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GB1546783A - Axial flow compressor for a gas turbine engine - Google Patents

Axial flow compressor for a gas turbine engine

Info

Publication number
GB1546783A
GB1546783A GB1673675A GB1673675A GB1546783A GB 1546783 A GB1546783 A GB 1546783A GB 1673675 A GB1673675 A GB 1673675A GB 1673675 A GB1673675 A GB 1673675A GB 1546783 A GB1546783 A GB 1546783A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
axial flow
flow compressor
compressor
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
GB1673675A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB1673675A priority Critical patent/GB1546783A/en
Publication of GB1546783A publication Critical patent/GB1546783A/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GB1673675A 1976-04-22 1976-04-22 Axial flow compressor for a gas turbine engine Expired GB1546783A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1673675A GB1546783A (en) 1976-04-22 1976-04-22 Axial flow compressor for a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1673675A GB1546783A (en) 1976-04-22 1976-04-22 Axial flow compressor for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1546783A true GB1546783A (en) 1979-05-31

Family

ID=10082740

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1673675A Expired GB1546783A (en) 1976-04-22 1976-04-22 Axial flow compressor for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB1546783A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4310286A (en) * 1979-05-17 1982-01-12 United Technologies Corporation Rotor assembly having a multistage disk
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4310286A (en) * 1979-05-17 1982-01-12 United Technologies Corporation Rotor assembly having a multistage disk
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee