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Case study Case

Tests der Cockpittüren von Düsenflugzeugen

  • Fallstudie Vibrationstest
  • Luft- und Raumfahrt
  • Zufällig

Test-Übersicht

■ EUT

600 mm × 50 mm × H1800 mm, 20 kg

Shaker fixture

1000 mm × 1000 mm × H2000 mm, 350 kg
PSD in Fig. 2, X-axis 5h, Y-axis 2.5h, Z-axis 2.5h, 4-point average control, 8 response measurement points

X-axis excitation

Requirement PSD Cockpit door

Memo

Verwendete Einrichtungen

Vibration test system with slip table: EMK2605S/EM16HM/H10
*Up to 2,000 Hz is not compatible with i260/H10
Vibration controller: K2 12 input 1output software Random
Acceleration sensor: VP-32 × 12 pcs.
Dedicated fixture: 350 kg

Dauer des Tests

8 Stunden / 2 Tage

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