公开(公告)号：US5398495A

公开(公告)日：1995-03-21

申请号：US228367

申请日：1994-04-15

申请人： Patrick S. A. Ciccia ,  Eric J. S. Lancelot

发明人： Patrick S. A. Ciccia ,  Eric J. S. Lancelot

IPC分类号： F02C9/26 ,  F02C7/057 ,  F23R3/10 ,  F23R3/12 ,  F23R3/26 ,  F23R3/28 ,  F23R3/46 ,  F02C9/00

CPC分类号： F23R3/26 ,  F05B2250/411

摘要： A generally annular combustion chamber for a gas turbine engine is disclosed having fuel injector assemblies, each with an oxidizer swirler, extending through an upstream end wall of the combustion chamber and control means connected to the control diaphragms of the oxidizer swirlers in order to move the control diaphragms between maximum and minimum flow positions. The upstream end wall of the combustion chamber defines complementary oxidizer intake orifices which have movable closure plates to selectively open or close the complementary oxidizer intake orifices. A mechanical linkage connects the closure plates to the control diaphragm of an adjacent air swirler such that, when the control diaphragms are in their maximum flow positions, the closure plates close the complementary oxidizer intake orifices, and when the control diaphragms are in their minimum flow positions, the closure plates are moved such that the complementary oxidizer intake orifices are fully open.

摘要翻译： 公开了一种用于燃气涡轮发动机的大体上环形的燃烧室，其具有燃料喷射器组件，每个燃料喷射器组件具有延伸通过燃烧室的上游端壁的氧化剂旋流器，以及连接到氧化器旋流器的控制膜片的控制装置， 在最大和最小流量位置之间控制隔膜。 燃烧室的上游端壁限定互补的氧化剂吸入口，其具有可移动的封闭板，以选择性地打开或关闭互补的氧化剂吸入口。 机械连杆将封闭板连接到相邻空气旋流器的控制膜片，使得当控制膜片处于其最大流动位置时，封闭板关闭互补氧化剂进气孔，并且当控制膜片处于其最小流量 位置，移动闭合板使得互补氧化剂吸入口完全打开。

公开(公告)号：US5317863A

公开(公告)日：1994-06-07

申请号：US57492

申请日：1993-05-06

申请人： Patrick, S. A. Ciccia ,  Patrice A. Commaret ,  Eric J. S. Lancelot

发明人： Patrick, S. A. Ciccia ,  Patrice A. Commaret ,  Eric J. S. Lancelot

IPC分类号： F02C3/30 ,  F23R3/04 ,  F23R3/26 ,  F23R3/28 ,  F02C9/00

CPC分类号： F23R3/04 ,  F23R3/26 ,  F05B2250/41 ,  F05B2250/411

摘要： A combustion chamber structure wherein the combustion chamber extends around a central, longitudinal axis and has primary oxidizer intake passageways whose positions along the central axis relative to an end of the combustion chamber are adjustable depending upon the operating conditions of the gas turbine engine. By controlling axial positions of the primary oxidizer intake passageways, the dwell time of the combustion gases and primary oxidizer inside the combustion zone of the chamber may also be controlled so as to increase the stability of the combustion, while at the same time minimizing the polluting emissions. The invention also encompasses the concept of adjusting the cross-sectional area of the primary oxidizer intake passageways as their positions along the central axis are adjusted. This enables a more accurate control of the volume of the primary oxidizer flow in addition to controlling the location of the flow.

摘要翻译： 一种燃烧室结构，其中所述燃烧室围绕中心纵向轴线延伸并且具有主要氧化剂进气通道，所述主氧化器进气通道相对于所述燃烧室的端部沿着所述中心轴线的位置可根据所述燃气涡轮发动机的操作条件而调节。 通过控制主氧化剂进气通道的轴向位置，也可以控制燃烧气体和主氧化剂在室内燃烧区内的停留时间，以增加燃烧的稳定性，同时使污染最小化 排放。 本发明还包括调整主氧化剂进气通道的横截面面积的概念，因为它们沿着中心轴线的位置被调节。 除了控制流动的位置之外，这使得能够更准确地控制主氧化剂流的体积。