Aeroplane static stress testing

Customer need / challenge

Aeroplane static stress testing simulates extreme flight conditions to assess the aircraft’s structural integrity. The challenge is accurately measuring the forces on key components without causing damage. Load cells are crucial for providing precise data on the stress experienced by parts like the fuselage and wings. This data helps engineers identify weak points and ensure the aircraft’s safety and reliability.

Interface solution

Diagram of our aeroplane static stress test solution

Interface suggests using multiple 1208 Flange Standard Precision Universal LowProfile Load Cells during the static stress test. 1208s are installed along the aircraft to measure forces and stresses that might be experienced during various flight conditions. Force is exerted on the aircraft and its wings. This allows engineers to make adjustments to the design to enhance performance and structural integrity.

Results

Our 1208 Flange Standard Precision Universal LowProfile Load Cells usage was a success, providing accurate, real-time data on the forces experienced during the aeroplane static stress test.

Materials

1208 Flange Standard Precision Universal LowProfile Load Cells

How it works

Multiple 1208 Flange Standard Precision Universal LowProfile Load Cells are installed at certain key points along the aircraft and its wings for the static stress test.
The static aircraft is subjected to a number of different flight conditions.
The load cells measure the forces at these specific locations, which are then sent to the customer’s computer system for analysis.

Products used in this application note

1208 Flange Standard Precision Universal LowProfile Load Cell

1208 Flange Standard Precision Universal LowProfile Load Cell. Read more about this product here.
Depending on the objectives of your test, the following two products may also be suitable:
- 1000 Series Fatigue Rated Load Cell
- 1200 Precision Series