Fig.1

High temperature components working at high gas temperature

Fig.2

Gas temperature “overheating”

Fig.3

Layered and variable operating condition acquisition technology for component characteristics in complete aircraft engine environment

Fig.4

Crossing from obtaining parameters of component on work line to obtaining complete characteristics of component

Fig.5

Method for solving core flow rate of aircraft engines in complete aircraft engine environment

Fig.6

Control method for multi-zone oil and gas transportation matching vortex core

Fig.7

Relationship between radial temperature distribution of gas and surface temperature of blades

Fig.8

Optimization of radial temperature distribution of gas under multiple failure modes

Fig.9

Influence of rotational inertia load at different speeds on working state of rotor［15］

Fig.10

Schematic diagram of rotor connection instability［14］

Fig.11

Influence of loose outer ring support structure on motion state of intermediate bearings［14］

Fig.12

Strengthening bending stiffness of connecting structure［14］

Fig.13

Monitoring and prediction methods for changes in vibration characteristics and component damages

Fig.14

Dual-channel control architecture

Fig.15

Schematic diagram of fault diagnosis based on engine model

Fig.16

Schematic diagram of fault diagnosis based on control system model

Fig.17

Schematic diagram of DLC coating on inclined plate of plunger fuel pump

Fig.18

Schematic diagram of fuel flow path oil filter

Fig.19

Schematic diagram of STORM technology principle

Fig.20

Schematic diagram of engine control mode switching

Fig.21

Heat transfer and dissipation pathways of aircraft-engine thermal management system

Fig.22

Typical gear pump schematic diagram

Fig.23

Schematic diagram of high flow electric fuel pump

Fig.24

Flow field model of medium in electro-hydraulic servo valve

Fig.25

Fuel oil radiator

Fig.26

Optimization design results of shell and tube fuel oil radiators

Fig.27

Microchannel heat exchanger

Fig.28

Basic ideas for diagnosing engine air circuit faults

Fig.29

Architecture of gas path fault diagnosis method based on model and data fusion

Fig.30

Time frequency analysis results of vibration signals before and after bearing failure

Fig.31

Schematic diagram of lubricating oil system［42］

Fig.32

Main monitoring parameters of lubricating oil system

Fig.33

Structure of life damage monitoring system

Fig.34

Schematic diagram of axisymmetric vector nozzle motion mechanism［50］

Fig.35

Schematic diagram of vector adjustment ring centering mechanism

Fig.36

Schematic diagram of wall temperature simulation results for full loop cooling nozzle

Fig.37

Image of fan with radar imaging

Fig.38

Comparison of RCS values before and after using absorbing waveguide fluid

Fig.39

Traditional afterburner

Fig.40

Suppression effect of radar scattering characteristics in integrated afterburner combustion chamber

Fig.41

Significantly shortened high-temperature core area of binary nozzle tail jet

Fig.42

Wideband radar stealth material