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Internal control rotor wing supporting piece structure

A technology for supporting parts and rotors, which is applied in the field of inner-operating rotor supporting parts, can solve the problems of difficult spline design, processing and assembly, inability to achieve multiple connections, and single function of the supporting parts, and achieves reduction of structural weight, installation and disassembly. The effect of convenient, weight-saving design

Pending Publication Date: 2022-01-18
CHINA HELICOPTER RES & DEV INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The support of the conventional rotor is splined to the rotor shaft and has a single function. To adopt the spline connection, the spline must first be designed on the support and the rotor shaft, and the spline connection requires a cone ring, a main shaft screw, a bearing Plates, locking screws and other structures, many connection structures
Moreover, the spline design, processing and assembly are difficult
Therefore, the conventional support has a single function and cannot realize multiple connection functions

Method used

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  • Internal control rotor wing supporting piece structure
  • Internal control rotor wing supporting piece structure
  • Internal control rotor wing supporting piece structure

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Experimental program
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Embodiment Construction

[0030] The present invention will be further explained by the specific embodiments:

[0031] The present invention discloses a support structure 1 of a coaxial rotor, including a support member 14, a first shoulder bushing 11, a second shoulder bushing 13, a third shoulder press 15, and a straight bushing 12, A shoulder bushing 11, the second shoulder bushing 13, the third shoulder bushing 15, and the straight bushing 12 cooperate with the support member 14.

[0032] The structure has a plurality of connection functions: connected to the inner rotor shaft 3, connected to the rocker assembly 4, connected to the torque arm, and connect 6;

[0033] This structure is a cylindrical segment for connection with a cylindrical surface of the inner rotor shaft. The cylindrical segment is a non-equivalent thickness cylinder, the wall thicknefits of the bolt connection area is the largest, and it is changed to the main bearer; the uppermost annular wall thickness is used to prevent a large de...

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PUM

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Abstract

The invention belongs to the field of rotor supporting piece structure design, and discloses an internal control rotor supporting piece structure. A hollow cylindrical section, a conical section, a reinforcing rib section and a circular ring section are sequentially divided from top to bottom; the hollow cylindrical section is connected with an inner rotor shaft; the circular ring section is connected with a guide cylinder; the circular ring section is further connected with a torque arm assembly; and the reinforcing rib section is connected with a rocker assembly. A plurality of first bolt holes are formed in the lower end of the hollow cylindrical section in the radial direction, and a shoulder lining is arranged in each first bolt hole; the hollow cylindrical section is connected with the inner rotor shaft through a bolt; the thickness of a bolt hole area of the hollow cylindrical section is largest, the thickness of an annular area close to the upper end face of the hollow cylindrical section is second, and the thickness of other parts of the hollow cylindrical section is smallest. The supporting piece structure is of a multifunctional structure, and the functions of quick and simple connection with the rotor shaft, the connection with the rocker assembly, the connection with the guide cylinder and the connection with the torque arm assembly are achieved.

Description

Technical field [0001] The present invention belongs to the field of rotor support structural design, which discloses an inner manipulating rotor support structure. Background technique [0002] The common-shaft double-rotor helicopter has the characteristics of fast flight, high housing efficiency, good motor, low noise, etc. . The common shaft helicopter has two rotors, two sets of automatic inclinters, two sets of rotings. The upper rotor automatic tilt unit of the coaxial helicopter is an internal manipulation structure. The entire manipulation system is located inside the helicopter rotor shaft, eliminating the interference of the external manipulation pulling rod to pneumatic interference compared to the routine external manipulation helicopter, and can effectively reduce the waste resistance of the rotor system in flight, improve the helicopter Performance, therefore in the inner manipulation system is widely used on different models of co-shaft helicopters. [0003] The s...

Claims

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Application Information

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IPC IPC(8): B64C27/32B64C27/52B64C27/10
CPCB64C27/32B64C27/52B64C27/10
Inventor 张飞李永鑫李德玉陆裕辉王健
Owner CHINA HELICOPTER RES & DEV INST