Carbon fiber composite aircraft

Abstract

The invention discloses a carbon fiber composite aircraft which comprises a manned seat bin and a paragliding, wherein the manned seat bin is provided with a seat bin framework made of a carbon fiber composite material; a driving assembly is arranged at the rear part of the seat bin framework; the seat bin framework comprises a left main supporting ring beam, a right main supporting ring beam and a back frame; the bottoms of the two main supporting ring beams are connected with each other through a plurality of transverse supporting rods; a front seat and a rear seat are arranged above the transverse supporting rods; a main front beam connection rod is arranged between the two main supporting ring beams on the front part of the seat bin framework; an arched front shock absorption supporting frame is arranged in the middle of the main front beam connection rod; the left side and the right side of the rear part of the seat bin framework are respectively hinged with a left rear shock absorption supporting frame and a right rear shock absorption supporting frame; and heavy load shock absorption springs are arranged between the rear shock absorption supporting frames. Shock absorption supports are arranged on front wheels and rear wheels of the manned seat bin framework made of the carbon fiber composite material, so that the weight of the manned seat bin is greatly reduced, and a passenger is wrapped in the manned seat bin framework; when the aircraft is landed, impact is greatly reduced; and the passenger is effectively protected.

Description

technical field [0001] The invention relates to a low-altitude flight equipment, in particular to a carbon fiber composite aircraft. Background technique [0002] In the prior art, low-altitude aircraft generally include a powered seat cabin and a paraglider. The disadvantage is that the passenger cabin is heavy and bears a huge impact when landing, which lacks effective protection for the occupants. Contents of the invention [0003] The technical problem to be solved by the present invention is to propose a carbon fiber composite aircraft with light weight and good protection against the deficiencies of the prior art. [0004] The technical problem to be solved by the present invention is achieved through the following technical solutions. A carbon fiber composite aircraft includes a manned seat cabin and a flying parachute, and is characterized in that: the manned seat cabin is provided with a seat made of carbon fiber composite material. The cabin frame is equipped w...

AI Technical Summary

Problems solved by technology

[0002] In the prior art, low-altitude aircraft generally include a powered cabin and a parachute. The disadvantage is that the passenger cabin is heavy and bears a huge impact when landing, which lacks effective protection for the occupants.

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