[go: up one dir, main page]

CA556217A - Preventing or reducing stalling of the early rows of axial-flow compressor blades of gas turbine engines - Google Patents

Preventing or reducing stalling of the early rows of axial-flow compressor blades of gas turbine engines

Info

Publication number
CA556217A
CA556217A CA556217A CA556217DA CA556217A CA 556217 A CA556217 A CA 556217A CA 556217 A CA556217 A CA 556217A CA 556217D A CA556217D A CA 556217DA CA 556217 A CA556217 A CA 556217A
Authority
CA
Canada
Prior art keywords
axial
preventing
gas turbine
turbine engines
compressor blades
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
CA556217A
Other languages
French (fr)
Inventor
Thomas Albert
Marlow John
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors Ltd
Publication date
Application granted granted Critical
Publication of CA556217A publication Critical patent/CA556217A/en
Expired legal-status Critical Current

Links

CA556217A Preventing or reducing stalling of the early rows of axial-flow compressor blades of gas turbine engines Expired CA556217A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA556217T

Publications (1)

Publication Number Publication Date
CA556217A true CA556217A (en) 1958-04-22

Family

ID=35722624

Family Applications (1)

Application Number Title Priority Date Filing Date
CA556217A Expired CA556217A (en) Preventing or reducing stalling of the early rows of axial-flow compressor blades of gas turbine engines

Country Status (1)

Country Link
CA (1) CA556217A (en)

Similar Documents

Publication Publication Date Title
CA556217A (en) Preventing or reducing stalling of the early rows of axial-flow compressor blades of gas turbine engines
AU206974B2 (en) Preventing or reducing stalling ofthe early rows of axial-flow compressor blades of gas turbine engines
AU572954A (en) Preventing or reducing stalling ofthe early rows of axial-flow compressor blades of gas turbine engines
CA611142A (en) Gas turbine engines
CA593841A (en) Shroud ring construction for turbines and compressors
CA577325A (en) Centrifugal compressor for a gas turbine engine
CA584125A (en) Blading for gas turbine engines
CA563822A (en) Plastic blades, particularly for a compressor rotor of a gas turbine engine
AU224140B2 (en) Improvements relating to turbine and compressor blades
CA562449A (en) Shroud assembly for gas turbine engines
CA523055A (en) Gas turbine jet engine
CA563511A (en) Axial flow compressors and gas turbine engines including such compressors
CA590522A (en) Gas turbine engines
CA604077A (en) Plastic axial-flow compressor for gas turbines
AU3529258A (en) Improvements relating to turbine and compressor blades
CA525007A (en) Gas turbine engines
CA533550A (en) Gas turbine engines
CA578623A (en) Stator structures for turbines or compressors of gas-turbine engines
CA557897A (en) Gas turbine engines
CA560126A (en) Gas turbine engines
CA559069A (en) Gas turbine engines
CA562157A (en) Gas turbine engines
CA567818A (en) Gas turbine engines
CA515286A (en) Locking arrangement for blading of axial-flow turbines and compressors
CA591548A (en) Compressor pressure limiter for gas turbine engines