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公开(公告)号：US5398495A
公开(公告)日：1995-03-21
申请号：US228367
申请日：1994-04-15
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。
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公开(公告)号：US5499499A
公开(公告)日：1996-03-19
申请号：US316338
申请日：1994-09-30
CPC分类号： F23R3/002 , F05B2260/201 , Y02T50/675
摘要： A cladded combustion chamber construction is disclosed in which the cladd tiles can be assembled and replaced without the necessity of disassembling the structural wall of the combustion chamber. The combustion chamber has a generally cylindrical wall with external and internal surfaces bounding the combustion chamber and has a plurality of cladding tiles located on one of the external and internal surfaces of the wall. To attach the cladding tiles to the combustion chamber structure, a plurality of channel shaped attaching devices are utilized extending in a generally circumferential direction around the wall of the combustion chamber and having a portion extending generally parallel to the wall, but spaced from the wall. The portion extending parallel to the wall of the combustion chamber has a circumferentially extending cut out portion whose circumferential length is slightly greater than the width of a cladding tile. The channel shaped attaching devices are spaced axially along the wall of the combustion chamber and are spaced apart a distance slightly greater than a length of a cladding tile. In order to attach the cladding tile to the combustion chamber wall, it is merely necessary to place one end of the tile in one of the channel members and to pass the other end of the tile through the circumferential cut out of the other attaching channel.
摘要翻译： 公开了一种包覆燃烧室结构，其中可以组装和更换包覆砖，而不需要拆卸燃烧室的结构壁。 燃烧室具有大致圆柱形的壁，其外表面和内表面包围燃烧室，并且具有位于壁的外表面和内表面中的一个上的多个包层砖。 为了将包层瓦片附接到燃烧室结构，利用多个通道形状的附接装置，其围绕燃烧室的壁沿大致圆周方向延伸，并具有大致平行于壁延伸但与壁间隔开的部分。 平行于燃烧室的壁延伸的部分具有周向延伸的切口部分，其圆周长度略大于覆盖层的宽度。 通道形安装装置沿着燃烧室的壁轴向间隔开，间隔开一个略大于包覆砖长度的距离。 为了将包层瓦片附接到燃烧室壁，仅需要将瓦片的一端放置在通道构件中的一个中，并使瓦片的另一端穿过另一个附接通道的圆周切口。
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3.发明授权Gas turbine combustion chamber with adjustable primary oxidizer intake passageways 失效燃气轮机燃烧室，可调一次氧化剂进气通道
公开(公告)号：US5317863A
公开(公告)日：1994-06-07
申请号：US57492
申请日：1993-05-06
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。
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