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US 2018/0149365 A1Published application
Turbine engine cvc combustion chamber module comprising a pre-combustion chamber
AssigneeSafran Helicopter Engines
InventorsGuillaume TALIERCIO, Christophe Nicolas Henri VIGUIER
Life of this patent
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Abstract
A turbine engine combustion chamber module including at least one constant-volume combustion chamber. The module includes, upstream of the at least one constant-volume combustion chamber, a precombustion chamber capable of producing hot combustion gases that supply the at least one constant-volume combustion chamber so as to allow the ignition thereof.
Claims6
1-7. (canceled)
A turbomachine combustion chamber module, comprising:
- a plurality of constant-volume combustion type combustion chambers distributed about an axis of rotation of the turbomachine,
- upstream of said plurality of constant-volume combustion type combustion chambers, a pre-combustion chamber capable of producing hot combustion gases supplying said plurality of constant-volume combustion type combustion chamber to allow the ignition thereof,
- wherein the pre-combustion chamber supplies hot combustion gases to the constant-volume combustion type combustion chambers through a rotary distributor type system.
Dependencies are inferred from the claim text.