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Case study Case Studies

Jet aircraft cockpit door testing

  • Vibration test case study
  • Aerospace
  • Random

Test overview

■ 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

Facilities used

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

Test time

8 hours /2 days