CN2320533Y

CN2320533Y - Knapsack aircraft

Info

Publication number: CN2320533Y
Application number: CN 97243759
Authority: CN
Inventors: 黄永吉
Original assignee: Individual
Current assignee: Individual
Priority date: 1997-10-30
Filing date: 1997-10-30
Publication date: 1999-05-26
Anticipated expiration: 2007-10-30

Abstract

The utility model relates to an aircraft used for making one human body fly in the sky, particularly the reasonable use and combination of the prior art and devices. The utility model is composed of rotary wings, engines, knapsack fixing devices, direction controlling devices, lift controlling devices, oil tanks, power supply, etc., wherein, support fixing devices are composed of the knapsack fixing devices, which are used for flying the human body in the sky; power and controlling devices of the aircraft are composed of two engines fixed on fixing plates, the oil tanks, accumulators, the direction controlling devices, and the lift controlling devices. Additionally, the back surfaces of support plates are fixedly provided with a hydraulic pressure supporting and pushing device which can make the fixing plates rotate around pivot shafts. The utility model steps the first step in research and practice in the field.

Description

A kind of backpack aircraft

The utility model is the aircraft that a kind of people's of being used for monomer aloft flies, and it relates to prior art and device are reasonably utilized and made up, to realize the purpose of people's monomer flight.

Since the mankind had been arranged, people were just dreaming of to hover on high as small bird always.Along with progress of science and technology, the mankind have invented various aircraft, and multi-form aircraft, helicopter constantly occur.But, in numerous aircraft of mankind invention, also do not have a kind ofly to use for a people, do not need too big place, but vertical takeoff and landing and flying in the aircraft of sky.Along with the process in epoch, this flight instruments is to occur.

In order to realize human dream, making full use of on the basis of prior art, the utility model proposes a kind of flight instruments of the people's of being applicable to monomer flight, in the research in this field and practice, stepped the first step.

On the basis of a large amount of research and experiments, the structure design of the utility model device--a kind of backpack aircraft has been seen blank, and it reaches measure by the following method and realizes:

This kind backpack aircraft is by rotor and driving engine, bears anchor fitting, directional controller, assemblies such as apparatus for controlling of lifting, fuel tank and power supply are formed, wherein, directional controller and apparatus for controlling of lifting all adopt the version of electromagnetism hand of rotation rudder, its technical scheme is open in Chinese patent 97250877.5, and architectural feature of the present utility model is:

1.. bear anchor fitting and support ejection device, hook plate, handrail and band and form by adapter plate, the negative plate of holder, pivot, hydraulic pressure, wherein, the top of the negative plate both sides of holder is equipped with hooked hook plate, the bottom is equipped with handrail, there is band to be connected between hook plate and the handrail, the negative anchor fitting of holder when having constituted human body flight thus;

2.. adapter plate is by being pivotally mounted in the top of the negative plate of holder, fixedly install the driving engine of two band rotors on the adapter plate side by side, on the adapter plate between two driving engines, be installed with fuel tank and storage battery, outside two engine center portions, cut up with a hay cutter top and be set with direction controller and yaw rudder sheet, be set with lifting controller and elevating rudder sheet in its underpart, in addition, handrail is provided with the control keypad, has constituted the power and the control setup of aircraft thus;

3.. at the back side of the negative plate of holder, fixedly install a hydraulic pressure and support ejection device, its other end is connected with the back side of adapter plate, and this device can make adapter plate along pivoted.

In addition, standby pack is arranged on the band so that use.

The drawing of accompanying drawing is described as follows:

Fig. 1,2,3,4 is the structural representation of the utility model different visual angles

Fig. 5 is a structural representation of bearing anchor fitting of the present utility model

Fig. 6 is the structural representation of electromagnetism hand of rotation rudder

Below with reference to drawings and Examples the utility model is further described:

Shown in accompanying drawing 1-6, this kind backpack aircraft, it is by rotor 1 and driving engine 2, bear anchor fitting, directional controller 6, apparatus for controlling of lifting 8, assemblies such as fuel tank 10 and power supply 11 are formed, wherein, directional controller and apparatus for controlling of lifting all adopt the version of electromagnetism hand of rotation rudder, its technical scheme is disclosed in Chinese patent 97250877.5, the architectural feature of electromagnetism hand of rotation rudder is, remove and comprise power supply, lead, outside the master cock, its architectural feature is mainly reflected on the rudder sheet slewing arrangement, rudder sheet slewing arrangement comprises rudder sheet 18, Insulating frame 19 and two semi-round insulcretes 20, the rudder sheet is installed in the crossbeam midway location of Insulating frame by adapter shaft steel pipe 21, and can the adapter shaft steel pipe be that axle rotates to realize direction control.The other end of rudder sheet respectively has a magnetic pole 22 up and down, connect one between two magnetic poles and rotate column 23, winding around is arranged on it, in addition, also respectively be provided with the left and right magnetic pole 24 of a band winding around in the left and right sides of Insulating frame, 25, two semicircle insulcretes 20 are installed in the two ends up and down of Insulating frame 19.During energising work, because the pole orientation of left and right magnetic pole 24,25 is opposite with the pole orientation of rotating column 23, the hand of rotation of may command rudder sheet.And architectural feature of the present utility model is:

1.. bear anchor fitting and support ejection device 15, hook plate 16, handrail 17 and band 3 and form by adapter plate 12, the negative plate 13 of holder, pivot 14, hydraulic pressure, wherein, the top of negative plate 13 both sides of holder is equipped with hooked hook plate 16, the bottom is equipped with handrail 17, there is band 3 to be connected between hook plate 16 and the handrail 17, standby pack 5 is arranged on the band 3 so that use, the negative anchor fitting of holder when having constituted human body flight thus, in addition, handrail 17 is provided with control keypad 4, has constituted the power and the control setup of aircraft thus;

2.. adapter plate 12 is installed in the top of the negative plate 13 of holder by pivot 14, fixedly install the driving engine 2 of two band rotors 1 on the adapter plate 12 side by side, between two driving engines at a distance of 50-60mm, rotor 1 exceeds the top 90-110mm of the negative plate 13 of holder, on the adapter plate between two driving engines 12, be installed with fuel tank 10 and storage battery 11, outside two engine center portions, cut up with a hay cutter top and be set with direction controller 6 and yaw rudder sheet 7, be set with lifting controller 8 and elevating rudder sheet 9 in its underpart;

3.. at the back side of the negative plate 13 of holder, fixedly install a hydraulic pressure and support ejection device 15, its other end is connected with the back side of adapter plate 12, this device can make adapter plate 12 rotate along pivot 14, the angular range that hydraulic pressure supports 12 rotations of ejection device 15 pushing tow adapter plates is the angle of 30-45 degree between the negative plate 13 of itself and holder, and adapter plate is stopped the optional position betwixt.

After the people bore this aircraft, and start the engine vertically goes up to the air, overall weight all hanging was not afraid of the influence of air-flow and sinuous flow under the rotor face.When the rotor face turn forward from vertical lifting surface be transformed into rise thrust face after, the aircraft flight that begins to travel forward, aircraft is when slower flight, the driver can utilize the anteflexion instinct of human body natural, overcome the influence of hypsokinesis torsion, handle the position of center of gravity, can freely control the direction of flight.When the aircraft high-speed flight, can revise heading rapidly and accurately and guarantee the stable of aircraft by control direction controller of the button on the handrail and lifting controller.

The aircraft that the utility model provides a kind of people's of being used for monomer to fly aloft, the development of this aircraft also only is in the starting stage with exploitation at present, the utility model makes full use of existing technology and device, reasonably utilized and made up, for the ideal that realizes the flight of people's monomer has stepped solid step forward.

Claims

1. backpack aircraft, it by rotor (1) and driving engine (2), bear anchor fitting, directional controller (6), apparatus for controlling of lifting (8), fuel tank (10) and power supply assemblies such as (11) and form, wherein, directional controller and apparatus for controlling of lifting all adopt the version of electromagnetism hand of rotation rudder, it is characterized in that:

1.. bear anchor fitting and support ejection device (15), hook plate (16), handrail (17) and band (3) and form by adapter plate (12), the negative plate (13) of holder, pivot (14), hydraulic pressure, wherein, the top of negative plate (13) both sides of holder is equipped with hooked hook plate (16), the bottom is equipped with handrail (17), there is band (3) to be connected between hook plate (16) and the handrail (17), the negative anchor fitting of holder when having constituted human body flight thus;

2.. adapter plate (12) is installed in the top of the negative plate (13) of holder by pivot (14), fixedly install the driving engine (2) of two band rotors on the adapter plate (12) side by side, on the adapter plate between two driving engines (12), be installed with fuel tank (10) and storage battery (11), outside two engine center portions, cut up with a hay cutter top and be set with direction controller (6) and yaw rudder sheet (7), be set with lifting controller (8) and elevating rudder sheet (9) in its underpart, in addition, handrail (17) is provided with control keypad (4), has constituted the power and the control setup of aircraft thus;

3.. at the back side of the negative plate (13) of holder, fixedly install a hydraulic pressure and support ejection device (15), its other end is connected with the back side of adapter plate (12), and this device can make adapter plate (12) rotate along pivot (14).

2. backpack aircraft according to claim 1 is characterized in that: standby pack (5) is arranged on band (3) and goes up so that use.

3. backpack aircraft according to claim 1 is characterized in that: at a distance of 50-60mm, rotor (1) exceeds the top 90-110mm of the negative plate (13) of holder between the driving engine (2) of two band rotors.

4. backpack aircraft according to claim 1 is characterized in that: the angular range that hydraulic pressure supports ejection device (15) pushing tow adapter plate (12) rotation is the angle of 30-45 degree between the negative plate (13) of itself and holder.