Civil aviation engine fuel pump support

The invention discloses a civil aviation engine fuel pump support. The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: NING XUEMEI, YUAN YAN
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention discloses a civil aviation engine fuel pump support. The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the supporting frame is of a disc-shaped structure, the edge of the back face of the supporting frame is fixedly connected with a dustproof edge of a circular-ring-shaped structure, a pipe hole allowing an oil pipe to penetrate through is formed in the top end of the supporting frame, a pipe body protection mechanism is installed at the pipe hole, the pipe body protection mechanism comprises a protection block which is installed on the supporting frame and a wear-resisting ring which is arranged inthe pipe hole, and fasteners used for connecting the supporting frame with an aero-engine are distributed on the surface of the supporting frame. According to the civil aviation engine fuel pump support, the contact abrasion