专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US3702174A Fluid distributors and thrusters 失效
标题翻译：流体分配器和THRUSTERS
公开(公告)号：US3702174A
公开(公告)日：1972-11-07
申请号：US3702174D
申请日：1971-02-18
申请人： AEROJET GENERAL CO
发明人： HANKINS RONALD A , CULVER DONALD W , SCAMMON HARRISON B JR
IPC分类号： F02K9/52 , F02K9/58 , F02K9/68 , B63H11/00 , B64D33/04
CPC分类号： F02K9/58 , F02K9/52 , F02K9/68
摘要： ACCORDING TO THE PRESENT DISCLOSURE, A FLUID DISTRIBUTOR COMPRISES A STACK OF A PLURALITY OF WAFERS. INLET APERTURES ARE PROVIDED THROUGH INLET WAFERS AND ARE IN FLUID COMMUNICATION WITH DISTRIBUTION APERTURES IN A DISTRIBUTION WAFER OUTLET APERTURES ARE PROVIDED IN FLUID COMMUNICATION WITH THE DISTRIBUTION WAFERS. PREFERABLY, METERING APERTURES AND TRANSFER APERTURES ARE PROVIDED IN SERIAL FLUID COMMUNICATION WITH SAID DISTRIBUTION APERTURES BETWEEN THE INLET AND OUTLET APERTURES. A THRUSTER ACCORDING TO THIS DISCLOSURE MAY INCLUDE A FIRST FLUID DISTRIBUTOR FOR RADIALLY INJECTING MONOPROPELLANT INTO A RADIAL CATALYST PACK, OR A SECOND FLUID DISTRIBUTOR FOR AXIALLY INJECTING MONOPROPELLANT INTO AN AXIAL CATALYST PACK.

2. 发明授权

US3922849A Injector for gas turbine combustor 失效
标题翻译：燃气轮机燃油机喷油器
公开(公告)号：US3922849A
公开(公告)日：1975-12-02
申请号：US40444573
申请日：1973-10-09
申请人： AEROJET GENERAL CO
发明人： KORS DAVID L , CULVER DONALD W
IPC分类号： F02C7/08 , F23R3/30 , F02C7/10 , B05B1/24 , F02G3/00
CPC分类号： F23R3/30 , F02C7/08 , F02G2250/03
摘要： Liquid fuel is introduced into thin, elongate vanes disposed in the airstream to a fuel combustor of a turbine or heat exchanger. An air heater is positioned upstream of the vanes and heated from heat energy withdrawn from the turbine exhaust gas. The vanes include thin and relatively wide fuel passages which terminate in a plurality of fuel discharge openings facing the turbine combustor. Liquid fuel is centrally introduced into the passages and flows towards the discharge openings. The heated air raises the temperature of the vanes which in turn raises the liquid fuel temperature. The relatively large fuel passage surface area-tovolume ratio assures an intimate and quick heat transfer so that the liquid fuel evaporates before it exits from the discharge openings to thereby effect a homogeneous intermixing of the vaporized fuel and the air prior to combustion.
摘要翻译：将液体燃料引入到设置在空气流中的薄的细长叶片中，到达涡轮机或热交换器的燃料燃烧器。空气加热器位于叶片的上游并且从从涡轮废气排出的热能加热。叶片包括薄且相对宽的燃料通道，其终止于面对涡轮机燃烧器的多个燃料排放开口。液体燃料被中心地引入通道并流向排放口。加热的空气升高叶片的温度，这又升高液体燃料温度。相对较大的燃料通道表面积与体积比确保了紧密和快速的热传递，使得液体燃料在从排出口离开之前蒸发，从而在燃烧之前实现蒸发的燃料和空气的均匀混合。

3. 发明授权

US3608833A Fluid distributors and thrusters 失效
标题翻译：流体分配器和THRUSTERS
公开(公告)号：US3608833A
公开(公告)日：1971-09-28
申请号：US3608833D
申请日：1969-10-13
申请人： AEROJET GENERAL CO
发明人： HANKINS RONALD A , CULVER DONALD W , SCAMMON HARRISON B JR
IPC分类号： F02K9/52 , F02K9/58 , B05B1/14 , F23D13/44
CPC分类号： F02K9/58 , F02K9/52
摘要： According to the present disclosure, a fluid distributor comprises a stack of a plurality of wafers. Inlet apertures are provided through inlet wafers and are in fluid communication with distribution apertures in a distribution wafer. Outlet apertures are provided in fluid communication with the distribution wafers. Preferably, metering apertures and transfer apertures are provided in serial fluid communication with said distribution apertures between the inlet and outlet apertures. A thruster according to this disclosure may include a first fluid distributor for radially injecting monopropellant into a radial catalyst pack, or a second fluid distributor for axially injecting monopropellant into an axial catalyst pack.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式