GB732625A - Improvements in or relating to compressed air turbines - Google Patents

Improvements in or relating to compressed air turbines

Info

Publication number
GB732625A
GB732625A GB24188/53A GB2418853A GB732625A GB 732625 A GB732625 A GB 732625A GB 24188/53 A GB24188/53 A GB 24188/53A GB 2418853 A GB2418853 A GB 2418853A GB 732625 A GB732625 A GB 732625A
Authority
GB
United Kingdom
Prior art keywords
compressed air
relating
turbine
air turbines
sept
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
GB24188/53A
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.)
PAUL KANIS
Original Assignee
PAUL KANIS
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 PAUL KANIS filed Critical PAUL KANIS
Publication of GB732625A publication Critical patent/GB732625A/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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/06—Adaptations for driving, or combinations with, hand-held tools or the like control thereof

Landscapes

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

Abstract

732,625. Compressed air turbine. KANIS, P. Sept. 1, 1953 [Sept. 1, 1952], No. 24188/53. Class 110 (3). In a turbine driven by compressed air fed to nozzles. 5, part only of the periphery of the blade is, provided with a cover 6 so that air impurities and snow or ice particles formed are centrifugally ejected. The cover corresponds with the nozzle arc and may be formed integrally with or separately from the casing 3. The turbine may be multi-stage and the rotor may be journalled on both sides.
GB24188/53A 1952-09-01 1953-09-01 Improvements in or relating to compressed air turbines Expired GB732625A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE732625X 1952-09-01

Publications (1)

Publication Number Publication Date
GB732625A true GB732625A (en) 1955-06-29

Family

ID=6639638

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24188/53A Expired GB732625A (en) 1952-09-01 1953-09-01 Improvements in or relating to compressed air turbines

Country Status (1)

Country Link
GB (1) GB732625A (en)

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