GB541349A - Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft - Google Patents
Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraftInfo
- Publication number
- GB541349A GB541349A GB1189940A GB1189940A GB541349A GB 541349 A GB541349 A GB 541349A GB 1189940 A GB1189940 A GB 1189940A GB 1189940 A GB1189940 A GB 1189940A GB 541349 A GB541349 A GB 541349A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propulsion
- aircraft
- relating
- gas turbines
- prime movers
- 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
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Discharge Lamp (AREA)
Abstract
541,349. Propelling ships. HEWSON, B. T., and LOCAN, A. July 19, 1940, No. 11899. [Class 114] [Also in Group XXVI] A combustion chamber 101 delivers gas to a central jet tube 100 and other ignition apparatuses 104 deliver gas through orifices 105 into the jet tube. The chamber 101 may be replaced by a funnel-shaped opening having a spring-pressed valve opening inwards with the air pressure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1189940A GB541349A (en) | 1940-07-19 | 1940-07-19 | Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1189940A GB541349A (en) | 1940-07-19 | 1940-07-19 | Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB541349A true GB541349A (en) | 1941-11-24 |
Family
ID=9994693
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1189940A Expired GB541349A (en) | 1940-07-19 | 1940-07-19 | Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB541349A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2435138A (en) * | 1943-01-15 | 1948-01-27 | Armstrong Siddeley Motors Ltd | Compound internal-combustion turbine plant |
US2454738A (en) * | 1944-01-31 | 1948-11-23 | Power Jets Res And Development | Internal-combustion turbine power plant |
US2477798A (en) * | 1941-04-08 | 1949-08-02 | Rolls Royce | Contrarotating axial flow high and low pressure turbine and compressor with bladed duct with turbine cooling |
US2479573A (en) * | 1943-10-20 | 1949-08-23 | Gen Electric | Gas turbine power plant |
US2518498A (en) * | 1946-03-25 | 1950-08-15 | Schulte Rudolph Carl | Propulsion system for aircraft |
US2531761A (en) * | 1944-12-02 | 1950-11-28 | Aerojet Engineering Corp | Thermal jet and rocket motor propulsion system |
US2593541A (en) * | 1947-04-03 | 1952-04-22 | Napier & Son Ltd | Cooling apparatus for use with aero or other engines |
US3410093A (en) * | 1967-05-26 | 1968-11-12 | Ghougasian John Nazareth | Reaction thrust engine with fluid operated compressor |
-
1940
- 1940-07-19 GB GB1189940A patent/GB541349A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2477798A (en) * | 1941-04-08 | 1949-08-02 | Rolls Royce | Contrarotating axial flow high and low pressure turbine and compressor with bladed duct with turbine cooling |
US2435138A (en) * | 1943-01-15 | 1948-01-27 | Armstrong Siddeley Motors Ltd | Compound internal-combustion turbine plant |
US2479573A (en) * | 1943-10-20 | 1949-08-23 | Gen Electric | Gas turbine power plant |
US2454738A (en) * | 1944-01-31 | 1948-11-23 | Power Jets Res And Development | Internal-combustion turbine power plant |
US2531761A (en) * | 1944-12-02 | 1950-11-28 | Aerojet Engineering Corp | Thermal jet and rocket motor propulsion system |
US2518498A (en) * | 1946-03-25 | 1950-08-15 | Schulte Rudolph Carl | Propulsion system for aircraft |
US2593541A (en) * | 1947-04-03 | 1952-04-22 | Napier & Son Ltd | Cooling apparatus for use with aero or other engines |
US3410093A (en) * | 1967-05-26 | 1968-11-12 | Ghougasian John Nazareth | Reaction thrust engine with fluid operated compressor |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB627832A (en) | Improvement in propulsion plant comprising a gas turbine driven airscrew | |
GB943839A (en) | Jet propulsion engines | |
GB586572A (en) | Improvements in internal combustion turbine plant for propulsion by jet action, at least in part | |
GB541349A (en) | Improvements in and relating to prime movers, more particularly gas turbines for the propulsion of aircraft | |
GB588847A (en) | Improvements in combustion chambers for internal combustion turbines | |
GB616695A (en) | Improvements in and relating to gas turbine power plants | |
GB572724A (en) | Improvements in or relating to aircraft propulsion | |
GB657789A (en) | Improvements relating to liquid fuel combustion equipment for gas-turbine engines | |
GB627634A (en) | Improvements in or relating to gas turbine aircraft propulsion power plants | |
GB587083A (en) | Improvements in combustion chambers for internal combustion turbines | |
GB648699A (en) | Improvements in or relating to gas-turbine engine fuel systems and liquid fuel injectors therefor | |
GB275677A (en) | Improvements in or relating to reaction-driven propellers | |
GB881967A (en) | Improved propulsion unit for use in vertical take-off aircraft | |
GB656930A (en) | Improvements in gas turbines | |
GB701320A (en) | Improvements in or relating to combustion equipment of gas-turbine engines | |
GB579511A (en) | Improvements in or relating to jet-propulsion apparatus for aircraft | |
GB588092A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB768969A (en) | Improvements in jet propulsion plant | |
GB733243A (en) | Improvements relating to aircraft | |
GB621407A (en) | Improvements relating to gas-turbine power-plants | |
GB584169A (en) | Improvements in or relating to power plants for aircraft | |
GB578005A (en) | Improvements in and relating to jet propulsion plant | |
GB700705A (en) | Combustion chambers for jet propulsion engines, gas turbines or other prime movers | |
GB847868A (en) | Improvements relating to vertical take-off aircraft | |
GB881663A (en) | Improvements in or relating to gas turbine propulsion units |