GB816507A - Apparatus for extracting energy from an elastic fluid such as gas - Google Patents
Apparatus for extracting energy from an elastic fluid such as gasInfo
- 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
Links
- 239000012530 fluid Substances 0.000 title abstract 5
- 239000000314 lubricant Substances 0.000 abstract 9
- 239000011810 insulating material Substances 0.000 abstract 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical group [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 1
- 238000010276 construction Methods 0.000 abstract 1
- 230000001050 lubricating Effects 0.000 abstract 1
- 230000036633 rest Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/08—Adaptations 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.
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)
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 |
-
1955
- 1955-11-18 GB GB3301055A patent/GB816507A/en not_active Expired
Cited By (3)
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 |
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