Assembled flight power module and aircraft

Abstract

The invention discloses an assembled flight power module and an aircraft, the assembled flight power module comprises a power module body, a motor and a propeller assembly, a duct is formed in the power module body, the motor is arranged in the duct, and the propeller assembly is arranged at the upper end of the motor. The invention belongs to the technical field of aircrafts. According to the invention, through modularization and unitization of components of the personal aircraft, compatibility and interchangeability of the components, especially modularization of power components and standardization of propulsion components, rapid assembly and disassembly of the personal aircraft are enhanced, so that the cost problem, the volume problem and the safety problem of the personal aircraft are solved. And maintenance and industrial problems are solved, the improvement of a personal aircraft industry chain is accelerated, and then the popularization of personal aircrafts is realized.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an assembled flight power module, and also to an aircraft. Background technique [0002] Existing commercial personal aerial vehicle mainly has two kinds of fixed wing and rotary wing. [0003] Fixed-wing aircraft must have sufficient sliding speed wings to generate sufficient lift. Therefore, fixed-wing aircraft not only require a runway for take-off and landing, but also have large wings and fuselages, which are difficult to carry and park. Difficult to popularize. [0004] In order to solve the ground problem of the take-off and landing site, the current personal aircraft generally develop towards the helicopter that can take off and land vertically; the helicopter is divided into various forms such as single propeller, multi-propeller, coaxial reverse double propeller and ducted propeller; The weight of the fuselage and load is pulled up vertically, and the investment in po...

AI Technical Summary

Problems solved by technology

[0004] In order to solve the ground problem of the take-off and landing site, the current personal aircraft generally develop towards the helicopter that can take off and land vertically; the helicopter is divided into various forms such as single propeller, multi-propeller, coaxial reverse double propeller and ducted propeller; The weight of the fuselage and load is pulled up vertically, and the investment in power is generally large. Therefore, the cost of vertical take-off and landing personal aircraft is relatively high, and the volume is not small. There are still site problems, and there are many safety hazards. For example, high-speed rotating rotors are easy to injure people or self-injury, etc. Whether it is a single-propeller or multi-propeller personal aircraft, the general diameter is about three or four meters, and the single-propeller personal aircraft is even larger, requiring more parking space than household The site requirements of the car, and it cannot be parked in a closed space such as a basement or a garage. In the case that residents in our country generally live in buildings, it has not yet reached the level of popularization.

[0005] There is also a type of personal aircraft that uses jet engines. Although it does not require a runway and is not large in size, due to the small output of personal aircraft and no design standards, the current cost of personal aircraft is generally high, and the cheap ones are about 300,000 yuan. Difficult to popularize in a short time

[0006] The current personal aircraft is still in its infancy, there is no industry standard and a complete industrial chain, and the problems of difficult maintenance, few and expensive parts are still difficult to solve

Images