GB1420722A - Hot-air turbine engine - Google Patents
Hot-air turbine engineInfo
- Publication number
- GB1420722A GB1420722A GB1156274A GB1156274A GB1420722A GB 1420722 A GB1420722 A GB 1420722A GB 1156274 A GB1156274 A GB 1156274A GB 1156274 A GB1156274 A GB 1156274A GB 1420722 A GB1420722 A GB 1420722A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- casings
- compressor
- disposed
- section
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1420722 Hot air turbine plant W HARTLEY 15 March 1974 11562/74 Heading F1G The invention relates to a hot air turbine engine in which the compressor, heating section and the turbine are formed as an integral rotor assembly. The assembly comprises an inner casing 2 and an outer casing 3 secured to a shaft 7 mounted in bearings 1, the two casings defining an annular passage open at the inlet end 8 and at the outlet end 9. Blades 4 are disposed between the casings at the inlet end to define a centrifugal compressor, and blades 5 are disposed between the casings at the outlet end to define a radial inward flow turbine. A series of partitions are disposed between the casings between the compressor and turbine portions to form the heating section. Air compressed in the compressor section is heated indirectly in the heating section, then expanded in the turbine section, the turbine acting to drive the compressor also to provide useful power. A stator casing 10 may be disposed around the outer casing 3, there being seals 11 at the ends and the space between the casings 10 and 3 may be evacuated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1156274A GB1420722A (en) | 1974-03-15 | 1974-03-15 | Hot-air turbine engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1156274A GB1420722A (en) | 1974-03-15 | 1974-03-15 | Hot-air turbine engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1420722A true GB1420722A (en) | 1976-01-14 |
Family
ID=9988529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1156274A Expired GB1420722A (en) | 1974-03-15 | 1974-03-15 | Hot-air turbine engine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1420722A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998030846A1 (en) * | 1997-01-14 | 1998-07-16 | Nowacki Jan Erik | Motor, refrigeration machine or heat pump |
-
1974
- 1974-03-15 GB GB1156274A patent/GB1420722A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998030846A1 (en) * | 1997-01-14 | 1998-07-16 | Nowacki Jan Erik | Motor, refrigeration machine or heat pump |
| US6196020B1 (en) | 1997-01-14 | 2001-03-06 | Jan-Erik Nowacki | Motor, refrigeration machine or heat pump |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |