TOGETHER FOR TURBOMACHINE AND ASSOCIATED TURBOMACHINE

FR3146493B1Active Publication Date: 2025-02-28SAFRAN AIRCRAFT ENGINES SAS
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Patent Information

Application Number
FR2023002185
Authority / Receiving Office
FR · FR
Patent Type
Patents
Current Assignee / Owner
Filing Date
2023-03-09
Publication Date
2025-02-28
Estimated Expiration
2043-03-09
Patent Text Reader

Abstract

Assembly for turbomachine comprising: - a fuel injector including an injector head (40) extending along a central axis (70), and - an injection system including a mixing bowl (50) and a ring (72) rotating about said central axis, the assembly further comprising means for supplying air (64) inside the bowl, said ring (72) being shaped to reduce or increase by rotation an air passage cross-section in said air supply means (64), the assembly comprising at least one controllable displacement device for said injector configured to move the injector head (40) along the central axis (70) between a first position and a second position, the assembly being configured to change the angular position of said ring (72) relative to the air supply means (64) when the injector head (40) is moved between the first position and the second position. Figure from the summary: Figure 17A
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