| 摘要 |
The present invention relates to a monitoring device for an aircraft engine compressor, which includes a photographing module and a display module. The photographing module comprises a bracket, which is fixed to the inside of an aircraft engine compressor to be removed; a camera unit, which is fixed to the bracket to be moved in different directions, photographs the operation status of the compressor, and produces the images; and a transmission side controller, which controls the camera unit and wirelessly transmits image signals of the camera unit. The display module comprises a display unit, which displays the image produced in the camera unit; and a receiving side controller, which receives image signals transmitted from the transmission side controller and controls the display unit. The bracket has multiple concave grooves, which prevents the heat of the compressor from being delivered to the camera unit. The camera unit prevents unnecessary light from being diffusely reflected, thereby making the diffusion angle of light constant by a diffused reflection prevention filter. Therefore, a user can precisely monitor the operation status of the aircraft engine compressor by using clear images. Also, heat influence can be minimized by a heat blocking glass tube, so heat stability can be increased. |
