GB549700A - Improvements in or relating to the propulsion of aircraft or vehicles - Google Patents

Improvements in or relating to the propulsion of aircraft or vehicles

Info

Publication number
GB549700A
GB549700A GB1565240A GB1565240A GB549700A GB 549700 A GB549700 A GB 549700A GB 1565240 A GB1565240 A GB 1565240A GB 1565240 A GB1565240 A GB 1565240A GB 549700 A GB549700 A GB 549700A
Authority
GB
United Kingdom
Prior art keywords
aircraft
compressor
shaft
exhaust
propulsion
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
GB1565240A
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.)
TURBO ENGINEERING CORP
Original Assignee
TURBO ENGINEERING CORP
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
Priority to US177669A priority Critical patent/US2216731A/en
Application filed by TURBO ENGINEERING CORP filed Critical TURBO ENGINEERING CORP
Priority to GB1565240A priority patent/GB549700A/en
Publication of GB549700A publication Critical patent/GB549700A/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

549,700. Pumps. JACKSON, L. MELLERSH-. (Turbo Engineering Corporation). Oct. 24, 1940, No. 15652. [Class 7 (ii)] [Also in Groups XXVI and XAXIII] An exhaust-driven turbo-compressor for supercharging the engines of aircraft or vehicles, and adapted to be arranged in the airstream, comprises a casing 8 having a forwardly-directed opening 22 through which the airstream enters in passing to compressor stages 20, 24 discharging at 10 to the engine, the exhaust from which enters at 12 into a chamber 32 leading by nozzles 30 to the blades 28 of a turbine mounted on the same shaft 14. The shaft 14 is hollow for the passage of cooling-air, which passes through holes 40 in the shaft into a chamber 42 having outlet apertures 44. Some of the air from the compressor is also directed through a passage 34 to cooling-passages 36, and is discharged at 38 with the exhaust gases. This discharge may be such as to assist in the propulsion of the aircraft &c. In modifications, the upper part o,f the casing 8 may be arranged within the body of the aircraft &c. or the whole unit may be disposed within a wing of an Aircraft inlet and discharge passages to and from the unit being formed in the wing structure. Specification 520,045, [Group XXVI], is referred to.
GB1565240A 1937-12-02 1940-10-24 Improvements in or relating to the propulsion of aircraft or vehicles Expired GB549700A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US177669A US2216731A (en) 1937-12-02 1937-12-02 Turbosupercharger mounting
GB1565240A GB549700A (en) 1940-10-24 1940-10-24 Improvements in or relating to the propulsion of aircraft or vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1565240A GB549700A (en) 1940-10-24 1940-10-24 Improvements in or relating to the propulsion of aircraft or vehicles

Publications (1)

Publication Number Publication Date
GB549700A true GB549700A (en) 1942-12-03

Family

ID=10062984

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1565240A Expired GB549700A (en) 1937-12-02 1940-10-24 Improvements in or relating to the propulsion of aircraft or vehicles

Country Status (1)

Country Link
GB (1) GB549700A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2263313A (en) * 1991-11-14 1993-07-21 Geoffrey Light Wilde Turbocharger with exhaust gas cooling.
WO2012045531A1 (en) * 2010-10-05 2012-04-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Supercharging device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2263313A (en) * 1991-11-14 1993-07-21 Geoffrey Light Wilde Turbocharger with exhaust gas cooling.
GB2263313B (en) * 1991-11-14 1994-11-09 Geoffrey Light Wilde Turbo charger
WO2012045531A1 (en) * 2010-10-05 2012-04-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Supercharging device

Similar Documents

Publication Publication Date Title
GB1497477A (en) Gas turbine engine
GB609926A (en) Improvements in or relating to internal-combustion turbines
GB588096A (en) Improvements in or relating to internal combustion turbine power plants
GB742477A (en) Improvements in or relating to bladed stator or rotor constructions for fluid machines such as axial-flow turbines or compressors
GB1273673A (en) Improvements relating to jet engines
GB583022A (en) Improvements relating to internal combustion turbines and the like
GB1251312A (en)
GB666416A (en) Gas turbine power plant for jet propulsion
GB1321657A (en) Ducted fan gas turbine jet propulsion engine
GB578306A (en) Improvements in an exhaust turbosupercharger
US2393713A (en) Aircraft supercharger
GB838602A (en) Improvements in or relating to gas turbine plant
GB549700A (en) Improvements in or relating to the propulsion of aircraft or vehicles
FR1288767A (en) Turbomachinery reactor
FR2389772A1 (en) Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream
GB881785A (en) Power plant for short forward or vertical take-off aircraft
GB881967A (en) Improved propulsion unit for use in vertical take-off aircraft
GB737081A (en) Improvements relating to jet propulsion engines
GB711985A (en) Improvements in gas turbines
GB800261A (en) Improvements in and relating to jet propulsion engines
GB654411A (en) Improvements in or relating to jet propulsion units
GB144259A (en) Improvements in and relating to turbo-superchargers for aeroplanes, airships and the like
GB1519449A (en) Gas turbine engine
GB1280361A (en) Improvements in or relating to gas turbine engines
GB694414A (en) Improvements in or relating to internal combustion gas turbine engines