Parameter

4.6.2.8 gas turbine technology

An internal combustion engine system that converts fuel energy into mechanical power through three main components: a compressor (which draws in and pressurizes air), a combustion system (which mixes fuel with compressed air and burns it at temperatures over 1100°C), and a turbine (which extracts energy from the hot gas to drive the compressor and generate mechanical work).
Gas turbines are used widely in power generation (achieving 33–44% efficiency in simple cycle, over 60% in combined cycle), aviation (jet engines), and marine/industrial propulsion.
Modern gas turbines can achieve inlet temperatures up to 1400°C using advanced cooling and materials, and combined-cycle plants with heat recovery can reach overall efficiencies approaching 80%

Hierarchy

4 technological themes
4.1 active aircraft control
4.2 data transfer technologies
4.3 energy carriers
4.4 net zero technologies
4.5 operational technologies
4.6 aircraft propulsion
4.6.1 propulsor integration on airframe
4.6.2 converting shaft power to thrust
4.6.2.1 advanced nacelle
4.6.2.2 open rotor
4.6.2.3 rim-driven fan
4.6.2.4 tip-drive fan
4.6.2.5 variable pitch fan blades
4.6.2.6 multi-engine single propulsor
4.6.2.7 composite fan blades & containment
4.6.2.8 gas turbine technology
4.6.2.8.1 ultra-high bypass
4.6.2.8.2 ultra-high specific power
4.6.2.8.3 high speed
4.6.2.9 composite cycle engine
4.6.2.10 high speed electric propulsion
4.6.2.11 electric boosting of combustion engines
4.6.2.12 direct drive technology
4.6.2.13 gas turbine + fuel cell (sofc)
4.6.3 converting fuel to shaft power
4.6.4 non-combustion based engine integration
4.6.5 other propulsion technologies
4.7 aircraft structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
1
Optimising together
N/A
Stripping down
N/A
Tech for you
N/A
Mad max

Milestone Timehorizon

PESTEL categories

Current

Short term

Medium term

Long term

Little to many relations with other Milestones