Abstract

The paper describes alternative start procedures if regular MiG-29 engine start procedures are disturbed. The work presents ground engine start procedures with a turbine starter and an automatic start of both engines. A procedure algorithm has been presented in case malfunctions are detected depending on the level of the malfunction complexity. Example results have been included that come from the flight operating parameters recorder showing the versatility of events that may occur when starting the MiG-29 engines.

Highlights

  • The advancement of aviation, construed as crossing one of the uncrossable boundaries for humans, initially continued in two independent directions

  • The components of the RD-33 engine are [3]: – low pressure rotor (LPR) with an axial four-stage fan and an air-cooled single stage axial turbine, – high pressure rotor (HPR) with an axial nine-stage compressor and an air-cooled single stage turbine, – annular combustor with fuel injectors located in the general collector, – afterburner chamber with flow mixing upstream of the afterburner, – ultrasound outlet nozzle with smooth adjustment of critical and outlet flow, – aggregate transfer case from the high pressure rotor, 3

  • The authors presented the applicable methodology used in case of a MiG-29 aircraft malfunction

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Summary

Introduction

The advancement of aviation, construed as crossing one of the uncrossable boundaries for humans, initially continued in two independent directions. The other direction were aircraft capable of flying thanks to aerodynamic force generated by dynamic interaction of air and stationary or movable airfoils. The first successful attempt to fly with an aircraft lighter than air took place already in the XVIII century. Aerostats and their hybrids – statodynes were a great success of aviation until the WWI when the progress in aviation weapons slowed their development because they were more susceptible to gunfire than aerodynes. Among aircraft operating because of dynamic interaction with air, the greatest advancement took place in propelled aerodynes: airplanes, rotorcrafts and ornithopetrs. Advancement of propulsion systems forces a development of new type of engines – starting from piston and jet engines ending with turbojet and turboprops.

Wprowadzenie
Analysis of malfunction states
Analiza stanów awaryjnych
Description of the research object
Procedura rozruchu silników
Engine start procedure
Analysis of malfunction states of the MiG-29 engines
Analiza stanów awaryjnych zespołu napędowego MiG-29
Conclusions
Podsumowanie

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