Parameter

4.6.2.1.3 ducted fan

A ducted fan is a type of propulsion system that consists of a fan or propeller enclosed within a duct or shroud. The fan blows air rearward, creating a high-velocity exhaust that produces thrust.

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
4.6.2.1.1 short nacelle
4.6.2.1.2 laminar nacelle
4.6.2.1.3 ducted fan
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
4.6.2.9 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
3
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