GB118650A - Improvements in Air or Gas Turbines. - Google Patents

Improvements in Air or Gas Turbines.

Info

Publication number
GB118650A
GB118650A GB935717A GB935717A GB118650A GB 118650 A GB118650 A GB 118650A GB 935717 A GB935717 A GB 935717A GB 935717 A GB935717 A GB 935717A GB 118650 A GB118650 A GB 118650A
Authority
GB
United Kingdom
Prior art keywords
air
fan
supplied
working
passages
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
GB935717A
Inventor
Thomas Frederick Bailes
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 GB935717A priority Critical patent/GB118650A/en
Publication of GB118650A publication Critical patent/GB118650A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

118,650. Bailes, T. F. Dec. 28, 1917. Axial-flow type; cooling parts; working-fluid supply.-A turbine working with sub-atmospheric expansion comprises a number of stages 8, 7, 6, 5 supplied with air at atmospheric pressure through an inlet 15, the air being heated by fuel sprayed through a nozzle 14. The final stage of the expansion is effected in a ring of nozzles 22, the velocity then remaining in the gases being converted into pressure energy in divergent passages 18, which are cooled by air blasts supplied through passages 16, 19. A fan 20 on the turbine shaft assists in re-compressing the exhaust and facilitates starting. The air blasts may be caused by a fan or by the motion of the apparatus through the air.
GB935717A 1917-12-28 1917-12-28 Improvements in Air or Gas Turbines. Expired GB118650A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB935717A GB118650A (en) 1917-12-28 1917-12-28 Improvements in Air or Gas Turbines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB935717A GB118650A (en) 1917-12-28 1917-12-28 Improvements in Air or Gas Turbines.

Publications (1)

Publication Number Publication Date
GB118650A true GB118650A (en) 1918-09-12

Family

ID=32343718

Family Applications (1)

Application Number Title Priority Date Filing Date
GB935717A Expired GB118650A (en) 1917-12-28 1917-12-28 Improvements in Air or Gas Turbines.

Country Status (1)

Country Link
GB (1) GB118650A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623356A (en) * 1952-12-30 Rotary compressor
US2977753A (en) * 1954-02-13 1961-04-04 Rech Etudes Prod Improvements in continuous flow gas engines
US3008402A (en) * 1955-02-25 1961-11-14 Rech Etudes Prod Means for displacing very large amounts of air
DE1119055B (en) * 1954-02-13 1961-12-07 Georges Boulet Jet propulsion

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623356A (en) * 1952-12-30 Rotary compressor
US2977753A (en) * 1954-02-13 1961-04-04 Rech Etudes Prod Improvements in continuous flow gas engines
DE1119055B (en) * 1954-02-13 1961-12-07 Georges Boulet Jet propulsion
US3008402A (en) * 1955-02-25 1961-11-14 Rech Etudes Prod Means for displacing very large amounts of air

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