DESIGN AND CALCULATION OF THE AIR CONDITIONING SYSTEM FOR A SMALL TRANSPORT AIRCRAFT WITH A TAKE-OFF WEIGHT OF UP TO 2 000 KG

Abstract

This article describes the air conditioning system as one of the most important systems of the aircraft. It has a significant impact on the comfort of the passengers, which is nowadays very important. The article describes the main types of air conditioning systems used today and a brief analysis of their components. It also describes how to select and design an appropriate air-conditioning system and air distribution system for an aircraft with a take-off weight of up to 2,000 kg.