CN212220551U

CN212220551U - Flying saucer aircraft

Info

Publication number: CN212220551U
Application number: CN202020643992.0U
Authority: CN
Inventors: 耿起志
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-04-26
Filing date: 2020-04-26
Publication date: 2020-12-25
Anticipated expiration: 2030-04-26

Abstract

The utility model discloses a flying saucer aircraft, including the dish body, flight oar, landing support, egg-shaped dish body middle part circumference is equipped with the electromagnetism track, the electromagnetism track is the "concave" style of calligraphy track that the middle part is inwards sunken, be provided with rather than complex electromagnetism suspension car in the electromagnetism track, the flight oar is connected in electromagnetism suspension car outer surface to can rotate around egg-shaped dish body along the electromagnetism track under the drive of electromagnetism suspension car, egg-shaped dish body both sides and lie in the position of flight oar lower part and still be equipped with turbine jet engine support, the last rotatable turbine jet engine that is connected with of turbine jet engine support, landing support sets up in egg-shaped dish body bottom, the landing support is folding support, and this application aircraft can be as a new aircraft, carries out activities such as transportation, travel, exploration; the aircraft can take off and land vertically without a special runway, and can fly in the air and simultaneously change the direction conveniently through the turbojet.

Description

Flying saucer aircraft

Technical Field

The utility model relates to an aircraft technical field specifically indicates a flying saucer aircraft.

Background

The existing aircrafts mainly comprise airplanes, gliders, helicopters and hot air balloons, and for disc aircrafts, the existing aircrafts are mainly embodied in movies and pictures, and the aircrafts have many limitations in flying, such as: the special runway is needed, and on the other hand, the existing aircraft is not in a central symmetrical structure, and has the defects of severe interference and inflexible steering when encountering abnormal airflow during air flight. Therefore, it is necessary to create a new aircraft mainly based on dish shape, and the variety of the aircraft can be increased.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problem, the utility model provides a technical scheme does: the utility model provides a flying saucer aircraft, includes the dish body, flight oar, landing support, dish body middle part circumference is equipped with the electromagnetism track, the electromagnetism track is the inside sunken "concave" style of calligraphy track in middle part, be provided with rather than the complex electromagnetism car that suspends in the electromagnetism track, the flight oar is connected in electromagnetism suspension car outer surface to can rotate around the dish body along the electromagnetism track under the drive of electromagnetism suspension car, dish body both sides still are equipped with the turbojet support on being located the position of flight oar lower part, be connected with the turbojet on the turbojet support, the turbojet of dish body one side is vertical setting, and the opposite side is horizontal setting, the landing support sets up in dish body bottom, the landing support is folding support.

As an improvement, the flight oar outside is equipped with the flight oar safety cover, the flight oar safety cover is including setting up in the flight oar outside and rather than the annular protective cradle that is in same horizontal plane, both ends extend the last dictyosome, the lower dictyosome that can cover the flight oar that set up respectively to the dish body direction about the annular protective cradle, go up the dictyosome, the end of lower dictyosome all is connected with the dish body.

As the improvement, the flight oar is including setting up in the outside annular flight oar support of electromagnetism suspension car, the outside circumference of annular flight oar support is equipped with the several paddle.

As an improvement, the paddle is an inclined paddle with an included angle with the horizontal plane.

As an improvement, the dish body is including the central cabin body that is equipped with the electromagnetism track, central cabin body upper portion is equipped with advancing device and places the cabin body, control center and place the cabin body and drive arrangement and place the cabin, central cabin body lower part is equipped with down advancing device and places the cabin body and place the cabin body for last advancing device, control center and place the cabin body, drive arrangement and place the power supply unit of the cabin body power supply and place the cabin body, drive arrangement places the cabin top and is the overhead hatch cover that can open and shut.

As an improvement, an escape ejection seat is arranged in the driving device placing cabin.

As an improvement, a turnover cabin door is arranged at the bottom of the dish body, steps are arranged on the inner side surface of the turnover cabin door, an access passage from the turnover cabin door to the cabin for placing the driving device is arranged in the dish body, and vertical steps arranged along the access passage are arranged in the access passage.

As an improvement, the outer surfaces of the upper propulsion device placing cabin body and the control center placing cabin body are paved with solar panels.

As a refinement, the openable top hatch is a transparent hatch.

As an improvement, a plurality of illuminating lamps are further arranged on the outer side of the annular protection support.

After the structure more than adopting, the utility model has the advantages of as follows: the aircraft can be used as a new aircraft for carrying out activities such as transportation, traveling, exploration and the like; the aircraft can take off and land vertically without a special runway, and can conveniently change directions through a transverse turbine jet or a direction control propulsion device of an upper propulsion device chamber and a lower propulsion device chamber below a flight propeller protective cover while flying in the air.

Drawings

Fig. 1 is a schematic structural diagram of the flying saucer aircraft of the present invention.

Fig. 2 is a schematic structural view of a protective cover for a flying oar in a flying saucer aircraft.

Fig. 3 is a schematic structural diagram of an electromagnetic track in a flying saucer aircraft of the present invention.

Fig. 4 is a schematic structural view of a flying oar in a flying saucer aircraft.

Fig. 5 is a schematic structural view of the steps in the flying saucer aircraft.

As shown in the figure: 1. the disc body, 1.1, the central cabin body, 1.2, go up propulsion unit and place the cabin body, 1.3, the control center places the cabin body, 1.4, the cockpit is placed to the piloting device, 1.5, the cabin body is placed to lower propulsion unit, 1.6, power supply unit places the cabin body, 2, flight oar, 2.1, annular flight oar support, 2.2, the paddle, 3, the support that descends, 4, the electromagnetic orbit, 5, the electromagnetic suspension car, 6, turbine jet support, 7, turbine jet, 8, flight oar safety cover, 8.1, annular protection support, 8.2, go up the dictyosome, 8.3, the dictyosome down, 9, the upset hatch door, 10, the access way, 11, go up the lower ladder, 12, the light.

Detailed Description

With the attached drawings, the flying saucer aircraft is characterized by comprising a saucer body 1, flying paddles 2 and a landing bracket 3, the middle part of the disc body 1 is circumferentially provided with an electromagnetic track 4, the electromagnetic track 4 is a concave track with the middle part sunken inwards, an electromagnetic suspension vehicle 5 matched with the electromagnetic track 4 is arranged in the electromagnetic track 4, the flying oar 2 is connected with the outer surface of the electromagnetic suspension vehicle 5, and can rotate around the disc body 1 along an electromagnetic track under the driving of an electromagnetic suspension vehicle 5, turbine jet supports 6 are also arranged at the two sides of the disc body 1 and at the lower part of the flying oar 2, rotatable coupling has turbojet 7 on turbojet support 6, turbojet 7 of dish body 1 one side is vertical setting, and the opposite side is horizontal setting, it sets up in 1 bottoms of dish body to descend support 3, it is folding support to descend support 3.

As a preferred embodiment of this embodiment, the flying oar protective cover 8 is arranged outside the flying oar 2, the flying oar protective cover 8 includes an annular protective support 8.1 which is arranged outside the flying oar 2 and is located at the same horizontal plane with the flying oar 2, the upper end and the lower end of the annular protective support 8.1 respectively extend towards the disc body 1 and are arranged to cover the upper net body 8.2 and the lower net body 8.3 of the flying oar 2, and the tail ends of the upper net body 8.2 and the lower net body 8.3 are connected with the disc body 1. The arrangement of the protective cover 8 of the flight oar does not influence the air circulation, and can prevent floating objects and birds from entering the rotor blade.

As a preferred embodiment of the present embodiment, the flying oar 2 includes an annular flying oar support 2.1 disposed outside the electromagnetic levitation vehicle 5, and a plurality of blades 2.2 are circumferentially disposed outside the annular flying oar support 2.1.

As a preferred embodiment of this embodiment, the blade 2.2 is an inclined blade having an angle with the horizontal plane.

As a preferred embodiment of this embodiment, the disk body 1 includes a central cabin 1.1 provided with an electromagnetic track 4, the upper portion of the central cabin 1.1 is provided with an upper propulsion device placing cabin 1.2, a control center placing cabin 1.3 and a steering device placing cabin 1.4, the lower portion of the central cabin 1.1 is provided with a lower propulsion device placing cabin 1.5 and a power supply device placing cabin 1.6 for supplying power to the upper propulsion device placing cabin 1.2, the control center placing cabin 1.3, the steering device placing cabin 1.4 and the lower propulsion device placing cabin 1.5, and the top of the steering device placing cabin 1.4 is an openable top cabin cover.

As a preferred embodiment of this embodiment, the electromagnetic track 4 is a recessed central track, the electromagnetic levitation vehicle 5 is embedded in the recessed central portion of the electromagnetic track 4, the magnetic poles of the electromagnetic levitation vehicle 5 and the electromagnetic track 4 are repulsive magnetic poles, the electromagnetic levitation vehicle 5 and the electromagnetic track 4 are kept in middle, up and down non-contact, and are in a levitation state, after the power supply is started, the electromagnetic coil traction force arranged inside the electromagnetic track 4 is utilized to make the electromagnetic levitation vehicle 5 rotate around the disk body 1 along the electromagnetic track 4, so as to drive a circle of flying paddles 2 on the periphery of the electromagnetic levitation vehicle 5 to rotate, when the rotation speed reaches a certain speed, the upward acting force of the flying paddles 2 is large enough to drive the whole disk body 1 to suspend upwards, then the rear portion of the flying disk is slightly pushed upwards by using a vertical turbine jet below a flying paddle protective cover, so that the flying paddles suck air from top to bottom, become from the top to the below inspiration air backward, the propulsion mode of emulation helicopter impels forward to this realizes the purpose of flying saucer suspension and flight, starts when flying the dish, and the rotor blade is rotatory, and its powerful centrifugal force can make whole dish body follow rotatory, consequently starts the setting simultaneously and controls the dish body with the horizontal turbojet of flying oar safety cover below and stabilize.

The transverse turbine jet arranged below the flight propeller protective cover can adjust the direction by increasing and reducing the rotating speed.

Set up in the direction control advancing device of two-layer advancing device room about the dish body, can set to left right interworking, realize the direction adjustment, if: when the vehicle turns to the left, the direction control propelling device on the right side is started, and the vehicle body can turn to the left side. When turning to the right, the direction control propulsion device on the left side can be started, and the dish body turns to the right side. The device can also be used for propelling by using the propelling device in an environment without air when a flying saucer is applied to outer space in the future. The direction can be adjusted by controlling the propulsion device by the direction of the propulsion device chamber.

The power supply group in the power supply room can be set as a battery pack or a nuclear power group, the power supply device is placed in the cabin body at the lower part of the disc body, and the flying disc can keep the gravity downward after the power supply device is installed, so that the flying disc cannot tilt or turn over;

as a preferred embodiment of the present embodiment, an escape ejection seat is arranged in the driving device placing cabin 1.4.

As a preferred embodiment of this embodiment, the control center placing cabin is further provided with a large parachute and an injection device for a flying saucer aircraft to land, and an outlet of the large parachute and the injection device are connected to a central position of the control device placing cabin, when the flying saucer breaks down or is powered off in the air flight process, the cabin cover is synchronously and automatically opened in a propping manner, or the flying saucer is directly blasted, and then the large parachute is ejected to land on the flying saucer, so that the safety of the flying saucer can be greatly improved, if the large parachute fails to be ejected, the flying saucer together with a seat is ejected out of the cabin through an escape ejection seat, a pilot pulls the parachute worn on the body, throws away the seat to land, and the safety of the pilot and the upward ejection posture of the head of the pilot can be guaranteed by means of an ejection mode of a military.

As a preferred embodiment of this embodiment, a turnover hatch door 9 is disposed at the bottom of the disk body 1, a step is disposed on an inner side surface of the turnover hatch door 9, an access passage 10 from the turnover hatch door 9 to the cab 1.4 of the driving device is disposed in the disk body 1, and a simple up-down step 11 is disposed in the access passage 10 up and down along the access passage 10.

As a preferred embodiment of this embodiment, the outer surfaces of the upper propulsion device placing cabin 1.2 and the control center placing cabin 1.3 are paved with solar panels.

As a preferred embodiment of the present embodiment, the openable top hatch is a transparent hatch.

As a preferred embodiment of the embodiment, a plurality of illuminating lamps 12 are further arranged on the outer side of the annular protective bracket 8.1, the lamps can be turned on at night and used for illuminating and beautifying during taking off and landing, and in addition, a headlamp can be arranged at one end of the flying saucer.

Based on the structure of the utility model, the utility model can be used as a new aircraft to carry out activities such as transportation, travel, exploration and the like; can be used as a space flight vehicle; can be used as a flying saucer simulation toy and the like.

The present invention and the embodiments thereof have been described above, but the description is not limited thereto, and the embodiment shown in the drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should understand that they should not be limited to the embodiments described above, and that they can design the similar structure and embodiments without departing from the spirit of the invention.

Claims

1. The utility model provides a flying saucer aircraft, its characterized in that, includes the dish body, flight oar, descending support, dish body middle part circumference is equipped with the electromagnetism track, the electromagnetism track is the inside sunken "concave" style of calligraphy track in middle part, be provided with rather than the complex electromagnetism car that suspends in the electromagnetism track, the flight oar is connected in the outer surface of electromagnetism suspension car to can rotate around the dish body along the electromagnetism track under the drive of electromagnetism suspension car, dish body both sides still are equipped with the turbojet support on lieing in the position of flight oar lower part, be connected with the turbojet on the turbojet support, the turbojet of dish body one side is vertical setting, and the opposite side is horizontal setting, the descending support sets up in dish body bottom, the descending support is folding support.

2. The flying saucer aircraft of claim 1, wherein a flying oar protecting cover is arranged outside the flying oar, the flying oar protecting cover comprises an annular protecting support which is arranged outside the flying oar and is positioned on the same horizontal plane with the flying oar, the upper end and the lower end of the annular protecting support extend towards the direction of the saucer body respectively and are provided with an upper net body and a lower net body which can cover the flying oar, and the tail ends of the upper net body and the lower net body are connected with the saucer body.

3. The flying saucer aircraft of claim 2, wherein the flying oar comprises an annular flying oar support arranged outside the electromagnetic levitation vehicle, and a plurality of blades are circumferentially arranged outside the annular flying oar support.

4. A flying saucer aircraft according to claim 3, wherein said blades are inclined blades arranged at an angle to the horizontal.

5. The flying saucer aircraft as claimed in claim 1, wherein the saucer body comprises a central cabin body provided with an electromagnetic track, the upper part of the central cabin body is provided with an upper propulsion device placing cabin body, a control center placing cabin body and a steering device placing cabin, the lower part of the central cabin body is provided with a lower propulsion device placing cabin body and a power supply device placing cabin body for supplying power to the upper propulsion device placing cabin body, the control center placing cabin body, the steering device placing cabin body and the lower propulsion device placing cabin body, and the top of the steering device placing cabin body is an openable top cabin cover.

6. The flying saucer aircraft as claimed in claim 5, wherein said driving device placing cabin is provided with an escape ejection seat.

7. The flying saucer aircraft according to claim 5, wherein said bottom of said saucer body is provided with a turnover door, said turnover door is provided with steps on an inner side, said saucer body is provided with an access passage from said turnover door to said cockpit, and said access passage is provided with vertical steps along said access passage.

8. The flying saucer aircraft as claimed in claim 5, wherein said upper propulsion device placing cabin and said control center placing cabin are laid with solar panels on outer surfaces thereof.

9. A flying saucer aircraft according to claim 5, wherein said openable top hatch is a transparent hatch.

10. The flying saucer aircraft of claim 2, wherein a plurality of illuminating lamps are further arranged outside said annular protecting frame.