Rear single-propeller compound-wing aircraft with non-thrust compound ailerons

Abstract

The invention relates to a compound lift aircraft with an expanded platform. The compound lift aircraft with the expanded platform is composed of a rear single-propeller compound-wing aircraft and non-thrust self-energized compound ailerons installed on the two sides of the rear single-propeller compound-wing aircraft body; the rear single-propeller compound-wing aircraft comprises a plane, compound lift wings fixedly installed on the two sides of the plane and a propeller; the plane is arranged as a deck platform; self-sealing ducted-fans are arranged in the compound lift wings, and wing hinges are designed on the outer sides of the compound lift wings; self-sealing ducted-fans are arranged in the non-thrust self-energized compound ailerons, power liquid and gas connectors and wing hingesare arranged on one sides or the two sides of the non-thrust self-energized compound ailerons, and the non-thrust self-energized compound ailerons are movably connected with the compound lift wings through the wing hinges. The compound lift aircraft with the expanded platform not only has the advantages of being short in take-off and landing distance, high in flying speed, high in wing structurestrength, capable of energy storage by means of the wings, low in flying energy consumption, long in hang time and the like, but also the large-area compound lift wings can be used as gliders in the emergency situation, thus the safety of the aircraft is greatly improved, and the safety of personnel and materials is ensured.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single propeller compound wing aircraft with a non-thrust compound auxiliary wing, belonging to the technical field of aircraft equipment. Background technique [0002] Existing aircraft are mainly divided into two categories: fixed-wing and vertical take-off and landing aircraft (such as helicopters and multi-rotors). Of course, there is also a vertical take-off and landing fixed-wing product. The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvantages of high ener...

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