公开(公告)号：US4226088A

公开(公告)日：1980-10-07

申请号：US880109

申请日：1978-02-22

申请人： Satoshi Tsukahara ,  Isao Sato ,  Yoshihiro Uchiyama ,  Masanobu Kusaba

发明人： Satoshi Tsukahara ,  Isao Sato ,  Yoshihiro Uchiyama ,  Masanobu Kusaba

IPC分类号： F23R3/12 ,  F23C99/00 ,  F23R3/04 ,  F23R3/54 ,  F02C7/22

CPC分类号： F23R3/04 ,  F23R3/54

摘要： A combustor for gas turbines includes a stepped cylindrical tube defining first, second and main combustion spaces. Primary air supply openings are formed in the tube portion defining the first combustion space, secondary air supply openings in the tube portion defining the second combustion space, and diluting air supply openings in the tube portion defining the main combustion space. To achieve effective cooling of the combustion gas within the combustion chamber, particularly in the second combustion space, and especially in the central portion thereof, and at the same time to maintain a stable combustion, the tube is formed so, and the cross-sectional areas of the primary, secondary and diluting air supply openings are dimensioned so, that 25 to 32% of the total amount of air supplied to the combustion chamber are used as primary air in the first combustion space, 38 to 50% as secondary air in the second combustion space, and less than 30% as diluting air in the main combustion space.

摘要翻译： 用于燃气轮机的燃烧器包括限定第一，第二和主燃烧空间的阶梯形圆柱形管。 主要空气供应开口形成在限定第一燃烧空间的管部分中，限定第二燃烧空间的管部分中的二次空气供应开口，以及限定主燃烧空间的管部分中的稀释空气供应开口。 为了有效地冷却燃烧室内的燃烧气体，特别是在第二燃烧空间，特别是在其中心部分，并且同时保持燃烧稳定的燃烧气体，管形成为这样，并且横截面 初级，次级和稀释空气供应开口的区域尺寸使得供应到燃烧室的空气总量的25％至32％用作第一燃烧空间中的一次空气，作为二次空气中的38％至50％ 第二燃烧空间，并且在主燃烧空间中稀释空气小于30％。