FR1274193A - Turbo-moteur à gaz - Google Patents

Turbo-moteur à gaz

Info

Publication number
FR1274193A
FR1274193A FR844900A FR844900A FR1274193A FR 1274193 A FR1274193 A FR 1274193A FR 844900 A FR844900 A FR 844900A FR 844900 A FR844900 A FR 844900A FR 1274193 A FR1274193 A FR 1274193A
Authority
FR
France
Prior art keywords
turbo engine
gas turbo
engine
gas
turbo
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
FR844900A
Other languages
English (en)
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
Priority claimed from GB40278/59A external-priority patent/GB895075A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR844900A priority Critical patent/FR1274193A/fr
Application granted granted Critical
Publication of FR1274193A publication Critical patent/FR1274193A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/062—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with aft fan
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR844900A 1959-11-26 1960-11-24 Turbo-moteur à gaz Expired FR1274193A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR844900A FR1274193A (fr) 1959-11-26 1960-11-24 Turbo-moteur à gaz

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB40278/59A GB895075A (en) 1959-11-26 1959-11-26 Turbine driven fan unit
FR844900A FR1274193A (fr) 1959-11-26 1960-11-24 Turbo-moteur à gaz

Publications (1)

Publication Number Publication Date
FR1274193A true FR1274193A (fr) 1961-10-20

Family

ID=26188279

Family Applications (1)

Application Number Title Priority Date Filing Date
FR844900A Expired FR1274193A (fr) 1959-11-26 1960-11-24 Turbo-moteur à gaz

Country Status (1)

Country Link
FR (1) FR1274193A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1301650B (de) * 1965-01-30 1969-08-21 Rolls Royce Mantelstromgasturbinenstrahltriebwerk

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1301650B (de) * 1965-01-30 1969-08-21 Rolls Royce Mantelstromgasturbinenstrahltriebwerk

Similar Documents

Publication Publication Date Title
FR1382232A (fr) Perfectionnements apportés aux moteurs à turbine à gaz
FR1203751A (fr) Perfectionnements aux moteurs à turbine à gaz
FR1227773A (fr) Ailettes de turbomoteurs à gaz
FR1262452A (fr) Grupe propulseur à turbine à gaz
FR1217966A (fr) Moteur à turbine à gaz
FR1203774A (fr) Perfectionnements aux moteurs à turbine à gaz
BE589863A (fr) Perfectionnements aux turbo-moteurs à gaz
BE592008A (fr) Perfectionnements aux moteurs à turbine à gaz.
FR1185339A (fr) Moteur à turbine à gaz
CH367662A (fr) Groupe à turbine à gaz
FR1218064A (fr) Perfectionnements aux moteurs à turbine à gaz
FR1259348A (fr) Perfectionnements aux moteurs à turbine à gaz
FR1247159A (fr) Brûleur à gaz
FR1285627A (fr) Groupe moteur à turbine à gaz
FR1303779A (fr) Turbine à gaz
FR1288601A (fr) Turbo-moteur à gaz
FR1276261A (fr) Turbine à gaz
FR1242634A (fr) Turboréacteur à gaz
FR1274193A (fr) Turbo-moteur à gaz
FR1286534A (fr) Turbine à gaz du type axial
FR1272447A (fr) Groupe moteur à turbine à gaz
BE589882A (fr) Compresseur de gaz
FR1254871A (fr) Robinet-fiche de raccordement à gaz
FR1197393A (fr) Moteur à turbine à gaz
FR1254175A (fr) Perfectionnements aux moteurs à turbine à gaz