A vertical take-off and landing (VTOL) aircraft
A vertical take-off and landing, aircraft technology, applied in the field of aircraft, can solve the problems of restricting the development and popularization of aircraft, customers unable to meet flight desires, and the runway cannot hover in the air, etc., to save space and improve efficiency.
Inactive Publication Date: 2019-01-25
FOSHAN SHENFENG AVIATION SCI & TECH
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Problems solved by technology
[0002] Traditional fixed-wing aircraft have the characteristics of safe flight, fast flight speed, long range and large carrying capacity, but they need to use the runway during take-off and landing and cannot hover in the air; while fixed-wing aircraft have become the first choice for people to travel, but are affected by Due to the limitation of the venue, most customers cannot satisfy their desire to fly, which greatly limits the development and popularization of aircraft
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[0013] Now in conjunction with accompanying drawing, the present invention is described in detail: a kind of vertical takeoff and landing aircraft, comprises fuselage 1, control system 5, first power unit 6, second power unit, wing, flat tail 13, the 3rd power unit, vertical Tail 18, landing gear 19.
[0014] The fuselage 1 includes a nose and a nacelle, the nose includes an engine 2 and a battery 3, and the nacelle includes an operating lever 4, a control system 5, a seat and an instrument panel; the first power unit 6 is located in front of the nose, and the The above-mentioned wings are located on the left and right sides of the fuselage 1, and there are two wings in total, and each wing has a first arc-shaped slot 9; the second power unit is located at the first arc-shaped slot 9 of the wing. In the middle; the horizontal tail 13 and the vertical tail 18 are located at the rear of the fuselage 1, and there are two horizontal tails 13, which are distributed on the left and ...
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A VTOL aircraft belongs to the technical field of aircraft and comprises a fuselage, a control system, a first power unit, a second power unit, a wing, a horizontal tail, a third power unit, a vertical tail and a landing gear. The fuselage comprises a nose and a nacelle, the nose comprises an engine and a battery, and the nacelle comprises an operating lever, a control system, a seat and an instrument panel. The first power unit is located in front of the nose, and the wing is located on the left and right sides of the fuselage. There are two wings in total, and each wing has an arc-shaped groove. A second power unit is located in the arcuate groove of the wing; Horizontal tail and vertical tail are located at the tail of the fuselage. The landing gear is located below the fuselage in a rear three-point configuration. The invention fully utilizes the lift force generated by the second power device and the third power device to drive the aircraft to take off and land vertically, saves the space required by the aircraft when taking off and landing, improves the efficiency in flight and the utilization rate of energy.
Description
technical field [0001] A vertical take-off and landing aircraft belongs to the technical field of aircraft, and in particular relates to a vertical take-off and landing aircraft. Background technique [0002] Traditional fixed-wing aircraft have the characteristics of safe flight, fast flight speed, long range and large carrying capacity, but they need to use the runway during take-off and landing and cannot hover in the air; while fixed-wing aircraft have become the first choice for people to travel, but are affected by Due to the limitation of the venue, most customers cannot satisfy their desire to fly, which greatly limits the development and popularization of aircraft. Contents of the invention [0003] The objective of the present invention is to overcome the deficiency of above-mentioned traditional aircraft, invent a kind of aircraft that can take off and land vertically. [0004] A vertical take-off and landing aircraft includes a fuselage, a control system, a fi...
Claims
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Login to View More IPC IPC(8): B64C27/28B64C27/52B64C29/00B64D31/00
CPCB64C27/28B64C27/52B64C29/0008B64D31/00
Inventor 罗哲远王志成
Owner FOSHAN SHENFENG AVIATION SCI & TECH