RU94952U1 - PLANE WITH AUXILIARY MAGAKYAN ENGINE - Google Patents

Abstract

 Aircraft consisting of a cockpit, operating compartment, passenger or cargo compartment, wings, fuselage, engine, stabilizer, keel, technical compartment, main landing gear, front landing gear, characterized in that it further comprises an auxiliary engine mounted in the aerodynamic fairing and working autonomously from the main system of the aircraft and driven by the energy of a powerful oncoming air flow during the flight of the aircraft.

Description

The utility model relates to the aviation industry.

Prototype: passenger, transport, military aircraft.

An analogue is the AN-26 military transport aircraft with two main turboprop engines and an auxiliary jet engine / Internet, http // desantnik.com.ua / type-air /.

The technical task is to create a more advanced aircraft.

The essence of the utility model - the problem is solved by the fact that the aircraft has an auxiliary engine, but unlike the analogue which has an auxiliary engine, it has a jet engine that operates autonomously from the main system of the aircraft and is driven by the energy of a powerful oncoming air stream during flight.

In statics, a utility model consists of: a cockpit - Fig. 1 position 1, a working compartment - Fig. 1 pos. 2, passenger or cargo salons - Fig. 1 pos. 3, wings - Fig. 1 pos. 4, the fuselage - Figure 1, position 5, the engine - Figure 1 position 6, the stabilizer - Figure 1 position 7, the keel - Figure 1 position 8, the auxiliary engine - Figure 1 position 9 and Figure 2 position 1 , technical compartment - Fig.1 pos.10, the main landing gear - Fig.1 pos.11, the front landing gear - Fig.1 pos.12.

The utility model: during takeoff, flight, landing, the main engines operate - Figure 1, position 6, driven by energy - obtained from the combustion of jet fuel.

The auxiliary engine - Fig. 1 pos. 9 and Fig. 2 pos. 1, made in the form of a well streamlined body, placed in an aerodynamic cowling - Fig. 2 pos. 6, works from a natural resource - a powerful oncoming air flow, pressing on the blades - Figure 2 pos.4 and rotating them.

The auxiliary engine - Fig. 1 pos. 9 and Fig. 2 pos. 1 is located between two main engines - Fig. 1 pos. 6 and their aerodynamic flows, and when the aircraft is flying creates its third aerodynamic blades with its rotating blades - Fig. 2 pos. 4 flow, which improves the overall aerodynamic characteristics of the aircraft and, in addition, the auxiliary engine - Fig. 1 pos. 9 and Fig. 2 pos. 1, having on the shaft - Fig. 2 pos. 5 rotor - Fig. 2 pos. 3, placed in the stator - Fig.2 pos.2, can serve as an electric power source.

Technical result: the presence of an auxiliary engine will improve the aerodynamic characteristics of the aircraft during flight.

Claims (1)

Aircraft consisting of a cockpit, operating compartment, passenger or cargo compartment, wings, fuselage, engine, stabilizer, keel, technical compartment, main landing gear, front landing gear, characterized in that it further comprises an auxiliary engine mounted in the aerodynamic fairing and working autonomously from the main system of the aircraft and driven by the energy of a powerful oncoming air flow during flight.