CN202783761U

CN202783761U - Air energy flyball

Info

Publication number: CN202783761U
Application number: CN 201220480168
Authority: CN
Inventors: 刘新广
Original assignee: Individual
Current assignee: Individual
Priority date: 2012-09-20
Filing date: 2012-09-20
Publication date: 2013-03-13
Anticipated expiration: 2022-09-20

Abstract

The utility model discloses an air energy flyball. A sealed shell is provided with a compressed air inlet and support legs; a cabin is attached on the sealed shell; a left valve, a right valve and an upper valve are arranged on the sealed shell; each valve is connected and communicated with the sealed shell; outlets of the left valve and the right valve face backwards along the horizontal direction, a basin-shaped rotor wing I which can rotate around the upper valve is sleeved on the upper valve; a basin edge is formed in a way that two concentric annuluses clamp a plurality of tile-shaped vanes of which the concave surfaces are slant along the same rotation direction; a hollow shaft sleeve is linked with the upper valve; a rotor ring II which can rotate around the shaft sleeve is linked on the shaft sleeve; air paths are formed in vanes of the rotor wing II; the air paths face an annular groove of the shaft sleeve; a vent hole at the side of each vane is downwards aslant to the concave surfaces of the tile-shaped vanes; a controller and a storage battery are arranged in the cabin; and the controller is connected with the storage battery, an air pressure sensor, a temperature sensor, the upper valve, the left valve and the right valve through leads. Compressed air in the flyball drives the rotor ring II and the basin-shaped rotor wing I to rotate to produce lifting force so as to drive the left valve and the right valve to produce propulsive force or to steer.

Description

Air can flyball

Technical field

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

Background technology

Existing aircraft is take heat engine (turbine engine, turboaxle motor, piston engine) or electric device as engine, and heat engine is take fuel as the energy, and electric device is take the electric energy of battery as the energy.Because the Flight Vehicle Structure take heat engine or electric device as engine is 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 large.

Summary of the invention

In order to overcome the defects of existing aircraft, the utility model designs a kind of air can flyball, take pressurized air and solar power as power, this aircraft control is simple, flight flexibly, load ratio is large, energy consumption is little, safe, reliable, environmentally friendly.

The utility model is achieved through the following technical solutions.

Show such as Fig. 1, Fig. 2.Make a spherical sealed housing 8 with a depression, spherical sealed housing 8 protrudes several supporting legs 11 towards ground side, and the cavity UNICOM of the inner chamber of supporting leg 11 and spherical sealed housing 8 has pressurized air to advance mouth 17 at spherical sealed housing 8; Curved cover plate 9 covers the depression of spherical sealed housing 8, and curved cover plate 9 lid connects with spherical sealed housing 8, the depression composition cabin 10 of curved cover plate 9 and spherical sealed housing 8, cabin 10 equipment (such as electron camera, navigating instrument etc.) that installs instruments; 10 interior controller 12, the storage batterys 13 of arranging in the cabin, baroceptor 14, temperature sensor 15, humidity sensor 16 10 penetrate spherical sealed housing 8 and probe in it from the cabin respectively, baroceptor 14, temperature sensor 15, humidity sensor 16 all with spherical sealed housing 8 sealed attachment; The structure that flies actuator before the described air energy flyball is: left rear side, right lateral side at spherical sealed housing 8 arrange respectively left valve 7, right valve 18, the outlet of left valve 7, right valve 18 is outside spherical sealed housing 8 and be in horizontal direction, left valve 7, right valve 18 connect with the UNICOM of spherical sealed housing 8 with left levelling pipe 24, right levelling pipe 25 respectively, and the outlet of left valve 7, right valve 18 is respectively as the left back spout of level, the right back spout of level outside spherical sealed housing 8.The end opening of upper valve 19 connect with spherical sealed housing 8 and with its cavity UNICOM, the spool 19-1 of upper valve 19 connects with actuator 6; Show that such as Fig. 1, Fig. 3, Fig. 4 No. one rotor 5 has several winged petioles, the cross sectional shape of winged petiole is like stream line pattern, and the mesopore that connects 4, numbers rotors 5 of a coupling block in the termination of each winged petiole is enclosed within the top cylindrical of valve 19 and is made into normal-running fit with it; Axle sleeve 20 is socketed in the upper end of valve 19, and the lower end of axle sleeve 20 had both been limited on a rotor 5 and moved, and a rotor 5 is rotated freely, the top annular groove UNICOM of the mesopore of axle sleeve 20 and axle sleeve 20, the mesopore of axle sleeve 20 also with upper valve 19 UNICOMs.Show such as Fig. 1 Fig. 3, an annulus 22 and No. two annulus 23 concentrics be enclosed within outside the axle sleeve 20 lower end of an annulus 22 and No. two annulus 23 and the upper client link of coupling block 4; Evenly connect some watts of shape blades 3 along the circle spacing between an annulus 22 and No. two annulus 23, the concave surface of all watts shape blade 3 is along same inclination one angle that turns to.Show that such as Fig. 1, Fig. 5, Fig. 6 the mesopore of No. two rotors 2 is enclosed within axle sleeve 20 top cylindricals and is made into normal-running fit with it; No. two rotor 2 has several winged petioles, and air flue is all arranged in each winged petiole, and air flue is facing to the annular groove of axle sleeve 20, each winged petiole only has a side that air gate 1 is arranged, air gate 1 declivity aims at watt concave surface of shape blade 3, makes the air flow energy shooting at watt concave surface of shape blade 3, the air flue UNICOM of pore 1 and winged petiole.Show that such as Fig. 1 back-up ring 21 connects with the upper end of axle sleeve 20, back-up ring 21 had both limited on No. two rotors 2 and had moved, and No. two rotors 2 are rotated freely.Controller 12 is connected with storage battery 13, baroceptor 14, temperature sensor 15, humidity sensor 16, upper valve 19, left valve 7, right valve 18 usefulness wires respectively.

Advance mouth 17 injecting compressed airs from pressurized air.Baroceptor 14, temperature sensor 15, humidity sensor 16 be pressure, temperature, the humidity of perception spherical sealed housing 8 interior gas respectively, and deliver to controller 12 and monitor.Control controller 12, and controller 12 is according to compressed-air actuated pressure, temperature, humidity and control instruction and control each valve opening.Control actuator 6 turns spool 19-1 and opens valve 19, and pressurized air is from fumarole 1 ejection of No. two rotors 2, thereby the moment of reaction causes No. two rotor 2 rotations to produce lift.The high pressure air of ejection impacts watt shape blade 3 makes rotor 5 produce lift with the direction rotation opposite with No. two rotor 2 hand of rotation, and the air-flow that impacts behind watt shape blade 3 also can make a rotor 5 increase lift from lower spray between annulus 22 and No. two annulus 23.A rotor 5 is with opposite with No. two rotor 2 hand of rotation, by designing a rotor 5, No. two rotors 2 with the different angles of attack, can solve lift that forward direction (to ball working direction rotation) winged petiole produces greater than backward winged petiole and cause the problem that air can flyball rolls.If close left valve 7, right valve 18, air can vertically be risen by flyball, by controlling the aperture of upper valve 19, air can be hovered by flyball.Control controller 12, left valve 7, right valve 18 are jet backward, and air can be flown before the flyball level, control the aperture of left valve 7, right valve 18, can make air can flyball turn to (if the right valve of left valve 7 opening ratios 18 is large, right-hand turning then, otherwise also anti-).Control controller 12 No. two, the aperture of valve 19 in the control is closed its left valve 7, right valve 18 simultaneously, can make air energy flyball at the uniform velocity or accelerate (by gravity) vertical landing.Control the aperture of each valve, can make air energy flyball obtain the flying speed of various flights.

Air can flyball be suitable for carrying out scout, monitoring, inspection, search and rescue, etc. the less demanding task of flying speed.

The effect that the utility model is useful:

1, air energy flyball is simple in structure, and cost is very little.

2, the quality of the seal casinghousing of air energy flyball, can accomplish that (using composite material) is less than casing and the alighting gear quality of existing aircraft, but air can flyball all valves, rotor total mass little more than the total mass of the driving engine of existing aircraft and transmission device, it is much smaller that the compressed air quality that it carries carries fuel mass than existing aircraft, the proportion of air energy flyball 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 flyball run up time, and this is to carrying out an urgent task very to power, and existing aircraft can't be reached.

When 4, can flyball annotating pressurized air for air, the room temperature environment of being everlasting, after finishing, if air can flyball 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 flyball in passing.This is its another outstanding advantages.

5, operation control is simple, and flight flexibly.

6, structure and the principle of work of air energy flyball have determined that it is longer than existing aircraft reliable operation, life-span.

7, pressurized air consumed or et out of order (except the fracture of ball fractured or rotor) situation under, air can descend by flyball, up current drives the lift that the rotor free rotation produces, and plays the effect of parachute, so the incomparable safety of air energy flyball.

8, owing to above-mentioned advantage, so described air energy flyball cost performance is high.

Description of drawings

Fig. 1 is the structural representation of air energy flyball;

Fig. 2 is the A-A cutaway view of Fig. 1;

Fig. 3 is the birds-eye view of watt shape blade 3 among Fig. 1, rotor 5, coupling block 4, an annulus 22, No. two annulus 23;

Fig. 4 is the B-B section-drawing of a rotor 5 among Fig. 3;

Fig. 5 is the birds-eye view of No. two rotors 2 among Fig. 1;

Fig. 6 is the C-C section-drawing of Fig. 5.

The specific embodiment

Claims

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

Make a spherical sealed housing (8) with a depression, spherical sealed housing (8) protrudes several supporting legs (11) towards ground side, the cavity UNICOM of the inner chamber of supporting leg (11) and spherical sealed housing (8) has pressurized air to advance mouth (17) at spherical sealed housing (8); Curved cover plate (9) covers the depression of spherical sealed housing (8), curved cover plate (9) lid connects with spherical sealed housing (8), the depression of curved cover plate (9) and spherical sealed housing (8) forms cabin (10), cabin (10) equipment that installs instruments; Controller (12), storage battery (13) are set in cabin (10), (10) penetrate spherical sealed housing (8) and probe in it from the cabin respectively for baroceptor (14), temperature sensor (15), humidity sensor (16), baroceptor (14), temperature sensor (15), humidity sensor (16) all with spherical sealed housing (8) sealed attachment; The structure that flies actuator before the described air energy flyball is: the left rear side in spherical sealed housing (8), right lateral side arranges respectively left valve (7), right valve (18), left valve (7), the outlet of right valve (18) is outside spherical sealed housing (8) and be in horizontal direction, left valve (7), right valve (18) is used respectively left levelling pipe (24), right levelling pipe (25) connects with the UNICOM of spherical sealed housing (8), left valve (7), the outlet of right valve (18) is respectively as the left back spout of level outside spherical sealed housing (8), the right back spout of level; The end opening of upper valve (19) connect with spherical sealed housing (8) and with its cavity UNICOM, the spool (19-1) of upper valve (19) connects with actuator (6); A rotor (5) has several winged petioles, and the cross sectional shape of winged petiole connects a coupling block (4) in the termination of each winged petiole like stream line pattern, and the mesopore of a rotor (5) is enclosed within the top cylindrical of valve (19) and is made into normal-running fit with it; Axle sleeve (20) is socketed in the upper end of valve (19), the lower end of axle sleeve (20) had both been limited on the rotor (5) and had been moved, a rotor (5) is rotated freely, the top annular groove UNICOM of the mesopore of axle sleeve (20) and axle sleeve (20), the mesopore of axle sleeve (20) also with upper valve (19) UNICOM; Being enclosed within outside the axle sleeve (20) of an annulus (22) and No. two annulus (23) concentric, the lower end of an annulus (22) and No. two annulus (23) and the upper client link of coupling block (4); Evenly connect some watts of shape blades (3) along the circle spacing between an annulus (22) and No. two annulus (23), the concave surface of all watts shape blade (3) is along same inclination one angle that turns to; The mesopore of No. two rotors (2) is enclosed within axle sleeve (20) top cylindrical and is made into normal-running fit with it; No. two rotors (2) have several winged petioles, air flue is all arranged in each winged petiole, air flue is facing to the annular groove of axle sleeve (20), each winged petiole only has a side that air gate (1) is arranged, air gate (1) declivity aims at watt concave surface of shape blade (3), make the air flow energy shooting at watt concave surface of shape blade (3), the air flue UNICOM of pore (1) and winged petiole; Back-up ring (21) connects with the upper end of axle sleeve (20), and back-up ring (21) had both limited on No. two rotors (2) and moved, and No. two rotors (2) are rotated freely; Controller (12) is connected with wire with storage battery (13), baroceptor (14), temperature sensor (15), humidity sensor (16), upper valve (19), left valve 7, right valve (18) respectively.