Aerial wind-energy power-station aircraft and aerial fixation aircraft device

Abstract

An aerial wind-energy power-station aircraft relates to the technical field of engineering such as manufacture of power-driven aircrafts, aerial wind power and photoelectricity, aerial transportation and military affairs. The aircraft comprises an aircraft body (1) or a buoyancy lift body (20), a control system (4) and a propelling system (5). The aircraft is characterized in that the aerial wind-energy aircraft also comprises an aerial wind power generation system (2), a storage system (3) of power electric energy and a grounding and water-connecting system (6), wherein the power propelling system (5) comprises an electric propelling flight system (5.1). When the grounding and water-connecting system (6) is connected to an easy-to-connect ground object (12), an aerial fixation aircraft device (13) and a water body (14), the system stays at a stationary state and can start aerial wind-power generation. When the storage system (3) of the power electric energy is filled with aerial wind electricity, the electricity can then be supplied to the electric propelling flight system (5.1), so that flight can be driven. In this way, no fuel is consumed, and the flight can be implemented by ''aerial wind energy and wind electricity''. The aircraft has a very low cost; and by the storage system (3) of the power electric energy or the aerial fixation aircraft device (13), the aerial wind electricity with the very low cost can also be conveyed to the ground for utilization.

Description

technical field [0001] The invention relates to engineering technical fields such as electric aircraft manufacturing, airborne wind power generation, airborne photovoltaic power generation, airborne transportation, airborne mobile houses, military airlift equipment, and military field power generation equipment. Background technique [0002] The existing aircraft has the following problems. 1. Most of the existing aircraft take off and land on the airport, and cannot take off and land vertically. 2. The flight range of existing vertical take-off and landing helicopters is short and slow. 3. The existing aircraft is not safe, as long as an accident occurs in the air, it may cause a fall. 4. Existing aircrafts are expensive and complicated to control, which limits their widespread use in a large number; it is not as easy as automobiles to widely enter the family and private daily fields. 5. The existing aircraft only has a function as a means of transportation, and does not...

AI Technical Summary

Problems solved by technology

1. Most of the existing aircraft rely on the airport to take off and land, and cannot take off and land vertically

2. The existing vertical take-off and landing helicopters have a short flight range and a slow speed

3. The existing aircraft is not safe, as long as an accident occurs in the air, it may cause a fall

4. Existing aircrafts are expensive and complicated to control, which limits their widespread use; it is not as easy as cars to widely enter the family and private daily fields

5. Existing aircraft only have the function of being a means of transportation, without adding the function of being an air power station

6. Existing aircraft can only be parked on the ground, not in the air

7. Existing aircraft have not fully developed the excellent structure of electric powered parachute

1. Existing powered parachutes only rely on lift to fly, and do not make full use of buoyancy instead of lift to reduce lift energy consumption and save fuel and energy

2. Existing paramotors consume liquid fuel and do not make full use of solar power

3. Most of the existing powered parachutes take off and land horizontally, and cannot take off and land vertically

4. The existing powered parachute is not safe, as long as an accident occurs in the air, it may cause a fall

1. Since the airborne fixed aircraft device (13) is not used, the external power lines and tethered ropes carried by itself are cancelled, resulting in the aerial photovoltaic power generation device being heavy, low in efficiency, high in cost, and unable to be used flexibly

2. Since there is no propulsion system's turn mechanism and pitch change mechanism, the airborne wind power system cannot adjust direction and speed, and the efficiency is low and the cost is high

3. Since the aerial wind power generation system is not installed on the two sides of the buoyant system, the spatial structure of the aerial photovoltaic power generation system is unstable

4. Since the buoyant system is not separated from the aerial wind power generation system by the length-adjustable sling group system, the center of gravity of the power generation equipment floating in the sky is too high, the overall structure is unstable, and it is easy to be blown over by strong winds and the whole body overturns

5. Since there is no length-adjustable sling group system to separate the buoyant system from the aerial wind power generation system, the attitude of the aerial photovoltaic power generation device cannot be adjusted, so that the solar panels cannot track sunlight and the photoelectric conversion rate cannot be improved.

6. Due to the small diameter of the aerial wind power generation system, the power generation is too small

Images