GB723310A - Improvements in and relating to jet propulsion units - Google Patents
Improvements in and relating to jet propulsion unitsInfo
- Publication number
- GB723310A GB723310A GB1951A GB1951A GB723310A GB 723310 A GB723310 A GB 723310A GB 1951 A GB1951 A GB 1951A GB 1951 A GB1951 A GB 1951A GB 723310 A GB723310 A GB 723310A
- Authority
- GB
- United Kingdom
- Prior art keywords
- relating
- jet propulsion
- propulsion units
- jet
- turbine
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
- F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
723,310. Jet-propulsion plant. POWELL, S. A. March 31, 1952 [Jan. 11, 1951], No. 19/51. Class 110 (3). In a gas-turbine jet-propulsion unit water under pressure is injected into the gas stream at a position downstream of the turbine 4, through a series of circumferentially-spaced nozzles 21 or through a porous wall. Water is supplied to the ring manifold 18 and through the pipes 19, 20 to the nozzles issuing therefrom in the downstream direction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1951A GB723310A (en) | 1951-01-11 | 1951-01-11 | Improvements in and relating to jet propulsion units |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1951A GB723310A (en) | 1951-01-11 | 1951-01-11 | Improvements in and relating to jet propulsion units |
Publications (1)
Publication Number | Publication Date |
---|---|
GB723310A true GB723310A (en) | 1955-02-09 |
Family
ID=9696920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1951A Expired GB723310A (en) | 1951-01-11 | 1951-01-11 | Improvements in and relating to jet propulsion units |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB723310A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3327480A (en) * | 1964-08-08 | 1967-06-27 | Heinkel Ag Ernst | Afterburner device with deflector means |
-
1951
- 1951-01-11 GB GB1951A patent/GB723310A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3327480A (en) * | 1964-08-08 | 1967-06-27 | Heinkel Ag Ernst | Afterburner device with deflector means |
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