GB958165A - Improvements in or relating to pressure equalizers - Google Patents
Improvements in or relating to pressure equalizersInfo
- Publication number
- GB958165A GB958165A GB1914862A GB1914862A GB958165A GB 958165 A GB958165 A GB 958165A GB 1914862 A GB1914862 A GB 1914862A GB 1914862 A GB1914862 A GB 1914862A GB 958165 A GB958165 A GB 958165A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pressure
- duct
- inlet ports
- end plates
- outlet port
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
- F04F13/00—Pressure exchangers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
958,165. Pressure exchangers. D. B. SPALDING. May 2, 1963 [May 17, 1962], No. 19148/62. Heading F1N. In a pressure exchanger serving as a pressure equalizer and comprising a ring of openended rotor cells 1 bounded by end plates 3, 4 having high and low pressure inlet ports 6, 8 connected to ducts 5, 7 and an intermediate pressure outlet port 9 connected to a duct 10, the supply of high pressure to port 6 is effected by an ejector the nozzle 13 of which is connected to a gas supply at a pressure greater than that prevailing in duct 5. As shown nozzle 13 is connected to the compressor of a gas turbine plant and induces a portion of the intermediate pressure gas bled from duct 10 through a duct 12. In a modification branch 12 is closed off from duct 10 and is connected to a vent 14 to atmosphere. In a further modification the end plates are provided with a plurality of pairs of high and low pressure inlet ports and an intermediate pressure outlet port for each pair of inlet ports. U.S.A. Specification 2,946,184 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1914862A GB958165A (en) | 1962-05-17 | 1962-05-17 | Improvements in or relating to pressure equalizers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1914862A GB958165A (en) | 1962-05-17 | 1962-05-17 | Improvements in or relating to pressure equalizers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB958165A true GB958165A (en) | 1964-05-13 |
Family
ID=10124550
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1914862A Expired GB958165A (en) | 1962-05-17 | 1962-05-17 | Improvements in or relating to pressure equalizers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB958165A (en) |
-
1962
- 1962-05-17 GB GB1914862A patent/GB958165A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB856674A (en) | Blades for gas turbine engines | |
GB943839A (en) | Jet propulsion engines | |
GB1016316A (en) | Air-cooled surface condenser | |
GB995962A (en) | Means for varying the flow of air or other gaseous medium in a distributing chamber | |
GB769373A (en) | Improvements in or relating to high-speed wind tunnels | |
GB1214892A (en) | Improvements in nuclear power plant suitable for use in aircraft propulsion systems | |
GB923557A (en) | Improvements in thrust diverting means for vtol and stol aircraft | |
GB765731A (en) | Improvements relating to pressure exchangers | |
GB839798A (en) | A device for inducing secondary air by ejecting action into a current of primary airand mixing them | |
GB958165A (en) | Improvements in or relating to pressure equalizers | |
GB792831A (en) | An improved gas-flow control device for a jet-propulsion plant | |
GB927207A (en) | Improvements in gas turbine units | |
GB1384959A (en) | Pressure wave machines | |
GB1070130A (en) | Aeofoil shaped blade for a fluid flow machine such as a gas turbine engine | |
GB827798A (en) | Improvements in or relating to pressure exchangers | |
GB913312A (en) | Jet propulsion engine | |
GB819304A (en) | Improvements in or relating to power plant including a pressure exchanger | |
GB792858A (en) | Improvements in or relating to pressure exchangers | |
GB1073195A (en) | Pressure exchanger | |
GB1118435A (en) | Improvements in and relating to turbines | |
GB921686A (en) | Improvements in or relating to pressure exchangers | |
GB854621A (en) | Improvements in or relating to pressure exchangers | |
GB372377A (en) | Improvements in or relating to turbines | |
GB917019A (en) | Improvements in and relating to pressure exchangers | |
GB923797A (en) | Improvements in or relating to pressure exchanger plant |