SKT UAS-OPH Optionally Piloted Helicopter
Full Envelope Flight Control
• SATCOM & LOSCOM Management
• Payload & Data Management
• Transponder and
ATC Radio Management
• Electrical System Management
(alternators, batteries, lighting, etc.)
• Engine & Fuel System Management
• Empty Weight: 350 kg
• MTOW: 700 kg
• Payload: 350 kg
• Endurance: Up to 8 hours
• Max. Speed: 204 km/h
• Cruising Speed: 166 km/h
High fidelity HILS
Pilot and payload
operator training
Mission optimisation /
simulation
Milling:
Turning:
EDM Electrical Errosion:
We use following equippment for welding:
• Laser Marking machines x 2
• Ink Jet Printer Gun
• CNC Engraving on Milling Machines
• Letter Cutter and Paint
• Wenzel Smart CMM 500x450x400mm
We use following equipment for welding:
• Kemppi Mastertig 2300 AC/DC for aluminium, stainless steel and steel TIG
• Kemppi Mastertig 3000 for stainless steel and steel TIG
• Kemppi Fastmig M420 for aluminium, stainless steel and steel MIG
• Varstroj 1405 for steel MAG
Konelek has successfully finished design and stress analysis of the complete general aviation aircraft structures. In the area of the civil and regional aircraft we have been part of the larger teams working on projects such as Airbus A350-1000 and Bombardier C-Series.
Conceptual and detail design of metallic, composite and hybrid structures using state of the art CAD, PDM and PLM tools. Static (linear and non-linear) analysis using hand calcs and FEM methods (GFEM, IFEM, DFEM). Damage Tolerance & Durability Analysis, Residual Strength Analysis, Fail Safe Analysis.
.In the area of systems installation we have experience in systems like: Electrical Systems Installation, Hydraulic Systems Installation, Bleed Air, Fuel Systems, Pitot Systems, Piston Engines. Members of our team gained experience in designing systems installation on brand new general aviation and civil aircraft and on the passenger to freighter conversions.
Konelek has experience in landing gear design including: general lay-out, attachment concepts, kinematics and detailed design studies, gear positioning and tyre sizing by checking several constraints (balance and stability, door clearance…), weight assessment and variation versus major drivers (design weight, attachment, kinematics), state of the art knowledge of materials, coatings, processes (Custom 465, Forcemate cold working design, Toughmet bushes design), fusible structure design for crashworthiness and fuel tank intact retention.
We also have experience in ground loads calculation and reporting for the different combinations of landing gear, aircraft and manoeuvre with high level of accuracy, rigid and flexible multibody formulation, Geometry and mass and stiffness and damping information, advanced tyre modelling.
Definition and design of the drop tests of landing gears and complete aircraft.
We can offer CAD design of Aerodynamic surfaces and structures and aero dynamic analysis by conventional and CFD tools including airfoil design and selection. Additionally we offer flow and thermal analysis by computational tools and hand calc methods.
What allows us to have good success in creating cost effective and working design is our experience in manufacturing gained in our tool manufacturing shop floor. We have experience in: Aircraft assembly tooling design (up to the size of the complete final assembly lines), Machining fixture design, Lifting slings, GSE ground support equipment, drilling and fettling tools, laser alignment tools, bootstraps, lifting cradles, zero-stress jacking tools subassembly tooling, layup moulds, etc.
Konelek also offers CNC programming and verification services. This capability covers high speed, multi-axis machining techniques, and machine tools, from machining cells to long bed multi-axis / multi-spindle machines.
We are involved in state of the art research in fly by wireless aeronautical technologies. We have
state of the art experience of implementation of more electric aircraft technologies like electrical braking systems.
We provide dynamic and kinematic analysis that can evaluate the behaviour of mechanical systems such as landing gear, control surfaces, doors, overhead bins, etc., prior to the availability of a physical prototype.
Titanium Compressor, finished part, soon to become the part of a Jet Engine.
Titanium Compressor, finished part, soon to become the part of a Jet Engine.
Installation of Nozzle assembly into Oil Feed Pipe
Installation of Oil Feed Pipe into Coalescence Chamber
Helicopter Gearbox Dummy Plate fresh from our workshop.
Safety Collars
Safety Collar allows safe replacement of the Landing Gears and other maintenance tasks. We make some of them.
Safety Collar is safety critical maintenance item, is made of the quality materials and load tested to insure prevention of the unintentional landing gear door closing.
Check out this great video
Check out this great video
Check out this great video
Check out this great video
Check out this great video
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