CN110920882A

CN110920882A - Water-air dual-purpose helicopter

Info

Publication number: CN110920882A
Application number: CN201910382199.1A
Authority: CN
Inventors: 王三保
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-05-05
Filing date: 2019-05-05
Publication date: 2020-03-27

Abstract

A water-air dual-purpose helicopter features that the push frames are arranged at bottom and back of helicopter, the upper push frame has the functions of lifting and floating, the lower push frame has the forward flying function, multiple small folding doors are arranged on push frame, the push frame is driven by power to push forward, the small folding doors close together, so preventing air from being affected by resistance and load, the push frame pushes back the multiple small folding doors to open, so generating huge collision force to push the helicopter forward.

Description

Water-air dual-purpose helicopter

Field of the invention

The invention relates to a helicopter for water and air use in the aviation field, wherein a pure-motor-driven aircraft type is added in the aviation field, and the pure-motor-driven aircraft type is different from the existing aircraft type, changes the difference in principle structure and function, and particularly improves the small oil consumption and the large function.

Background

The existing aircrafts in the whole world are of vortex jet type, and all the aircrafts in the whole world are of high-power engines, burn a large amount of oil to attract gas and explode to jet a large amount of gas to impact and collide with air to form resistance, so that the aircraft body is pushed backwards to move forwards, the air in the air is very empty, the air is a very thin contact body, no large explosion amount exists, the air pressure cannot become the strong propelling force of the aircrafts, and the oil consumption is remarkable.

Disclosure of Invention

In order to provide more excellent functions for the airplane, the invention provides a scheme of a water-air dual-purpose helicopter, the dual-purpose helicopter can save half of oil consumption compared with the existing airplane, but the dual-purpose helicopter can not be applied to a supersonic airplane and is suitable for short distance. Low degree, low speed, civil use, tour and sightseeing, short-distance transportation and emergency.

The invention solves the technical problem, and adopts the following scheme: the push frame is pushed by a push rod under the power of a power machine, the push frame pushes the multiple small folding doors forwards, the small folding doors are pushed forwards by the push frame, the air is not closed to form resistance, the push frame pushes the multiple small folding doors backwards, the planes of the multiple small folding doors are completely opened and are attached to the push frame to form a broad area push plate, air stamping and quick power, the two push plates have huge contact force to push the airplane body forwards, the power machine output power has an actual effect, the power airplane saves a large amount of oil, the push plate is contracted and connected with a power machine base, the power machine is arranged in a cabin, the two push rods extend out to be connected with the push frame, the push rod movable ring 3 and the shaft lever 4 are connected, the power machine base in the push-pull cabin of the hydraulic machine is linked to contract and push the push frame, the frame is connected with the bottom, the structure principle of the upper double push frame is the same, the function is the same, the multi-leaf small folding door on the water sailing push plate is opened and closed to form a large-scale palm, the water has no resistance, the multi-leaf small folding door on the backward pushing frame is fully opened to form huge pushing force, the machine body can move forwards quickly and can be lifted in water green, other structural systems can be matched with the high-depth technology of the existing airplane, the fine parts of the system are small in oil consumption, the expense is low, the airplane can be used between rural areas, towns, counties and villages to replace the use of the automobile in life, the demand of people who change in society in the era is met, the product which can be developed by the country is a good product, and when the large airplane uses the structure.

Drawings

The invention is further illustrated with reference to the following figures and examples.

Fig. 1 is a longitudinal sectional view of an embodiment of a helicopter for air and water use.

Fig. 2 is a schematic diagram of the combined structure of the helicopter for both air and water use of the invention.

Fig. 3 is a longitudinal sectional configuration view of an embodiment of the helicopter.

In the figure, 1, a push frame, 2, a lever beam, 3, a push rod loose ring, 4, a shaft lever, 5, a support loose ring, 6, a support, 7, a small folding door, 8, a long ring chain, 9, a straight lever, 10, a small folding door opening sample, 11, a door closing collision block, 12, a transverse lever, 13, a power push rod, 14, a push rod, 15 in the figure, a plane, 16, a push frame, 17, a shaft lever, 18, a shaft seat, 19, a small folding door, 20, a long ring chain, 21, a straight lever, 22, a door opening sample, 23, a transverse lever, 24, a push rod loose ring, 25, a push rod, 26, an eccentric fulcrum, 27, a push wheel, 28, a central shaft, 29, a motor, 30, a gear, 31, a gear, 32, a contraction frame, 33, a shaft seat and 34, a bottom beam.

Detailed Description

In figure 1, push frame 1 is arranged at the front and back of the bottom of the airplane respectively, a bar beam 2 is connected and installed at the bottom of the airplane, 4 a shaft lever is connected with a push rod loose ring 3, a bracket loose ring 5 and a bracket 6 are connected at the bottom of the airplane, a small folding door 7 is provided with a long strip ring chain 8, a plurality of small folding doors 7 are quickly opened and closed flexibly and firmly in flight, a straight lever 9, the push frame 1 and the plurality of small folding doors 10 are pushed forwards and closed without negative influence due to air resistance, the push frame 1 pushes the plurality of small folding doors 10 backwards and simultaneously opens the plane and is attached to the frame, a large navigation palm thrust with large area is formed, the navigation speed is extremely high, a door closing block 11, a transverse lever 12, a power push frame 13, a power push frame ring 14, (2 is combined with the airplane 15) is formed, the bar beam 2 is connected and installed with the push frame 16, a power lever on the push frame 16 is arranged on the shaft lever 17, a rotary shaft lever 18 is installed and flexibly and rotates in the shaft seat 18, a push rod 27 of a push rod eccentric wheel, the upper plane is attached on the frame 16, the long-strip ring chain 20, the push rod 25 of the eccentric wheel 27 is pushed up and down quickly and the push plate with wide area impacts air quickly to form huge force, two sides of the push rod are pushed to form double flying wings, the multi-leaf small folding door 10 swings up and down along with suspension flying, the lower double push rack flies forward, the upper double wings can lift, the straight lever 21, the door opening sample 22, the cross lever 23, the push rod loose ring 24, the push rod 25, the eccentric wheel loose pivot 26, the eccentric wheel 27, the central shaft 28, the motor 29, the power is received by the motor 29, the motor gear 30 drives the gear 31 to link the central shaft 28, the eccentric wheel 27 eccentric pivot 26 rotates the push rod 25, the push rod loose ring 24 is connected with the push rack 16 to rotate in a connecting ring, the bottom beam 34 of the push rack 32 shaft seat 33 is contracted, the two push racks are contracted by adopting a hydraulic press to push and pull the motor and the push rack, the safety factors, the water-air dual-purpose helicopter also has the characteristic of safety.

Claims

1. A water and air dual-purpose helicopter comprises a push frame, a push beam, a push ring, a shaft rod, a support ring, a support, a small folding door, a long-strip ring chain, a straight lever, a small folding door, a door closing block, a transverse lever, a power push rod, a push rod ring, a combined airplane, a push frame, a shaft rod, a shaft seat, a small push door, a long-strip ring chain, a straight lever, a door opening sample, a transverse rod, a push rod ring, a push rod, a push frame, a shaft seat, a motor, a gear 31, a contraction frame, a shaft seat, a motor, a bottom beam, a push rod ring, a power push rod, a push rod ring, a push rod.

2. The helicopter of claim 1, wherein said helicopter further comprises: the water-air dual-purpose helicopter (15) has different principles compared with the existing helicopter, and has different structures to push the frame (1) to push the helicopter to fly, so that the helicopter saves oil and is purely mechanically driven to fly.

3. The helicopter of claim 1, wherein said helicopter further comprises: the airplane is characterized in that a pushing frame (1) is arranged at the bottom of an airplane (15) and consists of a plurality of small folding doors (10) at the front and the back, the pushing frame (1) pushes the plurality of small folding doors (10) forwards to be completely closed without resistance to air, the pushing frame (1) pushes backwards, the plurality of small folding doors (10) on the pushing frame (10) are completely opened to form a large-area pushing plate, the two pushing plates are subjected to air resistance by fast rotation and air impact, and the machine body (12) is pushed forwards by applying huge air blocking rebound to the transmission rod force generated by the pushing frame (10).

4. The helicopter of claim 1, wherein said helicopter further comprises: a left pushing frame and a right pushing frame (1) are respectively arranged on the back of an airplane (15) and are pushed up by an eccentric wheel (27) to push a plurality of small folding doors (10) to be opened completely, so that a wide-area push plate is formed to rotate quickly, air impacts the two push plates to bear air resistance, a transmission rod force generated by the pushing frames (1) and air resistance are added to prevent a huge-force rebounding machine body (15) from flying upwards and directly, and the lifting effect is achieved.

5. The helicopter of claim 1, wherein said helicopter further comprises: the water-air dual-purpose helicopter (15) sails in water, the plurality of small folding doors fold the water forwards without resistance, and the large thrust which is pushed backwards to form a large ship palm with the rapid power and the plurality of small folding doors sails in water rapidly and takes off and lands on water.