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Locking mechanism for radome

A fairing and locking technology is applied in the field of improvement of a fairing locking mechanism in a helicopter power cabin, and can solve the problems of the influence of the fairing's aerodynamic shape, insufficient secondary protection of the locking mechanism, complex structure, etc., and achieves simple structure, aerodynamic Smooth-looking, quick on/off effect

Inactive Publication Date: 2013-07-17
HARBIN
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there are similar mechanisms on more mature helicopters in China, but the structure is relatively complicated, especially in the secondary protection of the locking mechanism.
At the same time, limited by the mechanism, most locking mechanisms have an impact on the aerodynamic shape of the fairing, so these effects need to be improved

Method used

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  • Locking mechanism for radome
  • Locking mechanism for radome
  • Locking mechanism for radome

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specific Embodiment approach

[0013] Specific embodiments: the present invention will be further described in detail below in conjunction with the accompanying drawings, please refer to Figure 1 to Figure 3 .

[0014] The locking mechanism includes: a lock assembly and a lock bracket assembly.

[0015] The lock assembly includes: rubber stop block 4, J-shaped piece 5, safety cover 6, pull ring 7, adjustable lock 8, rubber block 9, safety cover spring 10, shaft 11, U-shaped piece 12 and fastening assembly 13, 15 etc. The adjustable lock 8 is fixed on the U-shaped part 12 through bolts and self-locking nuts (fastening components 15); the pull ring 7 is directly installed on the adjustable lock 8; the rubber stopper 4 is clamped between the U-shaped part 12 and the J-shaped The parts 5 are fastened by bolts and self-locking nuts (fastening assembly 13); the safety cover spring 10 and the safety cover 6 are fixed on the U-shaped part through the shaft 11; the rubber block 9 is glued on the safety cover 6; ...

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Abstract

The invention belongs to the field of aircraft radome systems and relates to an improvement for a locking mechanism of an engine compartment radome system. The locking mechanism comprises a lock support assembly and a lock assembly, wherein the lock support assembly comprises a lock support 1, a clamp ring support, a clamp ring and a fastening assembly; and the lock assembly comprises a rubber stop block, a -shaped piece, a safety cap, a pull ring, an adjustable lock, a rubber block, a safety cap spring, a shaft, a U-shaped piece and fastening assemblies. When the locking mechanism is mounted, the lock assembly is in bolted connection with a radome, the lock support assembly is fixed on a platform with rivet. The lock support assembly and the lock assembly can fix the radome through matching of the clamp ring, the rubber stop block, the protective cap, the adjustable lock and other assemblies, so that a locking function is realized. The locking mechanism can fasten the radome and can provide secondary protection for the assemblies of the radome; the exchange among different batches of radomes can be met by adjusting the locking mechanism; and in addition, the shape of the locking mechanism is smooth, thereby realizing a rectifying effect.

Description

technical field [0001] The invention belongs to the field of helicopter fairing systems and relates to the improvement of the locking mechanism of the helicopter power cabin fairing. Background technique [0002] The main function of the locking device is to fix the fairing of the power cabin so that it forms a stable structure to protect various equipment in the power cabin. [0003] At present, there are similar mechanisms on more mature helicopters in China, but the structure is relatively complicated, especially in the secondary protection of the locking mechanism. At the same time, limited by the mechanism, most of the locking mechanisms have influence on the aerodynamic shape of the fairing, so these influences need to be improved. Contents of the invention [0004] The purpose of the present invention is to propose a new type of locking mechanism, which is installed on the fairing of the power cabin to meet the requirements of the fairing system on the secondary pr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C7/00
Inventor 王玉璠许兰波陈豹夏玉娟徐书博
Owner HARBIN
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