3. Impact test facility setup

Impact test facility setup 学习卡片

Passenger airbag (PAB) performance cannot be validated by a single test type. The PAB system must deploy reliably, at the right time, with the right pressure, and interact correctly with a restrained or out-of-position occupant. Three complementary facility configurations are used across the development cycle: the static deployment rig, the sled test, and the full vehicle crash test. Each answers a different question, and each imposes different constraints on instrumentation, fixture design, and correlation with CAE.

Static Deployment Rig: Free-Field and In-Vehicle Module Tests

The static deployment rig isolates the airbag module from vehicle dynamics. Its purpose is to characterize the inflator and cushion as a system: deployment timing, cushion pressure, seam integrity, and — critically for PAB — the interaction with the instrument panel (IP) tear seam and the windshield.

Two sub-configurations are common:

  • Free-field (open-air) deployment: the module is mounted on a rigid fixture with no IP or windshield. This gives the baseline cushion fill curve and is used for inflator lot acceptance and CAE material-model calibration.
  • In-vehicle-position static deployment: the module is installed in a production or representative IP, with the windshield and A-pillar trim present. This captures tear-seam opening, cushion trajectory over the IP top surface, and windshield contact.

A typical static rig setup uses a rigid steel frame anchored to a seismic mass. The module is bolted through its production mounting points with the production torque specification (for example, 8–10 N·m for M6 fasteners). The IP is supported so that its stiffness approximates the body-in-white (BIW) condition; a common mistake is to over-constrain the IP, which suppresses tear-seam opening and produces an unrealistically clean deployment.

Instrumentation for a static test usually includes:

  • At least two pressure transducers inside the cushion (vent-side and throat-side) sampled at ≥ 20 kHz.
  • High-speed video at 1000–2000 fps, with a calibrated grid in the field of view.
  • A current probe on the inflator squib to record the fire command and confirm the trigger time.
  • Optionally, a load cell under the module mount to capture reaction force.

The key output is the cushion pressure–time curve. For a 60 L class PAB at 23 °C, a representative curve rises to a first peak within roughly 15–25 ms of the fire command, then settles. If the first peak is late or low, suspect a restricted tear seam or a cold inflator. If the pressure spikes abnormally high, suspect a blocked vent or a cushion that failed to unfold.

Sled Test: Occupant Kinematics with Controlled Pulse

The sled test reproduces the crash pulse without destroying a full vehicle. It is the workhorse for PAB restraint-system tuning because it allows repeatable pulse control and dense instrumentation at lower cost than a full vehicle test.

The sled facility consists of a rail-mounted carriage, a propulsion system (typically a hydraulic or pneumatic accelerator, or a deceleration sled with a crushable or hydraulic absorber), and a body buck. For PAB work, the buck must reproduce the relevant BIW stiffness at the IP, toe board, and seat mounts. A common approach is to cut a section of the production BIW — the cowl, IP mounting structure, and floor pan — and weld it into the sled buck.

Pulse selection is the first engineering decision. For a frontal PAB evaluation, a typical pulse is a 50 km/h equivalent barrier pulse with a peak deceleration of about 35–40 g and a duration of 100–120 ms. The pulse is defined as a target corridor; the sled must stay inside the corridor at every time step. The corridor is usually specified as a band around a nominal curve, for example ±3 g or ±10% of the nominal value, whichever is greater.

Occupant setup follows the relevant regulation or internal standard. For a 50th percentile male Hybrid III, the seat is set to the mid-track position, the seat back angle to 25° from vertical, and the H-point located per the standard procedure. The PAB is fired at a time offset relative to the pulse onset — typically 10–20 ms after the pulse reaches its threshold — so that the cushion is fully inflated as the occupant moves forward.

Instrumentation on a PAB sled test typically includes:

Channel Sensor Typical Sample Rate Purpose
Sled acceleration Accelerometer on carriage 10 kHz Pulse verification
Occupant head acceleration Tri-axial accelerometer in head 10 kHz HIC calculation
Chest deflection Chest potentiometer / IR-TRACC 10 kHz Chest compression
Cushion pressure Pressure transducer 20 kHz Deployment timing
Fire command Current probe 20 kHz Trigger reference

After the test, the primary correlation metrics are head resultant acceleration, HIC15, chest deflection, and the time of head-to-cushion contact. The last is obtained from high-speed video and is the most sensitive indicator of deployment timing error. If the head contacts the cushion before it is fully pressurized, HIC rises sharply; if contact occurs after the cushion has begun to vent, the restraint effect is reduced.

Full Vehicle Crash Test: The Final Integration Check

The full vehicle test is the definitive validation. It uses a complete vehicle with production IP, windshield, seats, restraints, and all trim. The test can be a rigid barrier impact at 50 km/h (or the applicable regulatory speed), an offset deformable barrier (ODB) impact, or a pole test depending on the requirement.

For PAB evaluation, the critical difference from the sled is that the vehicle structure deforms. The IP moves rearward and downward as the front end crushes, which changes the effective distance between the module and the occupant. This structural motion is difficult to reproduce on a sled and is a major source of sled-to-vehicle correlation error.

Vehicle instrumentation mirrors the sled, with additional channels for:

  • Vehicle longitudinal and vertical acceleration at the B-pillar and tunnel.
  • IP displacement relative to the occupant compartment (using a string potentiometer or optical tracking).
  • Windshield strain or crack detection if the cushion interacts with the glass.

The fire time is controlled by the vehicle's airbag ECU, which uses crash sensors to discriminate the event. In a full vehicle test, the actual fire time is measured from the squib current and compared with the ECU's intended command. A delay of more than a few milliseconds between command and squib current indicates a wiring or connector issue.

Choosing the Right Configuration and Correlating with CAE

The three configurations form a progression. The static rig calibrates the inflator and cushion model. The sled validates occupant kinematics and restraint timing under a controlled pulse. The full vehicle test confirms that the integrated system works with real structural deformation.

For CAE correlation, each configuration maps to a different model scope:

  • Static rig → inflator mass-flow and temperature model, cushion fabric permeability, and seam failure criteria.
  • Sled → occupant positioning, seat belt interaction, and PAB firing time. The sled model uses a prescribed pulse, so structural deformation is not simulated.
  • Full vehicle → full frontal crash model with BIW, IP, and occupant. This is the most expensive and the most sensitive to material and joint modeling.
A practical correlation rule: if the sled test matches CAE within 10% on HIC and chest deflection, but the full vehicle test does not, the discrepancy is almost always in the structural deformation — IP rearward motion, toe board intrusion, or seat mount displacement. Check those before adjusting the airbag model.
Do not use a static deployment rig to tune occupant restraint timing. The static rig has no occupant and no pulse; it can only validate the inflator and cushion. Using static pressure data to set the sled fire time is a common and costly error.
PAB Evaluation Facility Progression and CAE Mapping Static Deployment Rig Module + IP + windshield No occupant, no pulse Outputs: cushion pressure, tear-seam opening, trajectory CAE: inflator + cushion model permeability, seam criteria Sled Test Body buck + occupant Controlled pulse corridor Outputs: HIC, chest deflection, head-cushion contact time CAE: occupant kinematics, fire timing, belt interaction Full Vehicle Crash Complete vehicle + BIW Barrier / ODB / pole Outputs: HIC, chest defl., IP displacement, ECU fire time CAE: full frontal model, BIW + IP + occupant calibrate integrate Correlation Checkpoints and Typical Failure Symptoms Static Rig Check Pressure peak late/low → restricted tear seam Pressure spike high → blocked vent / no unfold Fix: inflator model, permeability, seam Sled Check HIC high, contact early → fire too late HIC low, contact late → fire too early / venting Fix: fire time, occupant position, belt routing Full Vehicle Check Sled OK, vehicle not → structural deformation IP rearward motion, toe board intrusion Fix: BIW model, joints, seat mount stiffness

The facility setup is not a one-time decision. As the design matures, the same PAB module moves from static rig to sled to full vehicle, and the CAE model is refined at each stage. The correlation engineer's job is to ensure that the model scope matches the test scope — using a full vehicle model to correlate a static rig test, or a static rig model to predict sled HIC, will produce misleading results and wasted iterations.