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Engines & propellers

REAH Propulsion

Match the engine, propeller and aircraft.

Propeller geometry defined by blade sections, an operating map and helical wake lines
Propeller design and performance Software concept visual

Evaluate propulsion as an installed system. Connect engine performance, propeller choices, fuel consumption and heat rejection to the aircraft operating profile.

Concept

Portfolio preview. Portfolio definition builds on REAH's integration work. Engine-design and propeller modules require a scoped development programme.

The engineering question

What changes when the engine becomes an installation?

Choose the propulsion system with the aircraft in view.

01

Engine performance

Compare engine maps, available shaft power, fuel demand and heat rejection across the intended operating conditions.

02

Propeller design & matching

Explore preliminary blade geometry and operating maps. Match diameter, speed and loading to engine capability and aircraft requirements.

03

Engine design programmes

Define engine-type-specific design and analysis tools around a partner's architecture, reference data and validation requirements.

A focused evaluation

From your inputs to a useful engineering review.

Bring
Engine maps, propeller geometry or constraints, installation assumptions and operating profile.
Work towards
A propulsion trade study connecting shaft power, propeller operation, fuel demand and thermal consequences.
Designed for
Engine developers, propulsion engineers and aircraft integrators.
Concept

Evaluation access, supported functions and delivery milestones are agreed for your programme. The portfolio describes product direction; it does not establish general availability.

REAH Propulsion

Bring the case your team needs to solve.

Tell us about the workflow, the available evidence and your next engineering milestone. Let’s define a useful starting point.