Motivation

The aviation sector faces a profound challenge: reducing its environmental footprint while sustaining the performance, safety and economic viability that modern air travel demands. Reaching carbon neutrality by 2050 will require more than efficiency gains – it demands a step change in propulsion technology.

 

HyperMorpH is motivated by two converging opportunities:

 

  1. Liquid hydrogen is emerging as the leading candidate for zero-emission aviation fuel.
  2. The extreme cold of LH₂ creates ideal conditions for high-efficiency electric propulsion, making cryogenically cooled hyperconducting motors both technically attractive and economically viable in a hydrogen-powered future.

 

Advanced fibre-reinforced polymer (FRP) composites are the key enabler: lighter, stronger and more adaptable than metals, they allow this propulsion concept to be both high-performing and structurally feasible.

Core Objectives

01

Cryogenic Hyperconducting Electric Motor

To design and develop a cryogenic, ultra-light, high-power-density hyperconducting electric motor using sustainable thermoplastic FRP composites achieving step-change gains in efficiency, weight reduction and power density.

02

 

Self-Morphing Composite Aerostructures

To design and manufacture self-morphing intake and rotor-tip-casing structures using thermoplastic FRPs, shape-memory solutions and metastructures – optimised for BLI performance across a range of flight conditions.

03

 

Integrated Design Framework and Digital Tools

To develop an AI-supported digital toolkit combining Machine Learning, surrogate modelling, advanced data fusion and uncertainty quantification – enabling concurrent multidisciplinary optimisation of propulsion and aerostructures.

04

 

Lab-Scale Integration and Validation

To validate the integrated hyperconducting motor and morphing aerostructures in a laboratory-scale aft-mounted BLI configuration, demonstrating the synergistic performance of the full propulsion–aerostructure system at TRL 4.

05

Impact, Sustainability and Exploitation

To assess the technical, economic, environmental and societal viability of the developed solutions, and deliver a technology roadmap supporting future exploitation and higher-TRL development beyond the project.

Methodology

HyperMorpH follows a concurrent, multidisciplinary methodology that integrates materials development, digital simulation and experimental validation within a single coherent workflow. Work progresses in two phases: conceptual design and specification in the first 18 months, followed by detailed design, manufacturing, demonstration and validation through to project end.

 

The architecture of the project reflects its systemic ambition: rather than advancing individual components in isolation, HyperMorpH deliberately co-develops the motor, morphing aerostructures and digital tools in parallel, with shared interfaces and cross-WP feedback loops to ensure genuine integration.

 

Work Package Overview

  • WP1 / WP13 Management and Coordination (Phases 1 & 2)
  • WP2 / WP14 Communication, Dissemination and Exploitation (Phases 1 & 2)
  • WP3 Aircraft Architecture and System Requirements
  • WP4 / WP5 Hyperconducting Cryogenic Electric Motor: Conceptual & Detailed Design and Demonstration
  • WP6 / WP7 Self-Morphing Composite Aerostructures: Conceptual & Detailed Design and Demonstration
  • WP8 / WP9 Integrated BLI Propulsor–Aerostructures: System Design and Performance Assessment
  • WP10 Surrogate and Data-Driven Modelling of the Cyber-Physical System
  • WP11 Lab-Scale Validation of BLI Propulsor–Aerostructure Integration
  • WP12 Sustainability and Scalability Assessment

Find out more about Expected outcomes