GB685988A - Improvements relating to the propulsion of vehicles - Google Patents

Improvements relating to the propulsion of vehicles

Info

Publication number
GB685988A
GB685988A GB2178352A GB2178352A GB685988A GB 685988 A GB685988 A GB 685988A GB 2178352 A GB2178352 A GB 2178352A GB 2178352 A GB2178352 A GB 2178352A GB 685988 A GB685988 A GB 685988A
Authority
GB
United Kingdom
Prior art keywords
exchanger
turbine
pressure
jet
gas
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
Application number
GB2178352A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB2178352A priority Critical patent/GB685988A/en
Publication of GB685988A publication Critical patent/GB685988A/en
Expired legal-status Critical Current

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
    • F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air

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

685,988. Gas turbine jet propulsion plant. JENDRASSIK, G. June 13, 1950 [June 14, 1949], No. 21783/52. Divided out of 685,942. Class 110(iii) A jet-propulsion plant including a gas turbine 20 has pressure-exchanger 2 which supplies lowpressure air to a jet nozzle 3 and high-pressure hot gas which divides, one stream passing to the turbine 20, the second stream passing through a combustion chamber 11. The latter is returned through a duct 12 to the input side of the high-pressure scavenging zone of the exchanger. The turbine exhaust passes through a second jet nozzle 23. Fans, such as 14, may be used to assist in scavenging the exchanger cells. The rotor of the exchanger is mounted on a shaft 19 carrying a driving motor (not shown). Compression of the air in the exchanger is effected by expanding hot gases therein. Transfer pipes 17 connect expansion and compression cells. Gas delivered to a nozzle may be re-heated by burner means. The intermediate duct 6 between the fan 14 and the exchanger 2 is of constant cross-sectional area. The turbine, through reduction gearing, drives an airscrew hub 21, when the plant is used on an aircraft. Any type of pressure-exchanger may be used.
GB2178352A 1949-06-14 1949-06-14 Improvements relating to the propulsion of vehicles Expired GB685988A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2178352A GB685988A (en) 1949-06-14 1949-06-14 Improvements relating to the propulsion of vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2178352A GB685988A (en) 1949-06-14 1949-06-14 Improvements relating to the propulsion of vehicles

Publications (1)

Publication Number Publication Date
GB685988A true GB685988A (en) 1953-01-14

Family

ID=10168729

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2178352A Expired GB685988A (en) 1949-06-14 1949-06-14 Improvements relating to the propulsion of vehicles

Country Status (1)

Country Link
GB (1) GB685988A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE955557C (en) * 1953-04-05 1957-01-03 Max Adolf Mueller Dipl Ing Gas turbine engine with rotary valve and isochoric compression
DE1078373B (en) * 1956-06-04 1960-03-24 Dudley Brian Spalding Gas turbine system with pressure exchanger

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE955557C (en) * 1953-04-05 1957-01-03 Max Adolf Mueller Dipl Ing Gas turbine engine with rotary valve and isochoric compression
DE1078373B (en) * 1956-06-04 1960-03-24 Dudley Brian Spalding Gas turbine system with pressure exchanger

Similar Documents

Publication Publication Date Title
US2168726A (en) Propulsion of aircraft and gas turbines
US2748564A (en) Intermittent combustion gas turbine engine
US2487842A (en) Aircraft power plant apparatus
GB1069033A (en) Improvements in or relating to gas turbine jet propulsion engines
US3740949A (en) Fuel cooled ram air reaction propulsion engine
US2646663A (en) Semiopen circuit gas-turbine engine
US3733826A (en) Fuel cooled ram air reaction propulsion engine
GB713783A (en) Gas turbine propulsion units
US2757509A (en) Jet reaction propulsion units utilizing a pressure exchanger
GB955013A (en) Improvements in and relating to Composite Jet Engines
GB685988A (en) Improvements relating to the propulsion of vehicles
GB538022A (en) Improvements in the propulsion of aircraft
GB513751A (en) Improvements in power plants for aircraft
US3721093A (en) Reaction propulsion engine with vaporized fuel driven turbine
US2603948A (en) Multistage gas turbine blade cooling with air in high-pressure turbine stages
GB881967A (en) Improved propulsion unit for use in vertical take-off aircraft
GB624273A (en) Improvements in or relating to compressor systems
GB777694A (en) Improvements relating to internal combustion turbines in combination with ram-jet engines
GB706841A (en) Improvements relating to turbine jet propulsion power units
GB695891A (en) Improvements in or relating to gas-turbine engines
GB712633A (en) Improvements relating to gas-turbine engines
GB814380A (en) Power plant incorporating a dynamic compressor
GB617856A (en) Improvements relating to vehicle propulsion
GB588097A (en) Improvements in or relating to internal combustion turbine power plants
GB719479A (en) Improvements relating to gas turbine jet propulsion power units