See how a wire mesh layer with resistive elements dissipates carpet electrostatic charges while
An embedded heating layer in vehicle or aircraft lining delivers fast radiant cabin heating without combustion gases and also supports de-icing.
A partitioned mounting bracket secures large coaxial attenuators to rigid aircraft structures, preventing vibration-driven disconnection.
Plasma emission sensing guides laser perforation in acoustic panels, stopping before core walls and adhesive bonds are damaged.
Flexible outboard stringer clips secure aircraft fuselage insulation blankets without compression, easing installation and reducing condensation issues.
Optical emission sensing controls laser perforation depth in acoustic panels to avoid core wall and adhesive bond damage.
Porous outer layers and a channeled core reflect and dissipate sound waves to cut aircraft cabin noise without sacrificing lightweight panel structure.
Self-aligning feet position a partitioned acoustic cell on curved reflective layers, widening frequency attenuation without alignment loss.
A partitioned honeycomb cell with feet and a conduit broadens acoustic attenuation while maintaining alignment in curved aircraft propulsion structures.
A chamfered door edge, sharp junction, and triangular insert redirect airflow and suppress 5-10 kHz cavity noise at aircraft access doors.
A chamfer and sharp ridge stabilize flow separation at an aircraft access door, reducing cavity noise especially from 5 to 10 kHz.