发明名称 SYSTEM AND APPARATUS FOR COMBUSTION SWIRLER ANTI-ROTATION
摘要 A swirler comprising an anti-rotation feature is provided. The swirler may be installed on a combustor within a gas turbine engine. The swirler may comprise a generally cylindrical profile. In this regard, the swirler may be configured to provide a generally uniform profile within the combustor. The swirler may comprise a floating collar with an anti-rotation feature. The swirler may also include a collar end plate that defines a slot that at least partially encloses the anti-rotation feature and minimizes rotational movement of the floating collar.
申请公布号 US2016223193(A1) 申请公布日期 2016.08.04
申请号 US201615096624 申请日期 2016.04.12
申请人 United Technologies Corporation 发明人 EASTWOOD JONATHAN J.;JAUSE JONATHAN M.
分类号 F23D11/38;F23R3/28 主分类号 F23D11/38
代理机构 代理人
主权项 1. A combustor, comprising: a fuel injector; a combustion chamber configured to receive fuel from the fuel injector; and a swirler comprising a floating collar comprising an anti-rotation feature and a collar end plate defining a notch, wherein the swirler is installable on the fuel injector, and wherein the swirler is configured to deliver atomized fuel to the combustion chamber.
地址 Hartford CT US