GB1301104A - Improvements in or relating to closed-cycle heat engines - Google Patents
Improvements in or relating to closed-cycle heat enginesInfo
- Publication number
- GB1301104A GB1301104A GB3598369A GB3598369A GB1301104A GB 1301104 A GB1301104 A GB 1301104A GB 3598369 A GB3598369 A GB 3598369A GB 3598369 A GB3598369 A GB 3598369A GB 1301104 A GB1301104 A GB 1301104A
- Authority
- GB
- United Kingdom
- Prior art keywords
- working fluid
- particulate material
- discharging
- engines
- bed
- 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
- 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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
1301104 Closed cycle heat engines; gas turbine engines ROLLS ROYCE Ltd 17 July 1970 [17 July 1969] 35983/69 Heading F1G A closed cycle heat engine comprises at least one fluidized bed having a first flow path comprising at least one conduit which is embedded in use in the particulate material of the bed and which is connected to receive working fluid exhausted by the engine, and a second flow path adapted to contain the particulate material of the bed and which is adapted to be supplied with a cooling gas so as to fluidize the particulate material. The closed cycle gas turbine plant shown in Fig. 1 comprises compressor 12, working fluid heater 18, a first turbine 20 which drives the compressor and a second turbine 24 which drives a useful load which may be the transmission of a vehicle. The working fluid discharging from the power turbine 24 passes through a coil 40 which is disposed within the particulate material 38 of a fluidized bed heat exchanger 32, cooling air being supplied by fan 46 to fluidize the bed, the air entering at 42 and discharging at 44. In Fig. 2 the heat exchanger comprises four elements 37a through which the working fluid flows in series through coils 40u and to which cooling air is supplied in four parallel paths entering at 42a and discharging at 44a; the particulate material is indicated at 38a. In Fig.3 (not shown) the heat exchanger again comprises four elements (37b) through which the working fluid flows in series through coils (40b) and through which the cooling air flows in series entering each section at (42b) and discharging therefrom at (44b). The cooling air discharging from the heat exchangers may be utilised to preheat the working fluid passing to the heater 18. The particulate material may be sand. The invention is also applicable in the case of Rankine cycle engines in which the fluidized bed acts as a condenser and to closed cycle piston engines.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3598369A GB1301104A (en) | 1969-07-17 | 1969-07-17 | Improvements in or relating to closed-cycle heat engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3598369A GB1301104A (en) | 1969-07-17 | 1969-07-17 | Improvements in or relating to closed-cycle heat engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1301104A true GB1301104A (en) | 1972-12-29 |
Family
ID=10383681
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3598369A Expired GB1301104A (en) | 1969-07-17 | 1969-07-17 | Improvements in or relating to closed-cycle heat engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1301104A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
-
1969
- 1969-07-17 GB GB3598369A patent/GB1301104A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8708083B2 (en) | 2009-05-12 | 2014-04-29 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLE | Entries relating assignments, transmissions, licences in the register of patents | ||
PCNP | Patent ceased through non-payment of renewal fee |