SERVICE TUBE FOR TURBINE ENGINE

An apparatus and method of reducing operating temperatures of a gas turbine engine (10), exposed to a service tube assembly (84) by utilizing a skirt (98) and radially outer mount (90). The reductionin temperature exposure minimizes temperatures of the service tube during engine operation to reduce...

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Bibliographic Details
Main Authors JAKOMIN JOHN MARTIN, RAJAGOPALAN VINODH, AGARA KARTHIK GOPAL RAO, FEMIA STEVEN PAUL
Format Patent
LanguageChinese
English
Published 28.04.2020
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:An apparatus and method of reducing operating temperatures of a gas turbine engine (10), exposed to a service tube assembly (84) by utilizing a skirt (98) and radially outer mount (90). The reductionin temperature exposure minimizes temperatures of the service tube during engine operation to reduce the incidence of oil coking or varnish. 一种设备及方法，其通过使用裙部(98)和径向外安装件(90)来降低暴露于保养管组件(84)的燃气涡轮发动机(10)的操作温度。暴露温度的降低最小化保养管组件(84)在发动机(10)操作期间的温度以减小油焦化或覆膜的发生率。
Bibliography:Application Number: CN201911005252