GB587518A - Improvements in or relating to blades for axial flow compressors and turbines - Google Patents

Improvements in or relating to blades for axial flow compressors and turbines

Info

Publication number
GB587518A
GB587518A GB542643A GB542643A GB587518A GB 587518 A GB587518 A GB 587518A GB 542643 A GB542643 A GB 542643A GB 542643 A GB542643 A GB 542643A GB 587518 A GB587518 A GB 587518A
Authority
GB
United Kingdom
Prior art keywords
blades
turbines
relating
flow compressors
axial flow
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
GB542643A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB542643A priority Critical patent/GB587518A/en
Publication of GB587518A publication Critical patent/GB587518A/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

587,518. Turbine and compressor blades. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and HOWELL, A. R. April 5, 1943, No. 5426. Drawings to Specification. [Classes 110 (i) and 110 (iii)] Twisted blades for axial-flow compressors and turbines are such that the difference between the circumferential components of fluid velocity relative to a blade at inlet and outlet is inversely proportional to the distance from the axis of rotation. Specification 511,278 is referred to.
GB542643A 1943-04-05 1943-04-05 Improvements in or relating to blades for axial flow compressors and turbines Expired GB587518A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB542643A GB587518A (en) 1943-04-05 1943-04-05 Improvements in or relating to blades for axial flow compressors and turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB542643A GB587518A (en) 1943-04-05 1943-04-05 Improvements in or relating to blades for axial flow compressors and turbines

Publications (1)

Publication Number Publication Date
GB587518A true GB587518A (en) 1947-04-29

Family

ID=9795960

Family Applications (1)

Application Number Title Priority Date Filing Date
GB542643A Expired GB587518A (en) 1943-04-05 1943-04-05 Improvements in or relating to blades for axial flow compressors and turbines

Country Status (1)

Country Link
GB (1) GB587518A (en)

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