Parameter

4.7.3.15 passive load alleviation

Passive load alleviation refers to the use of design features or technologies that reduce the structural loads on an aircraft, without the need for active control systems, often through the use of flexible materials, smart structures or optimized geometries to minimize stress concentrations and improve overall efficiency while maintaining safety and performance.

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
4.7 aircraft structures
4.7.1 aerospace materials & manufacturing
4.7.2 aircraft fuselage
4.7.3 aircraft wings
4.7.3.1 in-wing energy storage
4.7.3.2 morphing structures
4.7.3.3 wing smart structures
4.7.3.4 riblets
4.7.3.5 flow control (passive) on wings
4.7.3.6 high aspect ratio wing
4.7.3.7 foldable winglets
4.7.3.8 foldable wings
4.7.3.9 flexible skin
4.7.3.10 laminar wings
4.7.3.11 prandtl plane
4.7.3.12 truss-braced wing
4.7.3.13 tube and wing optimization
4.7.3.14 wing bio-mimicry
4.7.3.15 passive load alleviation
4.7.3.16 wing structure as conductor
4.7.3.17 light/low mass paint/decals on wings
4.7.3.18 passive canards
4.7.3.19 in-flight cleaning of natural laminar flow leading edges
4.7.4 secondary structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
2
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