Analysis of non-standard MiG-29 engine start procedures

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.

Submit your paper

For Authors

Archive

Send by email

The hybrid concept of turboshaft engine working according to Humphrey cycle dedicated to variety power demand – CFD analysis

Experimental determination of compressor map of the DGEN 380 engine compressor using the WESTT CS/BV turbine engine simulator

The assessment of the technical condition of the bearing seals of the rotor shaft in a turbine helicopter engine based on the PM content in the exhaust gases

Microstructure analysis in the creep process of a gas turbine blade of the turbine engine

Indexes

Keywords index

Topics index

Authors index