Parameter

4.6.1.4 boundary layer ingestion rear end installation

Boundary Layer Ingestion (BLI) rear end installation refers to a propulsion system where an engine or fan is positioned at the rear of an aircraft, designed to ingest the boundary layer airflow that forms along the aircraft's fuselage. By ingesting this typically low-energy airflow, the engine can potentially increase its efficiency, as the energy that would otherwise be lost as drag can be recovered and converted into thrust.
This concept aims to reduce fuel consumption and emissions, particularly in hybrid or electric propulsion systems, by making more efficient use of the airflow around the aircraft.

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
4.6.1.1 over-wing propulsors
4.6.1.2 forward fuselage mounted fans
4.6.1.3 tail cone thruster (e.g. starc-abl)
4.6.1.4 boundary layer ingestion rear end installation
4.6.1.5 in-wing distributed propulsion
4.6.1.6 retrofitting new propulsion systems
4.6.1.7 propulsive fuselage
4.6.2 converting shaft power to thrust
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