CA1113009A - Turbine de puissance a gaz et moyen de refroidissement - Google Patents

Turbine de puissance a gaz et moyen de refroidissement

Info

Publication number
CA1113009A
CA1113009A CA310,429A CA310429A CA1113009A CA 1113009 A CA1113009 A CA 1113009A CA 310429 A CA310429 A CA 310429A CA 1113009 A CA1113009 A CA 1113009A
Authority
CA
Canada
Prior art keywords
turbine
engine
blade
coolant
heat exchanger
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA310,429A
Other languages
English (en)
Inventor
Robert J. Corsmeier
James P. Rauf
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to CA310,429A priority Critical patent/CA1113009A/fr
Application granted granted Critical
Publication of CA1113009A publication Critical patent/CA1113009A/fr
Expired legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
CA310,429A 1978-08-31 1978-08-31 Turbine de puissance a gaz et moyen de refroidissement Expired CA1113009A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA310,429A CA1113009A (fr) 1978-08-31 1978-08-31 Turbine de puissance a gaz et moyen de refroidissement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA310,429A CA1113009A (fr) 1978-08-31 1978-08-31 Turbine de puissance a gaz et moyen de refroidissement

Publications (1)

Publication Number Publication Date
CA1113009A true CA1113009A (fr) 1981-11-24

Family

ID=4112252

Family Applications (1)

Application Number Title Priority Date Filing Date
CA310,429A Expired CA1113009A (fr) 1978-08-31 1978-08-31 Turbine de puissance a gaz et moyen de refroidissement

Country Status (1)

Country Link
CA (1) CA1113009A (fr)

Similar Documents

Publication Publication Date Title
US4190398A (en) Gas turbine engine and means for cooling same
US4136516A (en) Gas turbine with secondary cooling means
US4137705A (en) Cooling air cooler for a gas turbine engine
US9765694B2 (en) Gas turbine engine heat exchangers and methods of assembling the same
US8998572B2 (en) Blade outer air seal for a gas turbine engine
US4861228A (en) Variable stator vane assembly
US4914904A (en) Oil cooler for fan jet engines
US10883382B2 (en) Outlet guide vane for aircraft turbomachine, comprising a lubricant cooling passage equipped with flow disturbance studs
US10697312B2 (en) Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function
US11143045B2 (en) Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct
US4118136A (en) Apparatus for attaching tubing to a rotating disk
WO2002038938A1 (fr) Reacteur a turbine a gaz avec derivation et procede de refroidissement pour fluide caloporteur
US10830076B2 (en) Outlet guide vane for turbomachine, made from several parts assembled together by attachment means outside the flow stream
EP0909878B1 (fr) Turbine à gaz
JP4527824B2 (ja) タービンロータの軸受用冷却系
EP3974622B1 (fr) Échangeur de chaleur rotatif
US3532443A (en) Engine lubrication
US2801518A (en) Gas turbine
US10683760B2 (en) Gas turbine engine component platform cooling
CA1113009A (fr) Turbine de puissance a gaz et moyen de refroidissement
CA1117025A (fr) Turbine a gaz a refroidissement secondaire
US12497999B2 (en) Bearing lubricant drain
EP3901418A1 (fr) Poches de refroidissement à face accouplée et à languette d'étanchéité
CN120693447A (zh) 用于引导轴并对气体发生器的轴承进行冷却的装置
Van Buijtenen et al. Mechanical Design of a High Efficiency 7.5 MW (10,000 HP) Gas Turbine

Legal Events

Date Code Title Description
MKEX Expiry