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Manned flying saucer

A flying saucer and personnel technology, applied in the field of aircraft, can solve the problems of complex air flight operations, slow speed, high energy consumption, etc., and achieve the effects of small landing area, fast flight speed and safe flight

Inactive Publication Date: 2015-05-27
STATE GRID CORP OF CHINA +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Helicopters are mainly used for low-altitude flights to perform special missions. They use propellers as the flight power, which has slow speed, high energy consumption, and high requirements for the flight environment. However, it is difficult to be widely used as an airborne vehicle.
However, the take-off and landing environment of existing types of aircraft is limited by various conditions, and the air flight operation is complicated, unable to take off and land vertically, and the control is inconvenient

Method used

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Embodiment Construction

[0028] Such as figure 1 As shown, the present invention includes an electric automatic control system, and a secondary vacuum chamber 2 is arranged outside the primary vacuum chamber 1, and the upper parts of the two vacuum chambers form a continuous and smooth arch to ensure that the two vacuum chambers are not squeezed by air pressure to the greatest extent. Compression deformation, the first-level vacuum chamber 1 accounts for 85% of the total volume of the flying saucer, and the second-level vacuum chamber 2 can provide maneuvering power for flying or submerging, and can quickly adjust the attitude of the flying saucer to ensure that the flying saucer can be out of control, mishandling, or appearing. Quickly adjust high-speed avoidance in the event of failure or danger. Solar panels 3 are installed on the top of the primary vacuum chamber 1. The DC motor system is installed at the bottom of the primary vacuum chamber 1. The DC motor system includes the main engine rotor 5 a...

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Abstract

The invention provides a manned flying saucer, relating to the technical field of aircrafts. The manned flying saucer comprises an electric automatic control system, a first-grade vacuum chamber and a second-grade vacuum chamber. A solar cell panel is installed on the top of the first-grade vacuum chamber; the second-grade vacuum chamber is arranged outside the first-grade vacuum chamber; a direct-current motor system is mounted on the bottom of the first-grade vacuum chamber and comprises a main engine rotor and stators locating at both sides of the main engine rotor; a storage battery pack is arranged around the direct-current motor system; a personnel cabin and a magazine are arranged at the periphery of the direct-current motor system; an auxiliary engine is arranged at the bottom of the second-grade vacuum chamber; air suction windows are arranged along the outer edge of the manned flying saucer; an atmospheric pressure highly-sensitive sensor is arranged at the lower end of the second-grade vacuum chamber and between the personnel cabin and the magazine; and a vertical-lift air suction window is arranged at the connection place of the second-grade vacuum chamber and the first-grade vacuum chamber. The manned flying saucer provided by the invention takes off and lands steadily, can stay in air for a long time and fly at a fast speed, is exempt from interference of electric waves and influence of road and weather conditions, is safe in flight, occupies a small area when landing and is especially applicable to aerial surveillance, command and urgent repair in the industries like the power supply industry, traffic and marine accident rescue, anti-terrorism and antiriot action and police enforcement.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a manned flying saucer. Background technique [0002] Existing manned aircraft mainly contain spaceships, helicopters, airplanes and the like. Helicopters are mainly used for low-altitude flights to perform special missions. They use propellers as flight power, have low speed, high energy consumption, and high requirements for the flight environment. However, they are difficult to be widely used as airborne vehicles. However, for existing various aircrafts, the take-off and landing environment is limited by various conditions, and the air flight operation is complicated, unable to take off and land vertically, and the control is inconvenient. In today's society, with the development of material science, computer automatic control technology and high-sensitivity sensors, the opening and closing of the suction window of high-elastic and smooth material required by the new type of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00B64D27/24
CPCY02T50/50Y02T50/60
Inventor 李劭毅
Owner STATE GRID CORP OF CHINA
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