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#thin wall

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Vista de Swept-Wing EDF Jet — Assembled Airframe and Complete Print Kit

Swept-Wing EDF Jet — Assembled Airframe and Complete Print Kit

OVERVIEW A swept-wing EDF aircraft printing project with a source-derived static assembled display. The actual fuselage, joined canopy, six-section left and right wings, multipart ailerons, horizontal stabilisers, elevators, vertical stabiliser and four-section rudder are positioned with rigid transforms. The complete display retains 47 mesh instances and 3,175,018 source triangles. No missing power-system or purchased hardware has been invented. The silver finish is a proposed model-making treatment, not evidence of a physical build or flight test. FILES AND VARIANTS The complete resource archive preserves 182 distinct payloads: 56 supplied STL resources plus 50 distinct STL variants recovered from native projects, 31 Simplify3D factory projects, four MatterControl slice files, 38 source G-code presets, two PDF documents and one JPEG reference. All source formats and alternatives remain available. Factory project references were reconciled to functional opaque filenames while numerical transforms and source machine commands were retained. Native factory GUI compatibility has not been certified. Separate downloads provide the full-resolution coloured 3MF assembly, its opaque native Blender scene archive and a convenience archive of all 106 STL resources. The 3MF is a full-resolution display, not a validated single-piece printing instruction. The Blender assembly was independently reopened. Detailed English guidance is included in the archives. Original manuals, decal material, necessary notices and 3DLabPrint credits remain available. OPTIONAL FITTINGS Separate native resources include EDF-ring size options, equipment mounting pieces, a canopy latch, wheel components, wing covers, nose guns and a small tail fitting. These remain supplied resources rather than proof of installed equipment in the display. Consult the guide for bought-in servos, EDF, electronics, springs, rods and landing-gear requirements. The digital assembly does not certify their operation or compatibility. SCALE AND DIMENSIONS The guide states approximately 1:8 and nominal dimensions around 1220 mm wingspan, 1220 mm length and 460 mm height. These are unverified source specifications. Current static digital bounds are approximately 1205.64 mm longitudinally, 1222.64 mm in span and 385.09 mm high, excluding uninstalled fittings and purchased landing gear. These are scene measurements, not physical measurements. Check native project units separately. To resize the complete display, use target dimension divided by its current dimension times 100. Rescaling changes wall thicknesses, hinge diameters, clearances and hardware fit; it does not create a certified RC variant. PRINTING ADVICE — UNTESTED No physical printing, hinge-operation, strength, balance or flight testing has been performed for this publication. Inspect each selected component, thin-wall skin, rib, seam and control bearing in your slicer. Do not replace the supplied lightweight structure with an assumed generic infill recipe. Check the first layer and every intended printed island. Review supports manually to avoid blocking passages or damaging mating surfaces. Disconnected internal structures can be intentional; do not automatically merge or repair every component. Test a representative thin-wall section and a small joint before printing the complete kit. Validate extrusion or exposure, adhesion, cooling, material mass and layer bonding on your own equipment. Clean and dry-fit sections before bonding. Check left/right identity, control direction and canopy-latch fit. The guide calls for completing each horizontal stabiliser with its elevator and associated hardware at the bench before attaching it to the tail. Missing hardware is not supplied by an assembled image. MACHINE-SPECIFIC FILES Preserved G-code has not been executed and is not universal ready-to-run output. Verify firmware dialect, origin, machine size, temperatures, tool selection, extrusion mode and start/end commands before considering any preset. Produce your own validated toolpaths when compatibility is uncertain. FINISH AND IMAGES The proposed aluminium coating and darker canopy are applied to the real assembled surfaces. Photographic presentation uses local-PC rendering and an empty workshop background generated by local AI; the actual model pixels are protected from AI redraw. It is a digital finishing illustration, not a photograph of a tested print. Use primer and thin paint coats on a test sample and protect joints and bearings from paint buildup. RIGHTS AND STATUS Free CC0 distribution follows the account holder's explicit authorization. Necessary source notices and credits are retained; original authorship is not reassigned to the publishing account. Opaque filenames do not make recognizable geometry anonymous. Printing and mechanical or flight performance remain untested. #ScaleModel #ModelAircraft #EDFJet #3DPrinting #ModelMaking #PrintKit #CC0

Tecnología
Sin probar
Material
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Dificultad
Sin especificar
Vista de Twin-Engine Flying Boat — Printable Airframe & Native Project

Twin-Engine Flying Boat — Printable Airframe & Native Project

OVERVIEW A civilian flying-boat airframe with a boat-shaped hull, elevated wing, twin printed nacelles and retractable wingtip floats. The ivory, navy and yellow finish is an illustrated paint scheme on the actual source geometry. Cockpit glazing is painted onto the solid canopy; no windows, motors or propellers have been fabricated. This digital package is not a physically built or flight-certified aircraft. DISPLAY AND INCLUDED RESOURCES The assembled display installs 50 original components with floats retracted. The editable project retains all 54 embedded source meshes: two optional water-rudder halves and two float-support joints are preserved separately, uninstalled. Their purchased wire, couplings and support hardware are absent. Source geometry and required credits remain intact. Nacelles are positioned from original mechanical attachment axes and mating boundaries. The original cowling shells have an illustrative sliding axial fit checked against sampled mesh sections. The supplied guide requires adjustment to the actual purchased propulsion stack; its physical clearance is not certified. Motors, propellers, ESCs, batteries, servos, receiver, wire linkages, clevises, wing braces and fasteners are not supplied as printable geometry. Clear exhibition supports in the images are photographic props excluded from the airframe downloads. The source archive preserves 62 distinct resources plus 54 extracted native STL instances. Its 119 members include these 116 payloads, an English guide, checksums and a technical-role inventory. Payloads comprise 32 standalone STL files, 13 native factory projects, 13 legacy G-code files, two PDFs, one reference image and one INI. The INI is folder metadata, not a slicer preset. Native embedded right-side parts and variants are retained. Authored-coordinate STL and baked printing-scene STL resources are identified separately. Names and dependency references were changed together and checked numerically. Original-slicer GUI compatibility is not certified. Optional old G-code job-name comments were replaced with opaque labels; non-comment executable bytes are unchanged. No machine commands were executed. DIMENSIONS AND SCALE The prepared installed display measures about 1,700.00 mm span × 1,046.74 mm length × 307.64 mm height, excluding optional mechanisms and photographic supports. The source guide describes a semi-scale design and reports 1,702 mm span with floats up, 1,613 mm with floats down and 1,046 mm length. These are not physical-print measurements. The source scale notation is ambiguous; an exact historical reduction ratio is not certified. Files use millimetres. Uniform scaling changes thin walls, holes, clearances and hardware compatibility. The assembled display is not a one-piece print layout. PRINTING — NOT TESTED HERE Read the preserved assembly guide, wire-pattern PDF and per-part native settings. The source author describes thin-wall PLA printing with a 0.4 mm nozzle and 0.25 mm layers on the author's equipment. Those historical settings are not newly tested or universal profiles. Review orientation, wall generation, extrusion width, cooling, bridging, supports and adhesion for your printer. Preserve intentional ribs, shell details, joints and drainage features; inspect toolpaths before replacing per-part settings with generic infill. Legacy G-code is machine-specific historical material. Review printer assumptions, coordinates, temperatures, motion limits and start/end sequences; regenerate suitable toolpaths for your own machine. Print time, mass, strength, waterproofness, stability, mechanical operation and flight performance have not been tested by this publisher. ASSEMBLY AND PAINT Dry-fit and test representative thin-wall pieces first. Use the supplied guides for bonding fuselage, wing, nacelle and tail sections. Numerical boundary and screw-axis checks establish digital relationships, not glue strength, full surface contact or a working mechanism. Hardware must be installed and checked for the actual build. Test compatible preparation, primer and paint on a spare piece; use thin coats and retain native surface details. No watertightness or suitability for water operation is certified by the images. CREDITS, LICENCE AND IMAGES The supplied documentation credits Martin Klöpfer / 3DLabGANG; those credits and notices are preserved. Tomás Piernas is the publishing account, not a claim of original design authorship. Free CC0 distribution follows the rights-holder authorisation provided for this import. Opaque filenames do not anonymise recognisable geometry or remove necessary credits. Images are local-PC digital presentations of the source model with fine enamel materials and local-AI photographic context, not photographs of a physical print. Proposed paint and photographic supports do not expand the printable parts list. The original corpus is unchanged. #FlyingBoat #ScaleModel #3DPrinting #RCAirframe #CC0

Tecnología
Sin probar
Material
—
Dificultad
Sin especificar