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GB646252A - Improvements in and relating to gas turbines - Google Patents

Improvements in and relating to gas turbines

Info

Publication number
GB646252A
GB646252A GB1908048A GB1908048A GB646252A GB 646252 A GB646252 A GB 646252A GB 1908048 A GB1908048 A GB 1908048A GB 1908048 A GB1908048 A GB 1908048A GB 646252 A GB646252 A GB 646252A
Authority
GB
United Kingdom
Prior art keywords
turbine
relating
gas turbines
jet
nozzle
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
GB1908048A
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 GB1908048A priority Critical patent/GB646252A/en
Publication of GB646252A publication Critical patent/GB646252A/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
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

646,252. Jet propulsion plant. LOMAX, F. July 15, 1948, No. 19080. [Class 110(iii)] Gases from a combustion chamber e are delivered through an annular nozzle g into a collecting chamber h from which they pass to the turbine c. The turbine discharges to a propulsion jet i. A turbine stage may drive a separate power shaft. The inner wall of the nozzle g may rotate with the turbine shaft and may be formed with peripheral grooves or blades.
GB1908048A 1948-07-15 1948-07-15 Improvements in and relating to gas turbines Expired GB646252A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1908048A GB646252A (en) 1948-07-15 1948-07-15 Improvements in and relating to gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1908048A GB646252A (en) 1948-07-15 1948-07-15 Improvements in and relating to gas turbines

Publications (1)

Publication Number Publication Date
GB646252A true GB646252A (en) 1950-11-15

Family

ID=10123435

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1908048A Expired GB646252A (en) 1948-07-15 1948-07-15 Improvements in and relating to gas turbines

Country Status (1)

Country Link
GB (1) GB646252A (en)

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