FR1238508A - Dual aerodynamic profile for turbo-augmentator rotor - Google Patents

Dual aerodynamic profile for turbo-augmentator rotor

Info

Publication number
FR1238508A
FR1238508A FR804209A FR804209A FR1238508A FR 1238508 A FR1238508 A FR 1238508A FR 804209 A FR804209 A FR 804209A FR 804209 A FR804209 A FR 804209A FR 1238508 A FR1238508 A FR 1238508A
Authority
FR
France
Prior art keywords
augmentator
turbo
rotor
dual
aerodynamic profile
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
FR804209A
Other languages
French (fr)
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of FR1238508A publication Critical patent/FR1238508A/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
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR804209A 1958-09-05 1959-09-03 Dual aerodynamic profile for turbo-augmentator rotor Expired FR1238508A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1238508XA 1958-09-05 1958-09-05

Publications (1)

Publication Number Publication Date
FR1238508A true FR1238508A (en) 1960-08-12

Family

ID=22411262

Family Applications (1)

Application Number Title Priority Date Filing Date
FR804209A Expired FR1238508A (en) 1958-09-05 1959-09-03 Dual aerodynamic profile for turbo-augmentator rotor

Country Status (1)

Country Link
FR (1) FR1238508A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1182474B (en) * 1961-10-25 1964-11-26 Siemens Ag Disk-type gas turbine with intermediate rings supporting the clamped disks against each other and blade root cooling by a gaseous medium
DE1185415B (en) * 1962-02-03 1965-01-14 Gasturbinenbau Und Energiemasc Device for cooling turbine disks of a gas turbine
DE1195605B (en) * 1963-03-14 1965-06-24 Ver Flugtechnische Werke Ges M Jet engine with a downstream two-circuit set
DE1256483B (en) * 1963-12-03 1967-12-14 Rolls Royce Gas turbine jet engine
FR2660256A1 (en) * 1990-03-28 1991-10-04 Ogor Joseph Nozzle (jet pipe) with a turbine (fan) for propelling motor vehicles

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1182474B (en) * 1961-10-25 1964-11-26 Siemens Ag Disk-type gas turbine with intermediate rings supporting the clamped disks against each other and blade root cooling by a gaseous medium
DE1185415B (en) * 1962-02-03 1965-01-14 Gasturbinenbau Und Energiemasc Device for cooling turbine disks of a gas turbine
DE1195605B (en) * 1963-03-14 1965-06-24 Ver Flugtechnische Werke Ges M Jet engine with a downstream two-circuit set
DE1256483B (en) * 1963-12-03 1967-12-14 Rolls Royce Gas turbine jet engine
FR2660256A1 (en) * 1990-03-28 1991-10-04 Ogor Joseph Nozzle (jet pipe) with a turbine (fan) for propelling motor vehicles

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