The modifications made to the Lancair LIVPT are particularly noteworthy, especially in the realm of air conditioning and pressurization systems. This unique system underwent a year-long evolution during the construction process. Unlike the standard setup that directs engine-heated air into the cabin through an air-to-air intercooler and firewall, the approach in N900WB diverges significantly.
In this aircraft, the system prioritizes conditioning the air before it enters the cabin. Initially, hot bleed air passes through a regulating shut-off valve, controlling the amount “bled” from the engine. The air then travels to the aft section, entering a flow pack commonly found in a Beech Kingair. Outside air is drawn in through a NACA scoop in the vertical fin. The flow pack enhances volume and reduces pressure. Subsequently, the air splits, with one path going through an air-to-air intercooler, and the other bypassing it. The air is then directed to the standard Lancair mix valve, now situated on a custom-built plenum housing the air conditioning evaporator. The mix valve is managed by an RC Allen trim servo. The conditioned air is channeled into the cabin through a 4" duct equipped with an inline turbo fan.
Efficiency is further improved by integrating a recirculation system. The aft pressure bulk was modified to create a duct channeling air back to the plenum with the evaporator, featuring an inline turbo fan to ensure positive airflow. A flapper valve prevents reverse airflow.
For enhanced floor heating, an electric heater was installed in the power pedestal. Notably, all composite parts for the system are custom-made using Styrofoam hand-formed molds and wet carbon layups. This system has proven highly effective, maintaining a comfortable environment at all operating altitudes. Beyond efficient functionality, it has significantly reduced cabin noise compared to the original design. The slowed air and increased volume during pressurization contribute to a quieter cabin experience, making this modified aircraft a tranquil and comfortable ride across various altitudes and speeds.
The standard procedure for installing the Lancair headliner involves directly applying the material to the fuselage shell. To enhance the interior's sculptured appearance, the builder opted to create an inner shell that would offer approximately one inch of relief around the windows. The objective was to achieve this relief without compromising the usable space in the cabin. This was executed by applying three layers of carbon over the exterior of the fuselage shell. Subsequently, hand-shaped form molds were created for each window to shape the window frames. The exterior shell was then transferred to the interior and securely bonded to the window frames, with a mounting system installed at the base of the shell.
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