CN201347198Y - Propeller vertical take-off and landing aircraft with rectifying device - Google Patents

Abstract

A propeller vertical take-off and landing aircraft with a rectifier is intended to provide a propeller vertical take-off and landing aircraft that does not produce left and right torsion swing during take-off, landing, flight and air stop, so that the aircraft can stably take off and land vertically, fly and stay in the air, and can ensure a certain degree of stability of the aircraft in an emergency, thereby playing a role of safety and energy saving. The propeller vertical take-off and landing aircraft includes a fuselage, a control device, a power device and a propeller, wherein the control device and the power device are installed in the fuselage, and the propeller is installed above the fuselage. The characteristic is that it also includes a rectifier, and the rectifier includes at least two rectifier plates, wherein the rectifier plates are in the shape of flat strips, and the plane of the flat plate is parallel to the axial direction of the aircraft propeller shaft, that is, perpendicular to the rotating plane of the propeller, and the rectifier plates are installed under the fuselage in a cross-intersecting manner.

Description

Propeller vertical take-off and landing aircraft with fairing

technical field

The utility model relates to a propeller aircraft, in particular to a propeller vertical take-off and landing aircraft with a rectifying device which can stably and safely take off and land vertically, fly and stay in the air.

Background technique

Known propeller vertical take-off and landing aircraft such as helicopters, model airplanes (or toy) propeller aircraft, etc. include organisms, control devices, power units and propellers. The control device and the power unit are installed in the body, and the propeller is installed above the body. There are two types of vertical take-off and landing aircraft with multiple propellers and a small rotor with single propeller and tail rudder. All rely on the rotation of the propeller, so that the air on the upper and lower surfaces of the propeller produces a pressure difference to bring lift to the aircraft, and then adjust the flight attitude of the aircraft by controlling the pitch of each blade of the aircraft or controlling the small rotor of the tail rudder of the aircraft. direction. Since the propeller generates lift by the rotating airflow, this rotating airflow will generate reverse torsion, causing the aircraft to twist left and right, so that it is difficult to make the aircraft take off and land stably, fly and stay in the air, which poses a potential threat to the safety of the aircraft. And the constant threat, that's its downside.

Contents of the invention

Aiming at the shortcomings of existing propeller aircraft, the purpose of this utility model is to provide such a propeller vertical take-off and landing aircraft with a rectifying device, which will not produce left and right torsion during take-off and landing, flight and air stay, so that the aircraft is stable. It can take off and land vertically, fly and stay in the air, and can ensure a certain degree of stability of the aircraft in an emergency, playing the role of safety and energy saving.

The technical solution adopted by the utility model to solve its technical problems is: including the body, the control device, the power device and the propeller, the control device and the power device are installed in the body, and the propeller is installed on the top of the body, and it is characterized in that: it also includes a rectifier The rectifying device comprises at least two rectifying plates, the rectifying plates are in the shape of flat strips, and the plane of the plates is parallel to the axial direction of the aircraft screw shaft, that is, perpendicular to the plane of rotation of the propeller, and the rectifying plates are intersected and installed under the body.

The beneficial effect of the utility model is that: the rectifying device composed of strip-shaped rectifying plates can make most of the rotating air flow generated by the rotation of the propeller vertically downward, and the reverse torque can be converted into a downward thrust, so that the aircraft can take off and land, fly and fly in the air. There will be no left and right torsion during the stop, and it can take off and land stably, fly and stay in the air; when the landing point is complicated, such as uneven ground or on a turbulent ship, the rectifier can act as a landing support. In this way, the propeller is prevented from hitting the ground when the aircraft is not perpendicular to the landing ground; and a certain lift force can be generated to play a role of safety and energy saving. When an emergency landing is required, the rectifying plate can make the aircraft descend vertically without tilting and rolling, so that the aircraft is in a stable state to a certain extent, thereby greatly improving the safety factor in emergency situations; the rectifying plate can adjust the flight direction by adjusting the angle And the effect of generating vector thrust. Especially in its embodiment, the annular wing is added, which can not only protect the propeller from spinning against objects close to the aircraft during flight and shutdown, but also prevent the horizontal wind from directly blowing on the propeller to affect the normal operation of the aircraft.

Description of drawings

Below in conjunction with accompanying drawing, the utility model is further described.

Fig. 1 is a structural representation (model airplane) of the present utility model.

Fig. 2 is a schematic diagram of the overall structure of the rectification device of the present invention.

Fig. 3 is a schematic structural diagram of the second embodiment of the present invention.

Fig. 4 is a schematic diagram of the combined structure of the rectifying device and the annular wing according to the second embodiment of the present invention.

Among the figure: 1 is the body, 2 is the propeller, 3 is the rectifying device, 4 is the annular wing, 31 is the rectifying plate, 32 is the rectifying plate. 33 is a connector, and 34 is a connector.

Detailed ways

Referring to accompanying drawing, the utility model comprises organic body 1, control device, power unit and propeller 2, and control device, power unit are contained in the body 1, and propeller 2 is contained in the top of body 1, is characterized in that: also comprises rectifying device 3, The rectifying device 3 includes at least two rectifying plates 31, 32, the rectifying plates are in the shape of flat strips, the flat plane is perpendicular to the plane of rotation of the propeller, and the rectifying plates 31, 32 cross each other, and the body 1 is installed on the rectifying plates 31, 32 superior. Rectifying plate 31,32 tops are connected with connecting piece 33,34, and connecting piece 33,34 profile can be arc shape, make connecting between rectifying plate itself and rectifying plate and between rectifying plate and the body into a stable whole. The cross section of the connectors 33, 34 can be rectangular, square, circular, streamlined or other shapes. According to the number of rectifying plates, cross connections in the shape of 'ten', 'well', 'feng' and 'm' can be formed. Inside the rectification device 3.

In the embodiment of the present utility model, the rectifying device 3 includes two rectifying plates 31, 32, the board surfaces of the two rectifying plates 31, 32 are vertical to the plane of rotation of the propeller, and the vertical intersection between the two rectifying plates 31, 32 is ' Cross ' shape, its top has connecting piece 33,34, and connecting piece 33 (or 34) is arc belt shape, and rectifying plate 31,32 forms annular belt shape, and body 1 is contained in this annular belt.

The rectifying plates 31, 32 cross each other, and the bottom line is in a plane, which can be used as a landing support, so that the whole aircraft can be parked on the ground smoothly. The flat strip structure of the rectifying plates 31 and 32 can change the lateral torsion force formed by the rotation of the propeller 2 into a downward thrust. So that the aircraft will not produce torsion.

The rectifying plates 31, 32 can also adjust the inclination angle between their plate surfaces and the plane of rotation of the propeller as required.

In the second embodiment of the present utility model, the annular wing in the "Annular Wing Vertical Take-Off and Landing Vehicle" that the applicant applied for patent protection on the same day is installed, so that the utility model also includes an annular wing 4, on which the annular wing 4 The narrow bottom and wide shape is in the shape of a ball table (spherical ring) or a truncated cone, and is installed on the rectification device 3 and surrounds the outside of the propeller 2. In this way, not only can the propeller 2 be protected from whirling against objects close to the aircraft during flight and shutdown, but also can prevent the cross wind from blowing directly on the propeller to affect the normal operation of the aircraft. And it can generate a certain lifting force, which plays the role of safety and energy saving.

Claims (4)

1. A propeller vertical take-off and landing aircraft with a rectifying device, comprising a body (1), a control device, a power device and a propeller (2), the control device and the power device are installed in the body (1), and the propeller (2) is installed in the body (1). Above the machine body (1), it is characterized in that it also includes a rectification device (3), the rectification device (3) includes at least two rectification plates (31), (32), and the lower part of the rectification plate is in the shape of a flat strip, which The plane of the flat plate is perpendicular to the plane of rotation of the propeller, and the rectifying plates (31), (32) cross each other, and the body (1) is installed on the rectifying plates (31), (32). 2. A propeller vertical take-off and landing aircraft with rectifying device according to claim 1, characterized in that: the upper part of the rectifying plate (31, 32) is connected with the connecting piece (33, 34), and the connecting piece (33, 34) 34) The shape is in an arc shape, so that the rectification plate itself and the rectification plate and between the rectification plate and the body are connected into a stable whole. The section of the connecting piece (33, 34) can be rectangular, square, circular, streamline shape. 3. A propeller vertical take-off and landing aircraft with rectification device according to claim 1 or 2, characterized in that: according to the number of rectification plates, the characters of "cross", "well" and "feng" can be formed , 'm' shaped cross, the body (1) is installed in the rectification device (3) composed of rectification plates (31, 32) and connectors (33, 34). 4. A propeller vertical take-off and landing aircraft with rectifying device according to claim 1 or 2, characterized in that it also includes a ring wing (4), the shape of which is narrow at the top and wide at the bottom, like a ball table Shape or truncated cone shape, and is installed on the rectification device (3) and surrounds outside the propeller.

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