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Helicopter tail shaft installing structure

An installation structure and technology for helicopters, which are applied in the directions of power units, bearings, and mechanical equipment on aircraft, and can solve problems such as shaft damage, bearing impact, and affecting the normal use of bearings.

Pending Publication Date: 2019-10-18
HARBIN DONGAN ENGINE GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the process of rotation and torsion transmission of the tail shaft, vibration is inevitable. When the speed reaches a critical value, the vibration is the largest, and the vibration will cause the axial movement and radial deflection of the shaft, which will cause impact on the bearing. If the bearing cannot The deflection along with the shaft, making this deflection "soft landing" will cause greater wear of the bearing, affect the normal use of the bearing, and at the same time damage the shaft itself

Method used

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  • Helicopter tail shaft installing structure
  • Helicopter tail shaft installing structure
  • Helicopter tail shaft installing structure

Examples

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Embodiment Construction

[0019] Such as figure 2 , 3 , Shown in 4, the tail shaft installation structure includes support 1, combined bearing 2, nut 3, nut 4, base 5, limit bolt 6, fuse 7, stud pile 8, joint bearing 9, bolt 10. Wherein, the combined bearing includes an outer ring 21 , a spherical outer ring 22 , a collar 23 , a sealing cover 24 , a cage 25 , rolling balls 26 , and an inner ring 27 . Two joint bearings 9 are installed on the lower part of the support 1, the inner ring of the joint bearing is slightly higher than the outer ring, and the outer ring is fixed to the support by flanging and embedding. The joint bearing is fixed on the base 5 by bolts 10 and nuts 4 . A lug is set on the outer edge near the mounting hole of the limit bolt 6, and the limit bolt is fixed and locked with a fuse. In addition, the web stiffener structure is used in the lower part of the support to reduce the weight without changing its strength. The combined bearing 2 is fixed on the support 1 by using double...

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PUM

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Abstract

The invention belongs to the field of helicopter tail shafts, and particularly relates to a helicopter tail shaft installing structure. A helicopter tail shaft is in a segmented type, and a supportingbase (1) is arranged at the connected position of two segments of the shaft; the two segments of the shaft are connected by a spline, and a combination bearing (2) is arranged in the supporting base(1); the combined portion of the two segments of the shaft is installed in the combination bearing (2); the combination bearing comprises a first bearing body and an outer ring (21); the first bearingbody comprises a spherical outer ring (22), a holder (25), a rolling ball (26) and an inner ring (27); the rolling ball (26) is fixed between the spherical outer ring (22) and the inner ring (27) through the holder (25), and rotating in the circumferential direction is guaranteed; the first bearing body is located in the outer ring (21); the spherical outer ring (22) and the outer ring (21) are in spherical face cooperation, and a combination bearing body is formed; and the first bearing body and the outer ring (21) can relatively swing. A helicopter tail shaft compensating structure is provided.

Description

technical field [0001] The invention belongs to the field of helicopter tail shafts, in particular to a helicopter tail shaft installation structure. Background technique [0002] The tail shaft of the helicopter is located between the main reducer, the intermediate reducer and the tail reducer, and its function is to transmit the power output from the tail of the main reducer to the tail reducer to drive the tail rotor. Due to the large distance between the main reducer and the tail rotor, it is a more reasonable combination method to divide the tail shaft into several short shafts, and the shafts are connected by bearing fulcrums, see figure 1 . In the process of rotation and torsion transmission of the tail shaft, vibration is inevitable. When the speed reaches a critical value, the vibration is the largest, and the vibration will cause the axial movement and radial deflection of the shaft, which will cause impact on the bearing. If the bearing cannot Deviating along wi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16C19/50F16C23/08F16C33/32F16C33/58F16C33/66B64D35/00
CPCF16C19/50F16C23/082F16C33/32F16C33/583F16C33/664B64D35/00
Inventor 徐童童于伟欧阳可平冯磊李远周丽芳张羽徐秀波齐晓辉胡克伟
Owner HARBIN DONGAN ENGINE GRP
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