CA564048A - Axial flow fans and compressors - Google Patents

Axial flow fans and compressors

Info

Publication number
CA564048A
CA564048A CA564048A CA564048DA CA564048A CA 564048 A CA564048 A CA 564048A CA 564048 A CA564048 A CA 564048A CA 564048D A CA564048D A CA 564048DA CA 564048 A CA564048 A CA 564048A
Authority
CA
Canada
Prior art keywords
compressors
axial flow
flow fans
fans
axial
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
CA564048A
Other languages
French (fr)
Inventor
A. Dean George
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
Publication date
Application granted granted Critical
Publication of CA564048A publication Critical patent/CA564048A/en
Expired legal-status Critical Current

Links

CA564048A Axial flow fans and compressors Expired CA564048A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA564048T

Publications (1)

Publication Number Publication Date
CA564048A true CA564048A (en) 1958-09-30

Family

ID=35736545

Family Applications (1)

Application Number Title Priority Date Filing Date
CA564048A Expired CA564048A (en) Axial flow fans and compressors

Country Status (1)

Country Link
CA (1) CA564048A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4492521A (en) * 1982-06-17 1985-01-08 Rolls-Royce Limited Sealed aerofoil blade/disc assembly for a rotor
US4878811A (en) * 1988-11-14 1989-11-07 United Technologies Corporation Axial compressor blade assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4492521A (en) * 1982-06-17 1985-01-08 Rolls-Royce Limited Sealed aerofoil blade/disc assembly for a rotor
US4878811A (en) * 1988-11-14 1989-11-07 United Technologies Corporation Axial compressor blade assembly

Similar Documents

Publication Publication Date Title
CA564048A (en) Axial flow fans and compressors
CA566698A (en) Centrifugal or radial flow fan impellers
CA564111A (en) Axial flow compressors
AU225569B2 (en) Improvements in axial flow fans
AU225195B2 (en) Improvements in axial flow fans
AU3458058A (en) Improvements in axial flow fans
AU3805658A (en) Improvements in axial flow fans
CA552760A (en) Centrifugal pumps and compressors
CA614179A (en) Axial flow compressors
CA566053A (en) Multi-stage axial flow compressor
CA554352A (en) Combined air exhauster and compressor
CA590294A (en) Axial-flow compressors and turbines
CA586468A (en) Axial flow compressors
CA576910A (en) Axial flow compressor
CA556346A (en) Ventilating fan assembly
CA567844A (en) Stator blade ring assemblies for axial flow compressors and the like
CA601515A (en) Axial flow compressors
CA632960A (en) Axial flow multi-stage compressors
CA551006A (en) Axial flow compressors
CA565244A (en) Air impeller and motor unit
CA592238A (en) Axial flow fan
CA560747A (en) Air compressors
AU223071B2 (en) Improvements in or relating to axial flow fans andthe like
CA553456A (en) Pumps or compressors
CA588895A (en) Combination fan and valve construction