Coaxial homodromous propeller with variable phase difference

A technology of propeller and phase difference, which is applied in the direction of propeller, transportation and packaging, aircraft parts, etc., can solve the problems of propeller aerodynamic efficiency reduction, unfavorable dynamics, shortening the range of propeller aircraft, etc.

A technology of propeller and phase difference, which is applied in the direction of propeller, transportation and packaging, aircraft parts, etc., can solve the problems of propeller aerodynamic efficiency reduction, unfavorable dynamics, shortening the range of propeller aircraft, etc.

CN113184167AActive Publication Date: 2021-07-30BEIHANG UNIV

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  • Coaxial homodromous propeller with variable phase difference
  • Coaxial homodromous propeller with variable phase difference
  • Coaxial homodromous propeller with variable phase difference

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Embodiment Construction

[0034] In order to understand the above-mentioned purpose, features and advantages of the present invention more clearly, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0035] In the following description, many specific details are set forth in order to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described here. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. EXAMPLE LIMITATIONS.

[0036] The present invention proposes a propeller that uses coaxial rotation in the same direction, that is, two propellers with coincident rotating axes are arranged front and rear along the thrust di...

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Abstract

The invention discloses a coaxial homodromous propeller with variable phase difference. Two propellers with coincident rotating shafts are arranged front and back in the thrust direction of the propellers and comprise front propellers, propeller rotating shafts, sliding sleeves and rear propellers. The two propellers rotate in the same direction. A certain phase difference exists between the rear propeller and the front propeller to ensure that the rear propeller is far away from the wake flow spiral surface of the front propeller. In the actual operation process, if the wake flow helicoid approaches the rear propeller due to the change of the forward ratio, the rear propeller adjusts the phase difference formed between the rear propeller and the front propeller through the forward and backward movement of the sleeve, so that the rear propeller can still be located outside the wake flow area of the front propeller. According to the invention, adverse aerodynamic interference and aerodynamic noise of a coaxial propeller system are reduced.

Description

technical field [0001] The invention belongs to the technical field of aircraft propulsion device design, in particular to a coaxial and same-direction propeller with variable phase difference. Background technique [0002] When the maximum diameter of the propeller is limited, the most important means to increase the thrust of the propeller is to increase the area of ​​the rotor blade, that is, to increase the solidity of the rotor. Increasing the solidity of the rotor can be achieved by increasing the chord length of the blade and increasing the number of blades. For example, propeller fighter jets in the 1930s mainly used two-bladed and three-bladed propellers, typical examples such as Yi-16 (two-bladed), La-9 (three-bladed), etc. But in the late 1940s, four-bladed propellers gradually became mainstream, such as Ki-84, P-51, etc. [0003] Considering that the efficiency of the propeller will decrease when the solidity of the rotor exceeds a certain range, the industry h...

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Application Information

Patent Timeline
30 Jul 2021
Publication
CN113184167A
IPC
B64C11/48
CPC
B64C11/48
Inventors
蒋崇文; 李志豪