Fuselage Shells/Cabin Structure

LATP + Hot Stamping

Carbon / PPS, PEKK

Rapid build rates, integration of stiffeners, weldable skin sections

Rotor Fairings & Nacelles

In-situ LATPLATP

Carbon / PEKK, PPS

High-temp capable, aerodynamic, suitable for repeated cycling

Wing Skins (Distributed Propulsion Designs)

LATP + Hot Stamping

Carbon / PEKK

Lightweight, strong, integrates actuation hardpoints, weldable

Battery/Energy System Housings

LATP + Vacuum Forming

Glass / PPS, PEI

Flame resistance, fast prototyping, dimensional repeatability

Interior Cabin Panels/Sidewalls

In-situ LATPLATP

Glass / PEI, PPS

Low weight, recyclable, compliant with cabin FST needsFST要求

Landing Skids/Support Beams

LATP + Hot Stamping

Carbon / PPS, PEKK

High toughness, crash resilience, integrated ribbing possible

Canopy/Upper Shell Fairing

In-situ LATP or LATP + Vacuum Forming

Glass / PPS

Lightweight, flame-resistant, ideal geometry for automated layup

Main Fuselage Shell (Fixed-Wing UAVs)

LATP + Hot Stamping

Carbon / PPS, PEKK

Stiff, lightweight, weather resistant, automated build

Wing Panels & Control Surfaces

In-situLATP or LATP + Hot Stamping

Carbon  / PPS, PEKK

Low mass, high stiffness, tailored layup

Multirotor Arms & Beams

In-situLATP

Carbon / PPS, PEKK

Excellent bending stiffness, fatigue resistance

Payload Bays & Modular Pods

LATP + Vacuum Forming

Carbon or Glass / PPS, PEKK

Modular, thermally stable, impact resistant

Landing Skids/Legs

In-situLATP

Carbon / PPS

Impact absorption, fatigue-resistant

Propeller Blades (Large Multirotors)

LATP + Vacuum Forming

Carbon / PPS 或 PEEK

Tailored stiffness, low inertia

Protective Fairings & Sensor Shrouds

In-situLATP

Glass / PEI, PPS

Lightweight, weatherproof, easily replaceable