Carrier aircraft arresting hook landing impact test equipment and method based on electromagnetic ejection
The invention discloses a carrier-based aircraft arresting hook landing impact test device and method based on electromagnetic ejection, and relates to the technical field of aviation aircraft test, and the test device comprises an electromagnetic acceleration track, a test bench, and a sliding tabl...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | The invention discloses a carrier-based aircraft arresting hook landing impact test device and method based on electromagnetic ejection, and relates to the technical field of aviation aircraft test, and the test device comprises an electromagnetic acceleration track, a test bench, and a sliding table trolley. The electromagnetic acceleration track is sequentially divided into a mover parking area, an electromagnetic acceleration area, an impact test area, an electromagnetic deceleration area and a hydraulic braking area from left to right according to functional sections. The test method comprises the following steps: S1, equipment homing; s2, equipment debugging; s3, simulating secondary impact; and S4, simulating primary impact. The sliding table trolley is accelerated through the electromagnetic ejection technology, the device has the advantages of being large in stored energy and controllable in speed, the sliding table trolley can be rapidly accelerated to the preset speed in a short time, the accelerati |
---|