Reading lamp structure integrating knob and hose

A technology of reading lights and knobs, which is applied in the field of aircraft lighting systems, to achieve the effect of optimizing the structure design, reducing the overall size, and making the knobs clear and easy to distinguish

Pending Publication Date: 2021-06-08
SHANGHAI AVIATION ELECTRIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that the knob of the reading light is placed on the control box in the prior art, and provide a new type of reading light structure in which the knob and the hose are integrated

Method used

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  • Reading lamp structure integrating knob and hose
  • Reading lamp structure integrating knob and hose
  • Reading lamp structure integrating knob and hose

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Embodiment Construction

[0013] The present invention will be further described in detail below through specific embodiments in conjunction with the accompanying drawings. It should be noted here that the descriptions of these embodiments are used to help understand the present invention, but are not intended to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0014] See Figures 1 to 4 , what is shown in the figure is a reading light structure in which the knob and the hose are integrated. The structure of the reading light is composed of a device housing 1, an installation front plate 2, a hose part 3, a lamp head part 4, a knob part 5, a damping block 6, a potentiometer part 7, a connecting guide rod 8 and a circuit printed board 9 and other parts. composition.

[0015] The device housing 1 has a housing top w...

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PUM

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Abstract

The invention discloses a reading lamp structure integrating a knob and a hose. The reading lamp structure is composed of a device shell, a mounting front plate, a hose part, a lamp holder part, a knob part, a potentiometer part, a connecting guide rod and a printed circuit board. The reading lamp structure has the beneficial effects that the appearance size of the hose type reading lamp is reduced, the installation space is saved, the operation is easy and convenient, and the knob is clear and easy to distinguish.

Description

technical field [0001] The invention relates to an aircraft lighting system, in particular, a reading light structure in which a knob and a hose are integrated. Background technique [0002] With the development of society and the replacement of various military and civil aircraft, the layout of the aircraft cabin is becoming more and more simplified and integrated, and the utilization rate of the cabin space is also continuously improving. In order to improve the utilization rate of the cabin space, the designers have racked their brains. [0003] For the convenience of pilots to read and operate, there is often a hose-type reading light with adjustable brightness, adjustable irradiation angle and fixation in the aircraft cabin. Usually, the knobs for dimming of hose-type reading lights are placed on the control box and separated from the hose. Compared with the smaller reading lamp, the dimming knob takes up a lot of space, and when there are many knobs and switches arou...

Claims

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Application Information

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IPC IPC(8): F21S8/00F21V23/04F21V21/32F21W107/30
CPCF21S8/00F21V23/04F21V21/32F21W2107/30
Inventor 杨富王晶高赟
Owner SHANGHAI AVIATION ELECTRIC
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