Nozzle for an engine, and engine
The use of a displaceable sliding body in the fuel line, utilizing pressure differences, addresses the weight challenge of traditional valves by offering a lightweight and efficient fuel flow mechanism for aviation engines.
Patent Information
- Authority / Receiving Office
- US · United States
- Patent Type
- Applications(United States)
- Current Assignee / Owner
- ROLLS ROYCE DEUT LTD & CO KG
- Filing Date
- 2025-11-05
- Publication Date
- 2026-06-18
AI Technical Summary
Existing nozzle designs for aviation engines with pressure-jet atomizers face challenges in providing weight-optimized mechanisms for connecting and disconnecting fuel mass flow due to the high weight of traditional valve systems.
A displaceable sliding body is used in the second fuel line, which blocks or opens the fuel line fluid-tightly based on pressure differences within the fuel and combustion chamber, utilizing a hydro-pneumatic adjustment mechanism without active control, allowing passive displacement for weight optimization.
This design provides a simple and reliable mechanism for connecting and disconnecting fuel flow, reducing weight and maintaining efficient fuel supply across varying engine power conditions.
Smart Images

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