5200.020000.04600.0
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Interactive 3D model of HVLA C-17 Cutaway Assembly

Enclosures and housings

HVLA C-17 Cutaway Assembly

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Bounding box
20000.0 × 5200.0 × 4600.0 mm
Engine
Precision B-rep
Parameters
28
Published
August 25, 2026

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The prompt

A parametric 3D CAD assembly visualization demonstrating the kinematic operation of the Hardened Vertical Logistics Airframe (HVLA) dual-tier structure inside an aircraft fuselage cross-section. 1. CONTEXT (BOUNDING ENVELOPE): Render a high-resolution, translucent cutaway profile of a high-wing military strategic airlifter (C-17 profile) cabin. Display the aircraft's primary structural frames, skin, and overhead ceiling infrastructure (crane rails and winches). The fuselage cutaway must provide 4.1 meters internal vertical clearance from the floor. 2. AIRCRAFT FLOOR MECHANICS: The primary cargo floor must be modeled with standard 463L pallet tie-down track geometry. The HVLA structure is securely fastened to this grid via standard mechanical interface hardpoints. 3. KINEMATIC DUAL-TIER ASSEMBLY (MOTION): The HVLA system must be modeled as a fully articulated assembly, not a static render. It features two distinct, movable structural decks: - Define a prismatic joint (vertical constraint) that allows the elevated UPPER DECK platform (which must hold a military payload) to actuate linearly. - Define a simultaneous, reciprocal kinematic constraint that causes the LOWER DECK CASSETTE (trench-locking mechanism) to compress or expand vertically based on the Upper Deck position. - The prompt must specify kinematic interaction where moving the upper deck down causes the lower deck trench mechanism to reduce its volume. 4. VEHICLE PAYLOAD SPECIFICATIONS: On the moving elevated UPPER DECK, model a single, detailed Land Rover Wolf (TUL/TUM HD) utility vehicle, modified specifically for air transport configuration to fit low-headroom clearances: - Model the vehicle in a special "air transport configuration": - The front windshield assembly is folded 90-degrees FORWARDS, resting flat on the engine hood bonnet. - The modular roll cage protection system is completely DISASSEMBLED and stowed horizontally alongside the vehicle body to further reduce total height. - Model standard low-profile air transport suspension compression settings. 5. OUTPUT DETAILS: - Render the system at 45-degree isometric front cutaway perspective. - Show component bodies (Fuselage Cutaway, HVLA Lower Cassette, HVLA Upper Deck, Land Rover Wolf (AT Config)) as distinct solid bodies. - Include kinematic visualization indicators showing the 1.0m+ cleared safety headroom remaining beneath the aircraft ceiling infrastructure when the vehicle is stowed.

Parameters

NameValueRange
Fuselage Internal Vertical Clearance4100 mm3500 – 5000
Fuselage Inner Width5200 mm4500 – 6000
Fuselage Skin Thickness100 mm50 – 200
Number of Structural Frame Ribs5 mm2 – 8
Crane Rail Ceiling Offset200 mm100 – 400
Cargo Floor Length20000 mm15000 – 25000
Cargo Floor Width5000 mm4000 – 6000
Cargo Floor Thickness400 mm200 – 600
463L Tie-Down Track Count5 mm2 – 10
Tie-Down Track Width60 mm20 – 120
Tie-Down Track Depth30 mm10 – 80
Hardpoint Count8 mm2 – 16
Hardpoint Pad Size200 mm80 – 400
Hardpoint Pad Height50 mm20 – 120
HVLA Lower Cassette / Upper Deck Elevation500 mm250 – 900
HVLA Upper Deck Thickness300 mm100 – 500
HVLA Lower Cassette Length5500 mm4500 – 7000
HVLA Lower Cassette Width2800 mm2200 – 3500
Prismatic Guide Post Size120 mm60 – 200
Upper Deck Platform Length5200 mm4500 – 6500
Upper Deck Platform Width2800 mm2200 – 3500
Land Rover Wolf Length4500 mm4000 – 5000
Land Rover Wolf Width2000 mm1800 – 2200
Land Rover Wolf Height (Reduced)1800 mm1500 – 2000
Folded Windshield Thickness80 mm40 – 150
Stowed Roll Cage Length3500 mm2500 – 4500
Stowed Roll Cage Width400 mm200 – 600
Stowed Roll Cage Height500 mm200 – 700

Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.