aid of a tube, an outlet of each valve is used as an outer nozzle of the sealed shell, some of the nozzles vertically face the ground, some of the nozzles are horizontal, some of the horizontal nozzles are leftward, some of the horizontal nozzles are rightward, some of the horizontal nozzles are forward, some of the horizontal nozzles are backward, a controller and a storage battery are arranged in the cabin, an air pressure sensor, a temperature sensor and a humidity sensor respectively penetrate through the sealed shell from the cabin and extend into the sealed shell, and the controller is respectively connected with the storage battery, the air pressure sensor, the temperature sensor, the humidity sensor and the valves by the aid of leads.

Description

Air can with the solar power composite aircraft

Technical field

Relate to the aviation aircraft technology, particularly a kind of air can with the solar power composite 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, design a kind of air can with the solar power composite aircraft, be power with pressurized air and solar power, this Flight Vehicle Structure is simple, load ratio is big, energy consumption is little, vibration is little, fly more flexible, environmental protection.

Realize 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 is made to drive chamber, (like electron camera, the navigating instrument etc.) equipment that installs instruments, lade or equipment and used; On said seal casinghousing, plurality of valves is set, the import of each valve directly or with pipe communicates with the cavity of seal casinghousing, and the outlet of each valve is as the spout outside seal casinghousing; Said spout, the edge that has is vertical towards ground, the along continuous straight runs that has, the spout of along continuous straight runs has left, has to the right, has forward, has backward; The quantity of said valve and layout require to confirm according to the shape of seal casinghousing or flicon, and promptly quantity can increase and decrease, layout can change; 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 is connected with lead with storage battery, BARO sensor, temperature sensor, humidity sensor, valve respectively.

Said air can be taken advantage of the direct beam riding of people with the solar power composite 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 the controller injection flow that comes control cock according to pressure, temperature, the humidity of gas with the acquisition needs reaction thrust.Each valve of controller control is jet; Can make that air can vertically with the solar power composite aircraft rise, precedingly flies, turns, climbs, hovers, rotates, underriding, horizontal left, level move to right, level is retreated, vertical landing, and obtain various flying speeds through the injection flow of each valve of controller control.Because flight flexibly, if electron camera is installed in the cabin, air can be adapted to scout, monitor, patrols, searches and rescues, sows etc. with the solar power composite aircraft especially.

The effect that the utility model is useful:

1, air can be extremely simple with solar power composite aircraft structure, and non-aviation specialty originating firm can both be made easily, and cost is minimum.

2, air can with the quality of the seal casinghousing of solar power composite aircraft; Can accomplish suitable even little many with the casing and the alighting gear quality of existing aircraft; But air can be little more than the total mass of driving engine that has aircraft now and transmission device with all valve total masss of solar power composite aircraft; It is much little that the compressed air quality that it carries carries fuel mass than existing aircraft; In a word air can with little more than existing aircraft of the proportion of solar power composite aircraft, so its load (estimating greater than 60%) is more much bigger than existing aircraft, energy consumption is little.

3, existing aircraft run up time is at 1-10 minute, and air can be short to and can take off immediately with the solar power composite 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 driven by engine turbine or the propeller of existing aircraft, thereby vibration, noise are big, and air can with solar power composite aircraft friction almost, noise is compared less.

5, because the height of the power density ratio electric device formula of hot machine (turbine engine, turboaxle motor, piston engine) formula engine adopts hot machine formula engine so have the aircraft overwhelming majority now.But the power of hot machine formula engine receives ambient air density, temperature effect big, when ambient air density diminishes, during temperature build-up, horsepower output reduces very serious, efficient reduces greatly.And air can have nothing to do with power and ambient air density, the temperature of solar power composite aircraft, power stability, efficient height.

When 6, can annotate pressurized air with the solar power composite aircraft for air, the room temperature environment of being everlasting is after the completion; If air can be with the solar power composite aircraft to outdoor; It can absorbing environmental heat 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 in passing with the solar power composite aircraft.This is its another outstanding advantage.

7, said air can control simply with the solar power composite aircraft, and flight flexibly.

8, said air can determine it longer than existing aircraft reliable operation, life-span with the structure and the principle of work of solar power composite aircraft.

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

10, owing to above-mentioned advantage, so said air can be high with solar power composite aircraft cost performance.

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 section-drawing of Fig. 2;

Fig. 4 is the B-B section-drawing of Fig. 2;

Fig. 5 is the C-C section-drawing of Fig. 2;

Fig. 6 is the D-D section-drawing of Fig. 1;

Fig. 7 is the E-E section-drawing of Fig. 1;

Fig. 8 is the structural representation of embodiment 2;

Fig. 9 is the F-F section-drawing of Fig. 8;

Figure 10 is the structural representation of embodiment 3;

Figure 11 is the birds-eye view of Figure 10;

Figure 12 is the left view of Figure 10;

Figure 13 is the G-G cutaway view of Figure 11;

Figure 14 is the upward view of Figure 10.

The specific embodiment

Embodiment 1:

Show like Fig. 1 to Fig. 7.Make a seal casinghousing 1 of a fixed wing aircraft shape; The inner chamber of the left front wing 3, the right front wing 9, the left back wing 5, the right back wing 10, a vertical tail 4 all is communicated with the cavity of a seal casinghousing 1; A seal casinghousing 1 is towards ground side protrusion front leg strut 8 and rear support leg 7; The inner chamber of the inner chamber of front leg strut 8, rear support leg 7 all is communicated with the cavity of a seal casinghousing 1, on a seal casinghousing 1, has pressurized air to advance mouth 6 No. one; Cover plate 11 connects with the upper forepart of a seal casinghousing 1 forms do

driving chambers

2,2, numbers cabins, a cabin, the equipment that installs instruments (like electron camera, navigating instrument etc.), lade or equipment usefulness; Valve 20, back valve 17, left front valve 22, right front valve 21, left back valve 24, a right back valve 23 before front side, rear side, left side, the right side of a seal casinghousing 1 are provided with No. one respectively; Valve 18 under valve 19, the back under before preceding downside, the back downside of a seal casinghousing 1 are provided with respectively; The import of said each valve communicates with the cavity of a seal casinghousing 1; The outlet of valve 20 before No., back valve 17, left front valve 22, right front valve 21, left back valve 24, a right back valve 23 is as the horizontal spout outside seal casinghousing 1; Before down valve 19, back down the outlet of valve 18 as spout under outer vertical of seal casinghousing 1, said each valve and seal casinghousing 1 sealed attachment; Controller 15, a storage battery 16 are set in a cabin 2; BARO sensor 12, temperature sensor 13, a humidity sensor 14 penetrate a seal casinghousing 1 from a cabin 2 respectively and probe in it, they and seal casinghousing 1 sealed attachment; Controller 15 all is connected with lead with storage battery 16, BARO sensor 12, temperature sensor 13, humidity sensor 14, said each valve respectively.

Said air can be taken advantage of the direct beam riding of people with the solar power composite aircraft, also can pass through remotely pilotless beam riding, and beam riding and remotely pilotless beam riding all realize through controller.Advance mouth 6 injecting compressed airs for No. one from pressurized air.BARO sensor 12, temperature sensor 13, humidity sensor 14 be pressure, temperature, the humidity of gas in seal casinghousings of perception 1 respectively; And deliver to a controller 15 and monitor, and controller 15 is controlled each valve according to pressure, temperature, the humidity of gas injection flow is to obtain suitable reaction thrust.Control controller 15 No. one; Following valve 19, back descend valve 18 jet downwards before opening, and close all the other valves simultaneously, and air can be risen with the solar power composite aircraft is vertical; Following valve 19, the back downward jet amount of valve 18 down before the control can make air hover with the solar power composite aircraft; Control controller 15 No. one; Following valve 19, the following valve 18 downward jet air that make in back can be in required height with the solar power composite aircraft before opening; And open the back valve 17 jet backward, close all the other valves simultaneously, can make air can with solar power composite aircraft level before fly; Control controller 15 No. one; Following valve 19, the following valve 18 downward jet air that make in back can be in required height with the solar power composite aircraft before opening; It is jet to open the right back valve of left front valve 22, No. one 23, closes all the other valves simultaneously, and air can be bent to right with the solar power composite aircraft; Control controller 15 No. one; Following valve 19, the following valve 18 downward jet air that make in back can be in required height with the solar power composite aircraft before opening; It is jet to open the left back valve of right front valve 21, No. one 24, closes all the other valves simultaneously, and air can be turned left with the solar power composite aircraft; When turnon left, right-hand corner,, can make the aircraft pivot stud if regulate the jet amount of right front valve 21, left back valve 24 or left front valve 22, a right back valve 23; Current degree at full speed reaches in the time of making lift that aircraft produces with its gravitational equilibrium, valve 18 under valve 19, the back down before closing; Control controller 15 No. one, down valve 18 is jet downwards down valve 19, back before opening, and the jet amount of valve 19 is greater than back valve 18 down down before making, and it is jet backward to open back valve 17, closes all the other valves simultaneously, and air can be climbed with the solar power composite aircraft; Control controller 15 No. one, down valve 18 is jet downwards down valve 19, back before opening, and the jet amount of valve 19 is less than back valve 18 down down before making, and it is jet backward to open back valve 17, closes all the other valves simultaneously, and air can be dived with the solar power composite aircraft; Control controller 15 No. one, down valve 18 is jet downwards down valve 19, back before opening, and it is jet to open the right back valve of right front valve 21, No. one 23, closes all the other valves simultaneously, can make air can with solar power composite aircraft horizontal left; Control controller 15 No. one, down valve 18 is jet downwards down valve 19, back before opening, and it is jet to open the left back valve of left front valve 22, No. one 24, closes all the other valves simultaneously, and air can be moved to right with solar power composite aircraft level; Control controller 15 No. one, following valve 19, back descend valve 18 jet downwards before opening, and valve 20 before opening No., close all the other valves simultaneously, and air can be retreated with solar power composite aircraft level; Control controller 15 No. one, down valve 18 is jet downwards down valve 19, back before opening, and controls jet amount, closes all the other valves simultaneously, can make air can with the solar power composite aircraft at the uniform velocity or quicken (leaning on gravity) vertical landing.Control controller 15 No. one, the jet amount of control related valves can make air can obtain the flying speed of various flights with the solar power composite aircraft.

This air can be suitable for carrying out the higher task of flying speed with the solar power composite aircraft.

Embodiment 2:

Show like Fig. 8, Fig. 9.Making one has the spherical seal casinghousing 25 of a depression, and spherical seal casinghousing 25 protrudes several supporting legs 30 towards ground side, and the inner chamber of supporting leg 30 is communicated with the cavity of spherical seal casinghousing 25, on spherical seal casinghousing 25, has pressurized air to advance mouth 28 No. two; Curved cover plate 38 covers the depression of spherical seal casinghousing 25; And curved cover plate 38 lids connect with spherical seal casinghousing 25; Curved cover plate 38 is formed 37, No. two cabins, No. two cabins 37 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.), lade or equipment usefulness; The right back valve of the left back valve of valve 42, No. two 40, No. two 26, left valve 39, right valve 27 before front side, left rear side, right lateral side, left side, the right side of spherical seal casinghousing 25 are provided with No. two respectively, the outlet of each valve are outside spherical seal casinghousing 25 and be in horizontal direction; Downside at spherical seal casinghousing 25 is provided with following valve 34 No. one, and it exports outside spherical seal casinghousing 25 and is in vertical direction; The import of valve 42 before No. two, left valve 39, right valve 27, a following valve 34 all communicates with the cavity of spherical seal casinghousing 25; The outlet of valve 42, left valve 39, right valve 27 is respectively as horizontal spout, left horizontal spout, right horizontal spout before outside spherical seal casinghousing 25 before No. two; The outlet of a following valve 34 is as the vertical time spout to spherical seal casinghousing 25 outside, they all with spherical seal casinghousing 25 sealed attachment; No. two left back valves 40, No. two right back valves 26 are communicated with the cavity of spherical seal casinghousing 25 with left levelling pipe 41, right levelling pipe 43 respectively; And left levelling pipe 41, right levelling pipe 43 and spherical seal casinghousing 25 sealed attachment, the outlet of No. two left back valves 40, No. two right back valves 26 is respectively as the left back spout of level, the right back spout of level outside spherical seal casinghousing 25; No. two controllers 36, No. two storage batterys 35 are set in No. two cabins 37; No. two BARO sensors 31, No. two temperature sensors 32, No. two humidity sensors 33 penetrate spherical seal casinghousing 25 from No. two cabins 37 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; No. two controllers 36 all are connected with lead with No. two storage batterys 35, No. two BARO sensors 31, No. two temperature sensors 32, No. two humidity sensors 33, said each valve respectively.

Said air can be taken advantage of the direct beam riding of people with the solar power composite aircraft, also can pass through remotely pilotless beam riding, and beam riding and remotely pilotless beam riding are all implemented through controller.Advance mouth 28 injecting compressed airs for No. two from pressurized air.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 36 and monitor, and No. two controllers 36 are controlled each valve according to pressure, temperature, the humidity of gas injection flow is to obtain suitable reaction thrust.Control controller 36 No. two, it is jet downwards to open a following valve 34, closes all the other valves simultaneously, and air can be risen with the solar power composite aircraft is vertical, controls the downward jet amount of following valve 34, and air can be hovered with the solar power composite aircraft; Control controller 36 No. two; Open the following valve 34 downward jet air that make and to be in required height with the solar power composite aircraft; And open No. two left back valves 40 and No. two right back valves 26 jet backward, close all the other valves simultaneously, can make air can with solar power composite aircraft level before fly; Control controller 36 No. two; Open the following valve 34 downward jet air that make and to be in required height with the solar power composite aircraft; And it is jet backward to open No. two left back valves 40, closes all the other valves simultaneously, and air can be bent to right or pivot stud with the solar power composite aircraft; Control controller 36 No. two; Open the following valve 34 downward jet air that make and to be in required height with the solar power composite aircraft; And it is jet backward to open No. two right back valves 26, closes all the other valves simultaneously, and air can be turned left or pivot stud with the solar power composite aircraft; Control controller 36 No. two, open following valve 34 No. one, and open left valve 39, close all the other valves simultaneously, air can be moved to right with solar power composite aircraft level; Control controller 36 No. two, open following valve 34 No. one, and open right valve 27, close all the other valves simultaneously, can make air can with solar power composite aircraft horizontal left; Control controller 36 No. two, open No. two before valve 42, and open following valve 34 No. one, close all the other valves simultaneously, air can be retreated with solar power composite aircraft level; Control controller 36 No. two, it is jet downwards to open a following valve 34, and controls jet amount, closes all the other valves simultaneously, can make air can with the solar power composite aircraft at the uniform velocity or quicken (leaning on gravity) vertical landing.Control controller 36 No. two, the jet amount of control related valves can make air can obtain the flying speed of various flights with the solar power composite aircraft.

This air can be suitable for carrying out the less demanding task of flying speed with the solar power composite aircraft.

Embodiment 3:

Show like Figure 10 to Figure 14.Make No. two seal casinghousings 44 of a triangle (seeing) from Figure 11; The inner chamber of No. two vertical tails 47 is communicated with the cavity of leg-of-mutton seal casinghousing 44; No. two seal casinghousing 44 protrudes several supporting legs 45 towards ground side; The inner chamber of supporting leg 45 is communicated with the cavity of No. two seal casinghousings 44, on No. two seal casinghousings 44, has pressurized air to advance mouth 46 No. three; Cover plate 48 connects with the upper forepart of No. two seal casinghousings 44 forms No. three cabin 48-1, and No. three cabin 48-1 make to drive chamber, the equipment that installs instruments (like electron camera, navigating instrument etc.), lade or equipment and use; This aircraft casing to No. two seal casinghousings 44 and No. three cabin 48-1 compositions is wing shapes along any section that is parallel to G-G (seeing from Figure 11) sectional plane; The right back valve of No. three left back valves 49, No. three 50, No. two following valves 60 are set respectively in rear side both sides, the bottom surface of No. two seal casinghousings 44; The import of said each valve communicates with the cavity of No. two seal casinghousings 44; The outlet of No. three left back valves 49, No. three right back valves 50 is as the horizontal rear jet outside No. two seal casinghousings 44; The following outlet of No. two following valves 60 be arranged on No. two seal casinghousing 44 bottom surfaces and intersect criss-cross dummy pipe 61, rear tube 57, left conduit 59, right conduit 62 and be communicated with; The outlet of dummy pipe 61, rear tube 57, left conduit 59, right conduit 62 is all vertically downward as to the outer vertical time spout of No. two seal casinghousings 44, said each valve and No. two seal casinghousing 44 sealed attachment; Lightweight weighting material 58 is filled and led up the crosswise groove that dummy pipe 61, rear tube 57, left conduit 59, right conduit 62 form on No. two seal casinghousing 44 bottom surfaces; No. three controllers 54, No. three storage batterys 55 are set in No. three cabin 48-1; No. three BARO sensors 51, No. three temperature sensors 52, No. three humidity sensors 53 penetrate No. two seal casinghousings 44 from No. three cabin 48-1 respectively and probe in it, they and No. two seal casinghousing 44 sealed attachment; No. three controllers 54 all are connected with lead with No. three storage batterys 55, No. three BARO sensors 51, No. three temperature sensors 52, No. three humidity sensors 53, said each valve respectively.

Said air can be taken advantage of the direct beam riding of people with the solar power composite aircraft, also can pass through remotely pilotless beam riding, and beam riding and remotely pilotless beam riding all realize through controller.Advance mouth 46 injecting compressed airs for No. three from pressurized air.No. three BARO sensors 51, No. three temperature sensors 52, No. three humidity sensors 53 be pressure, temperature, the humidity of gas in No. two seal casinghousings of perception 44 respectively; And deliver to No. three controllers 54 and monitor, and No. three controllers 54 are controlled each spout according to pressure, temperature, the humidity of gas injection flow is to obtain suitable reaction thrust.Control controller 54 No. three; It is jet downwards through said each catheter nozzle to open No. two following valves 60, closes all the other valves simultaneously, and air can be risen with the solar power composite aircraft is vertical; Through controlling the downward jet amount of following valve 60 controls No. two, air can be hovered with the solar power composite aircraft; Control controller 54 No. three; Through controlling the downward jet amount of following valve 60 controls No. two; Make air be in required height with the solar power composite aircraft, and open No. three left back valves 49 simultaneously, No. three right back valves 50 are jet backward, can make air can with solar power composite aircraft level before fly; Control controller 54 No. three; Through controlling the downward jet amount of following valve 60 controls No. two, make air be in required height with the solar power composite aircraft, open left back valve 49 No. three; Close right back valve 50 No. three, air can be bent to right with the solar power composite aircraft; Control controller 54 No. three; Through controlling the downward jet amount of following valve 60 controls No. two, make air be in required height with the solar power composite aircraft, open right back valve 50 No. three; Close left back valve 49 No. three, air can be turned left with the solar power composite aircraft; When turnon left, right-hand corner,, can make the aircraft pivot stud if regulate the jet amount of No. three left back valves 49, No. three right back valves 50; Current degree at full speed reaches in the time of making lift that aircraft produces and its gravitational equilibrium, closes following valve 60 No. two; Control controller 54 No. three, open the left back valve of No. two following valves 60, No. three 49, No. three right back valves 50, and control jet amount, can make air can with solar power composite aircraft oblique ascension; Control controller 54 No. three, open No. two following valves 60, No. three left back valves 49 are jet backward, close following valve 60 simultaneously No. two, and air can tiltedly will with the solar power composite aircraft; Control controller 54 No. three, open following valve 60 No. two, and control jet amount, close all the other valves simultaneously, can make air can with the solar power composite aircraft at the uniform velocity or quicken (leaning on gravity) vertical landing.Control controller 54 No. three, the jet amount of control related valves can make air can obtain the flying speed of various flights with the solar power composite aircraft.

This air can be prone to control owing to valve is few with the solar power composite 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.

Claims

Air can with the solar power composite 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; On said seal casinghousing, plurality of valves is set, the import of each valve directly or with pipe communicates with the cavity of seal casinghousing, and the outlet of each valve is as the spout outside seal casinghousing; Said spout, the edge that has is vertical towards ground, the along continuous straight runs that has, the spout of along continuous straight runs has left, has to the right, has forward, has backward; The quantity of said valve and layout are confirmed according to the shape or the flicon requirement of seal casinghousing; 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 is connected with lead with storage battery, BARO sensor, temperature sensor, humidity sensor, valve respectively
According to the said air of claim 1 can with the solar power composite aircraft; It is characterized in that: a seal casinghousing (1) of making a fixed wing aircraft shape; The inner chamber of the left front wing (3), the right front wing (9), the left back wing (5), the right back wing (10), a vertical tail (4) all is communicated with the cavity of a seal casinghousing (1); A seal casinghousing (1) is towards ground side protrusion front leg strut (8) and rear support leg (7); The inner chamber of the inner chamber of front leg strut (8), rear support leg (7) all is communicated with the cavity of a seal casinghousing (1), on a seal casinghousing (1), has pressurized air to advance mouth (6) for No. one; Cover plate (11) connects with the upper forepart of a seal casinghousing (1) forms a cabin (2); Valve (20), back valve (17), left front valve (22), right front valve (21), a left back valve (24), a right back valve (23) before front side, rear side, left side, the right side of a seal casinghousing (1) are provided with No. one respectively; Valve (18) under valve (19), the back under before preceding downside, the back downside of a seal casinghousing (1) are provided with respectively; The import of said each valve communicates with the cavity of a seal casinghousing (1); The outlet of valve before No. (20), back valve (17), left front valve (22), right front valve (21), a left back valve (24), a right back valve (23) is as the horizontal spout outside a seal casinghousing (1); Before down valve (19), back down the outlet of valve (18) as spout under vertical to a seal casinghousing (1) outside, said each valve and a seal casinghousing (1) sealed attachment; A controller (15), a storage battery (16) are set in a cabin (2); A BARO sensor (12), a temperature sensor (13), a humidity sensor (14) penetrate a seal casinghousing (1) from a cabin (2) respectively and probe in it, they and a seal casinghousing (1) sealed attachment; A controller (15) all is connected with lead with a storage battery (16), a BARO sensor (12), a temperature sensor (13), a humidity sensor (14), said each valve respectively.
According to the said air of claim 1 can with the solar power composite 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 (30) towards ground side; The inner chamber of supporting leg (30) is communicated with the cavity of spherical seal casinghousing (25), on spherical seal casinghousing (25), has pressurized air to advance mouth (28) for No. two; Curved cover plate (38) covers the depression of spherical seal casinghousing (25), and curved cover plate (38) lid connects depression composition No. two cabins (37) of curved cover plate (38) and spherical seal casinghousing (25) with spherical seal casinghousing (25); Valve (42), No. two left back valves (40), No. two right back valves (26), left valve (39), right valve (27) before front side, left rear side, right lateral side, left side, the right side of spherical seal casinghousing (25) are provided with No. two respectively, the outlet of each valve are outside spherical seal casinghousing (25) and be in horizontal direction; Downside at spherical seal casinghousing (25) is provided with a following valve (34), and it exports outside spherical seal casinghousing (25) and is in vertical direction; The import of valve before No. two (42), left valve (39), right valve (27), a following valve (34) all communicates with the cavity of spherical seal casinghousing (25); The outlet of valve before No. two (42), left valve (39), right valve (27) is respectively as horizontal spout, left horizontal spout, right horizontal spout before outside spherical seal casinghousing (25); The outlet of a following valve (34) is as the vertical time spout to spherical seal casinghousing (25) outside, they all with spherical seal casinghousing (25) sealed attachment; No. two left back valves (40), No. two right back valves (26) use left levelling pipe (41), right levelling pipe (43) to be communicated with the cavity of spherical seal casinghousing (25) respectively; And left levelling pipe (41), right levelling pipe (43) and spherical seal casinghousing (25) sealed attachment, the outlet of No. two left back valves (40), No. two right back valves (26) are respectively as the left back spout of level, the right back spout of level outside spherical seal casinghousing (25); No. two controllers (36), No. two storage batterys (35) are set in No. two cabins (37); No. two BARO sensors (31), No. two temperature sensors (32), No. two humidity sensors (33) penetrate spherical seal casinghousing (25) from No. two cabins (37) 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; No. two controllers (36) all are connected with lead with No. two storage batterys (35), No. two BARO sensors (31), No. two temperature sensors (32), No. two humidity sensors (33), said each valve respectively.
According to the said air of claim 1 can with the solar power composite aircraft; It is characterized in that: make No. two seal casinghousings of a triangle (44); The inner chamber of No. two vertical tails (47) is communicated with the cavity of leg-of-mutton seal casinghousing (44); No. two seal casinghousings (44) protrude several supporting legs (45) towards ground side, and the inner chamber of supporting leg (45) is communicated with the cavity of No. two seal casinghousings (44), on No. two seal casinghousings (44), have pressurized air to advance mouth (46) for No. three; Cover plate (48) connects with the upper forepart of No. two seal casinghousings (44) forms No. three cabins (48-1); This aircraft casing to No. two seal casinghousings (44) and No. three cabins (48-1) are formed is wing shapes along any longitudinally section that is parallel to this housing; In rear side both sides, the bottom surface of No. two seal casinghousings (44) No. three left back valves (49), No. three right back valves (50), No. two following valves (60) are set respectively; The import of said each valve communicates with the cavity of No. two seal casinghousings (44); The outlet of No. three left back valves (49), No. three right back valves (50) is as the horizontal rear jet outside No. two seal casinghousings (44); The following outlet of No. two following valves (60) be arranged on No. two seal casinghousings (44) bottom surface and intersect criss-cross dummy pipe (61), rear tube (57), left conduit (59), right conduit (62) and be communicated with; The outlet of dummy pipe (61), rear tube (57), left conduit (59), right conduit (62) is all vertically downward as the vertical spout down outside No. two seal casinghousings (44), said each valve and No. two seal casinghousings (44) sealed attachment; Lightweight weighting material (58) is filled and led up the crosswise groove that dummy pipe (61), rear tube (57), left conduit (59), right conduit (62) form on No. two seal casinghousings (44) bottom surface; No. three controllers (54), No. three storage batterys (55) are set in No. three cabins (48)-1; No. three BARO sensors (51), No. three temperature sensors (52), No. three humidity sensors (53) penetrate No. two seal casinghousings (44) from No. three cabins (48-1) respectively and probe in it, they and No. two seal casinghousings (44) sealed attachment; No. three controllers (54) all are connected with lead with No. three storage batterys (55), No. three BARO sensors (51), No. three temperature sensors (52), No. three humidity sensors (53), said each valve respectively.