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公开(公告)号：US20180283694A1
公开(公告)日：2018-10-04
申请号：US15472940
申请日：2017-03-29
Applicant: Delavan Inc.
Inventor： Jacob Greenfield , Thomas J. Ocken , Jason A. Ryon
Abstract: An assembly for a turbomachine can include a fuel nozzle and a combustion liner. The fuel nozzle and the combustion liner can be attached to each using a plurality of clip joints such that the combustion liner is longitudinally fixed relative to the fuel nozzle but such that the combustion liner can radially move relative to the fuel nozzle.
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