KR980002642A - Gas Turbine Engine Lubrication System - Google Patents

Gas Turbine Engine Lubrication System Download PDF

Info

Publication number
KR980002642A
KR980002642A KR1019960022006A KR19960022006A KR980002642A KR 980002642 A KR980002642 A KR 980002642A KR 1019960022006 A KR1019960022006 A KR 1019960022006A KR 19960022006 A KR19960022006 A KR 19960022006A KR 980002642 A KR980002642 A KR 980002642A
Authority
KR
South Korea
Prior art keywords
main
pipe
lubricating oil
starting
storage tank
Prior art date
Application number
KR1019960022006A
Other languages
Korean (ko)
Other versions
KR100296336B1 (en
Inventor
권우성
Original Assignee
이대원
삼성항공산업 주식회사
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 이대원, 삼성항공산업 주식회사 filed Critical 이대원
Priority to KR1019960022006A priority Critical patent/KR100296336B1/en
Publication of KR980002642A publication Critical patent/KR980002642A/en
Application granted granted Critical
Publication of KR100296336B1 publication Critical patent/KR100296336B1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06—Arrangements of bearings; Lubricating

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

윤활유를 저장하는 저장탱크(10)와, 저장탱크(10)에 시동흡임관(11)을 통하여 연결되고 시동모터에 의해 작동되는 시동윤활펌프(12)와, 저장탱크(10)에 주흡입관(15)을 통하여 연결되고 기어박스(2)의 축(18)에 연결되어 작동하는 주윤활펌프(16)와, 시동윤활펌프(12)와 시동토출관(13)을 통하여 연결되고 주윤활펌프(16)와 주토출관(17)을 통하여 연결되며 공급되는 윤활유에 포함된 이물질을 제거하는 주필터(22)와, 주필터(22)와 냉각관(25)을 통하여 연결되고 윤활유의 냉각을 행하는 냉각장치(26)와, 냉각장치(26)를 통과한 윤활유가 흐르는 주공급관(31)과, 주공급관(31)에서 분기되어 각각의 기계부품(2),(4),(6)에 윤활유를 공급하고 보조필터(32),(35),(37)가 설치되며 끝에는 노즐이 설치되는 분기공급관 (33),(35),(37)과, 각각의 기계부품(2),(4),(6)에 윤활을 행한 윤활유가 저장탱크 (10)로 복귀하는 복귀관(39),(41),(43),(45)을 포함하는 가스 터빈 엔진 윤활시스템을 제공한다.A storage tank 10 for storing lubricating oil, a starting lubrication pump 12 connected to the storage tank 10 through the start suction pipe 11 and operated by the starter motor, and a main suction pipe to the storage tank 10 ( 15 is connected via the main lubrication pump 16, which is connected to the shaft 18 of the gearbox 2, the starting lubrication pump 12 and the starting discharge pipe 13, and the main lubrication pump ( 16) and the main filter 22 which is connected through the main discharge pipe 17 and removes the foreign matter contained in the supplied lubricant, and the main filter 22 and the cooling tube 25 to cool the lubricant Lubricating oil is supplied to the cooling device 26, the main supply pipe 31 through which the lubricating oil passing through the cooling device 26 flows, and branched from the main supply pipe 31 to the respective mechanical parts 2, 4, and 6. Branch supply pipes (33), (35), (37), which are provided with auxiliary filters (32), (35), (37), and nozzles are installed at the ends thereof, and respective mechanical parts (2) and (4). Lubricating oil It provides a gas turbine engine lubrication system comprising a return pipe 39, 41, 43, 45, which returns to the tank section 10.

Description

가스 터빈 엔진 윤활시스템Gas Turbine Engine Lubrication System

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음Since this is an open matter, no full text was included.

제1도는 본 발명 가스 터빈 엔진 윤활시스템의 일실시에를 개략적으로 나타내는 블럭도.1 is a block diagram schematically showing one embodiment of the gas turbine engine lubrication system of the present invention.

제2도는 가스 터빈 엔진을 개략적으로 나타내는 부분 단면도.2 is a partial cross-sectional view schematically showing a gas turbine engine.

Claims (1)

윤활유를 저장하는 저장탱크와, 상기한 저장탱크에 시동흡입관을 통하여 연결되고 시동모터에 의해 작동되는 시동윤활펌프와, 상기 한 저장탱크에 주흡입관을 통하여 연결되고 기어박스의 측에 연결되어 작동하는 주윤활펌프와, 상기한 시동윤활펌프와 시동토출관을 통하여 연결되고 상기한 주윤활펌프와 주토출관을 통하여 연결되며 공급되는 윤활유에 포함된 이물질을 제거하는 주필터와, 상기한 주필터와 냉각관을 통하여 연결되고 윤활유의 냉각을 행하는 냉각장치와, 상기한 냉각장치를 통과한 윤활유가 흐르는 주공급관과, 상기한 주공급관에 서 분기되어 각각의 기계부품에 윤활유를 공급하고 보조필터가 설치되며 끝에는 노즐이 설치되는 분기공급관과, 각각의 기계부품에 윤활을 행한 윤활유가 저장탱크로 복귀하는 복귀관을 포함하는 가스 터빈 엔진 윤활시스템.A storage tank for storing lubricating oil, a starting lubrication pump connected to the storage tank through a starting suction pipe, and operated by a starting motor, and connected to the storage tank through a main suction pipe and connected to a side of a gearbox. A main filter connected to the main lubrication pump, the starting lubrication pump and the starting discharge pipe, connected to the main lubrication pump and the main discharge pipe, and removing foreign substances contained in the supplied lubricating oil; A cooling device connected to the cooling pipe to cool the lubricant, a main supply pipe through which the lubricant flows through the cooling device flows, branched from the main supply pipe to supply lubricant to each mechanical part, and an auxiliary filter is installed. And a branch supply pipe at which the nozzle is installed, and a return pipe for returning the lubricating oil lubricated to each machine part to the storage tank. Turbine engine's lubrication system. ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019960022006A 1996-06-18 1996-06-18 Lubrication system of gas turbine engine KR100296336B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019960022006A KR100296336B1 (en) 1996-06-18 1996-06-18 Lubrication system of gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019960022006A KR100296336B1 (en) 1996-06-18 1996-06-18 Lubrication system of gas turbine engine

Publications (2)

Publication Number Publication Date
KR980002642A true KR980002642A (en) 1998-03-30
KR100296336B1 KR100296336B1 (en) 2001-11-22

Family

ID=37528009

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019960022006A KR100296336B1 (en) 1996-06-18 1996-06-18 Lubrication system of gas turbine engine

Country Status (1)

Country Link
KR (1) KR100296336B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100726759B1 (en) * 2000-09-26 2007-06-11 삼성테크윈 주식회사 Apparatus and method for providing gas turbine engine with lubricant

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100781151B1 (en) * 2001-12-29 2007-11-30 삼성테크윈 주식회사 Oil tank for gas turbine engine and lubricating system therewith

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59123606U (en) * 1983-02-10 1984-08-20 いすゞ自動車株式会社 Internal combustion engine oil purification device
JPS6194215U (en) * 1984-11-26 1986-06-18

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100726759B1 (en) * 2000-09-26 2007-06-11 삼성테크윈 주식회사 Apparatus and method for providing gas turbine engine with lubricant

Also Published As

Publication number Publication date
KR100296336B1 (en) 2001-11-22

Similar Documents

Publication Publication Date Title
US4875551A (en) Pre-lubricant oil pressure adapter
US5682851A (en) Oil system for an engine that includes an auxiliary priming pump
US6305342B1 (en) Lubrication system for internal combustion engine
KR950032985A (en) Lubrication method of turbocharger bearing and apparatus for same
KR920021840A (en) Exhaust Air Removal and Bypass System and How It Works
US20180179924A1 (en) Engine lubrication structure and motorcycle
JP2001241313A (en) Lubricating oil supplying device of internal combustion engine
KR980002642A (en) Gas Turbine Engine Lubrication System
JP6025564B2 (en) System for lubricating a two-cycle engine
US2739758A (en) Rotary compressor
US1000188A (en) Automatic lubricator for motor-car engines.
JPS55101729A (en) Lubricating system for internal combustion engine equipped with exhaust turbocharger
RU21804U1 (en) INTERNAL COMBUSTION ENGINE LUBRICATION SYSTEM
JPH01116211A (en) Residual fuel treater
KR940021937A (en) Horizontal rotary compressor
KR100195404B1 (en) Oil supply structure of crankshaft
RU2194167C2 (en) Internal combustion engine lubrication system
KR100210146B1 (en) Engine oil system
SU1719664A1 (en) Engine lubricating system
RU2166646C2 (en) Internal combustion engine lubrication system
KR200144334Y1 (en) Lubricant Chiller
KR100221729B1 (en) Aiming device for a head lamp
KR19980041282U (en) Bypass structure of oil
KR960005513Y1 (en) Engine lubrication system
SU979661A1 (en) Apparatus for prestart lubrication of i.c. engine turbocompressor

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E902 Notification of reason for refusal
E701 Decision to grant or registration of patent right
GRNT Written decision to grant
FPAY Annual fee payment

Payment date: 20090430

Year of fee payment: 9

LAPS Lapse due to unpaid annual fee