GB816507A - Apparatus for extracting energy from an elastic fluid such as gas - Google Patents

Apparatus for extracting energy from an elastic fluid such as gas

Info

Publication number
GB816507A
GB816507A GB3301055A GB3301055A GB816507A GB 816507 A GB816507 A GB 816507A GB 3301055 A GB3301055 A GB 3301055A GB 3301055 A GB3301055 A GB 3301055A GB 816507 A GB816507 A GB 816507A
Authority
GB
United Kingdom
Prior art keywords
lubricant
pump
gas
supplied
outlet
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
GB3301055A
Inventor
Judson Sterling Swearingen
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.)
Air Products Inc
Original Assignee
Air Products Inc
Filing date
Publication date
Application filed by Air Products Inc filed Critical Air Products Inc
Publication of GB816507A publication Critical patent/GB816507A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/08Adaptations for driving, or combinations with, pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sliding-Contact Bearings (AREA)

Abstract

816,507. Lubricating. AIR PRODUCTS Inc. Nov. 18, 1955, No. 33010/55. Class 12 (3). Apparatus for extracting energy from an elastic fluid such as a gas comprises a turbine 1, or other elastic fluid expansion engine, operable to remove energy from the fluid upon expansion of the latter, and a pump 6 coupled thereto and having an inlet 10 and an outlet 8 for an hydraulic fluid, e.g. a lubricant, which is circulated in a closed system including a cooler &c. 9. In the construction shown, a gas turbine having a gas inlet 2 and a gas outlet 3 has its rotor 25 carried on a vertical shaft 27 which passes through a radial bearing 4 and rests upon a thrust bearing 5. The lower end of the shaft is connected to a pump rotor carrying impeller blades 53. The pump is adapted to discharge lubricant under pressure through the outlet 8 and the cooler 9 and back through the pump inlet 10. Part of the lubricant from the outlet 8 is supplied to a connection 11 leading to the bearing 4 and part is supplied to a connection 12 leading to the thrust bearing 5. Lubricant supplied to these bearings is drawn off through a connection 13 into a reservoir 14 which is provided at the top with a receptacle 16 provided with a small leak 17. The outlet 8 of the pump is connected to the receptacle through a valve 18 whereby, during the operation of the apparatus, the receptacle 16 may be supplied with lubricant in quantity greater than that which can leak through the opening 17. The gas turbine is enclosed by a cover-plate 19 and a seal is provided between the housing and the rotor 25, comprising a carbon ring 28 carried on a flexible metallic bellows 29. The shaft 27 below the rotor passes through a sleeve 31 which fits close to, but not in tight frictional engagement with, the shaft 27, and is carried on a plate 32 closing an opening in the turbine housing 1. Below the plate 32 is a block 34 of thermal insulating material surrounded by a sleeve 36. Thermal insulating material 40 surrounds the entire turbine housing. Leakage of gas down the outside of the shaft 27 is prevented by the lubricant passed to the bearings 4 and 5. In order that the inlet pressure required by the pump may be high enough, lubricant is supplied to the pump through a connection 58 with a tip 59 located within the entrance to a restriction 57 from the pipe 10. When the apparatus is in use lubricant entering the top of the reservoir 14 will gradually fill the receptacle 16, the level in the lower part of the reservoir falling to the line 62, so that the space 44 below the radial bearing 4 will be kept drained of lubricant which would otherwise be beaten into froth.
GB3301055A 1955-11-18 Apparatus for extracting energy from an elastic fluid such as gas Expired GB816507A (en)

Publications (1)

Publication Number Publication Date
GB816507A true GB816507A (en) 1959-07-15

Family

ID=1743270

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3301055A Expired GB816507A (en) 1955-11-18 Apparatus for extracting energy from an elastic fluid such as gas

Country Status (1)

Country Link
GB (1) GB816507A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009017473A3 (en) * 2007-07-27 2010-08-12 Utc Power Corporation Oil recovery from an evaporator of an organic rankine cycle (orc) system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009017473A3 (en) * 2007-07-27 2010-08-12 Utc Power Corporation Oil recovery from an evaporator of an organic rankine cycle (orc) system
CN101970808A (en) * 2007-07-27 2011-02-09 Utc电力公司 Oil recovery from an evaporator of an organic rankine cycle (orc) system
US8769952B2 (en) 2007-07-27 2014-07-08 United Technologies Corporation Oil recovery from an evaporator of an organic rankine cycle (ORC) system

Similar Documents

Publication Publication Date Title
US2133879A (en) Shaft packing
US2257011A (en) Lubricating and cooling system for the stuffing boxes for pumps and like engines
US2266107A (en) Centrifugal refrigerating apparatus
GB698898A (en) Improvements in elastic fluid turbines
US3099385A (en) Turbo blowers
US2463898A (en) Turbine sealing construction
GB816507A (en) Apparatus for extracting energy from an elastic fluid such as gas
US3103176A (en) Turbine-driven centrifugal pump
US2485447A (en) Sealing arrangement for the shafts of turbomachines of thermal power plants in which the greater part of a gaseous medium continuously describes a closed cycle under pressure above atmospheric
US2992618A (en) Liquid-metal pump seal
US2883214A (en) Stuffing-box assembly having a liquid seal
GB1229049A (en)
US2804021A (en) Apparatus for extracting energy from gas
US3597024A (en) Liquid ring seal
US3220352A (en) Pump lubrication system
CN216199268U (en) Self-balancing multistage pump outer water cooling cavity structure
GB850234A (en) A shaft sealing device
GB677490A (en) Oil supply and scavenge system
GB834923A (en) Improvements in or relating to sealing means
US3520640A (en) Fluid circulator
GB783118A (en) Bearing assemblies for supporting rotary shafts
US3151702A (en) Zero gravity lubricating system
GB777954A (en) Improvements in or relating to axial-flow and centrifugal compressors and gas turbines
GB840671A (en) Improvements relating to centrifugal pumps
GB1022692A (en) Improvements in electrical machines having liquid cooled rotors