| 摘要 |
The present invention relates to an intake cover of an aircraft of which a structure is simple for the intake cover of an aircraft to be easily manufactured and for a manufacturing cost to be reduced. Moreover, the intake cover of an aircraft is easily installed and removed through weight lightening, and in installing and removing processes, worries with respect to an accident can be dispelled. The intake cover of an aircraft comprises: a body formed to have column shape wherein a hollow portion is provided, and having a mounting groove along an external wall, wherein a path extends from an internal side to an upper surface of the mounting groove; a handle having a grip unit which protrudes to an upper portion of the body and a rod portion which is formed in both ends of the grip unit and inserted into the path; and a sealing member which is installed to be inserted into and protrude to the mounting groove, and is in contact with an end portion of the rod portion. When the handle is pushed to be inserted into the inside of the body, the sealing member protrudes to the outside by means of an end of the rod portion and is in contact with an inner circumferential surface of an intake of an aircraft. Moreover, a cover is fixated to the intake by only movement to push the handle when installing the intake cover of an aircraft. |
