ES175320A1 - Una instalación de turbina de combustión interna - Google Patents

Una instalación de turbina de combustión interna

Info

Publication number
ES175320A1
ES175320A1 ES175320A ES175320A ES175320A1 ES 175320 A1 ES175320 A1 ES 175320A1 ES 175320 A ES175320 A ES 175320A ES 175320 A ES175320 A ES 175320A ES 175320 A1 ES175320 A1 ES 175320A1
Authority
ES
Spain
Prior art keywords
internal combustion
combustion turbine
turbine installation
installation
internal
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
ES175320A
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical Co Ltd
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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Publication of ES175320A1 publication Critical patent/ES175320A1/es
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
    • F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
ES175320A 1943-08-11 1946-10-17 Una instalación de turbina de combustión interna Expired ES175320A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13027/43A GB586572A (en) 1943-08-11 1943-08-11 Improvements in internal combustion turbine plant for propulsion by jet action, at least in part

Publications (1)

Publication Number Publication Date
ES175320A1 true ES175320A1 (es) 1946-11-16

Family

ID=10015467

Family Applications (1)

Application Number Title Priority Date Filing Date
ES175320A Expired ES175320A1 (es) 1943-08-11 1946-10-17 Una instalación de turbina de combustión interna

Country Status (2)

Country Link
ES (1) ES175320A1 (es)
GB (1) GB586572A (es)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB622627A (en) * 1947-04-02 1949-05-04 Armstrong Siddeley Motors Ltd Means for preventing an internal-combustion turbine unit from icing
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2577919A (en) * 1947-07-22 1951-12-11 Snecma Association on flying machine of compressor-jet units with ramjet units
US2526941A (en) * 1948-06-10 1950-10-24 Northrop Aircraft Inc Gas turbine system for aircraft propulsion
US2687779A (en) * 1949-01-31 1954-08-31 Adolphe C Peterson Combined propulsion and rotary wing sustentation unit for aircraft
US2628474A (en) * 1949-05-13 1953-02-17 Floyd T Hague Annular combustion liner having conical reentrant walls with fuel reversing elements
US2679725A (en) * 1949-07-15 1954-06-01 Sharma Devendra Nath Exhaust effusion turbine jet propulsion power unit
US2658334A (en) * 1950-03-25 1953-11-10 Bristol Aeroplane Co Ltd Braking aircraft
US2781634A (en) * 1950-11-01 1957-02-19 Curtiss Wright Corp Compressor flow control means
US2823516A (en) * 1951-10-30 1958-02-18 Garrett Corp Ducted fan power plant for aircraft
US2920843A (en) * 1956-06-18 1960-01-12 Curtiss Wright Corp Turbo-jet boost augmenter
DE1153943B (de) * 1958-10-10 1963-09-05 Bmw Triebwerkbau Ges M B H Gasturbinenstrahltriebwerk in Zweikreisbauart
US3009318A (en) * 1960-04-22 1961-11-21 Ryan Aeronautical Co Turbofan engine with reversible pitch fan
US3387457A (en) * 1965-03-01 1968-06-11 George H. Garraway Combined turbojet and turboprop engine
FR1520460A (fr) * 1967-01-11 1968-04-12 Snecma Perfectionnements aux turboréacteurs à flux multiples
US6442930B1 (en) * 2000-03-31 2002-09-03 General Electric Company Combined cycle pulse detonation turbine engine

Also Published As

Publication number Publication date
GB586572A (en) 1947-03-24

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