GB586572A - Improvements in internal combustion turbine plant for propulsion by jet action, at least in part - Google Patents

Improvements in internal combustion turbine plant for propulsion by jet action, at least in part

Info

Publication number
GB586572A
GB586572A GB13027/43A GB1302743A GB586572A GB 586572 A GB586572 A GB 586572A GB 13027/43 A GB13027/43 A GB 13027/43A GB 1302743 A GB1302743 A GB 1302743A GB 586572 A GB586572 A GB 586572A
Authority
GB
United Kingdom
Prior art keywords
jet
compressor
propulsion
unit
auxiliary unit
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
GB13027/43A
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
Priority to GB13027/43A priority Critical patent/GB586572A/en
Priority to ES175320A priority patent/ES175320A1/en
Publication of GB586572A publication Critical patent/GB586572A/en
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)

Abstract

586,572. Gas turbines. SMITH, D. M., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Aug. 11, 1943, No. 13027. [Class 110 (iii)] An auxiliary or augmentor jet AJ is energized by a combustion chamber Ca Ca which receives air from the compressor of the main jet-propulsion unit. The air may be taken from the H.P. end of the compressor or from an intermediate point. The auxiliary unit may include a twotiered jet augmentor with turbine blades ACT and compressor blades D, F. The auxiliary unit may have a compressor which further compresses the air received from the main unit and is driven by a turbine wheel separate from the jetaugmentor. An auxiliary unit without a jetaugmentor has a turbine which drives an airscrew. Another auxiliary unit consists only of a combustion chamber and a jet. Specification 586,551 is referred to.
GB13027/43A 1943-08-11 1943-08-11 Improvements in internal combustion turbine plant for propulsion by jet action, at least in part Expired GB586572A (en)

Priority Applications (2)

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
ES175320A ES175320A1 (en) 1943-08-11 1946-10-17 AN INTERNAL COMBUSTION TURBINE INSTALLATION

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
GB586572A true GB586572A (en) 1947-03-24

Family

ID=10015467

Family Applications (1)

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

Country Status (2)

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

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526941A (en) * 1948-06-10 1950-10-24 Northrop Aircraft Inc Gas turbine system for aircraft propulsion
US2577919A (en) * 1947-07-22 1951-12-11 Snecma Association on flying machine of compressor-jet units with ramjet units
US2625010A (en) * 1947-04-02 1953-01-13 Armstrong Siddeley Motors Ltd Means for preventing internal-combustion turbine units from icing
US2628474A (en) * 1949-05-13 1953-02-17 Floyd T Hague Annular combustion liner having conical reentrant walls with fuel reversing elements
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2658334A (en) * 1950-03-25 1953-11-10 Bristol Aeroplane Co Ltd Braking aircraft
US2679725A (en) * 1949-07-15 1954-06-01 Sharma Devendra Nath Exhaust effusion turbine jet propulsion power unit
US2687779A (en) * 1949-01-31 1954-08-31 Adolphe C Peterson Combined propulsion and rotary wing sustentation unit for 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
US3009318A (en) * 1960-04-22 1961-11-21 Ryan Aeronautical Co Turbofan engine with reversible pitch fan
DE1153943B (en) * 1958-10-10 1963-09-05 Bmw Triebwerkbau Ges M B H Gas turbine jet engine in two-circuit design
US3387457A (en) * 1965-03-01 1968-06-11 George H. Garraway Combined turbojet and turboprop engine
US3486328A (en) * 1967-01-11 1969-12-30 Snecma Multiflow turbojet engine
JP2001355515A (en) * 2000-03-31 2001-12-26 General Electric Co <Ge> Combined cycle pulse detonation turbine engine

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2625010A (en) * 1947-04-02 1953-01-13 Armstrong Siddeley Motors Ltd Means for preventing internal-combustion turbine units 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 (en) * 1958-10-10 1963-09-05 Bmw Triebwerkbau Ges M B H Gas turbine jet engine in two-circuit design
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
US3486328A (en) * 1967-01-11 1969-12-30 Snecma Multiflow turbojet engine
JP2001355515A (en) * 2000-03-31 2001-12-26 General Electric Co <Ge> Combined cycle pulse detonation turbine engine
JP4705727B2 (en) * 2000-03-31 2011-06-22 ゼネラル・エレクトリック・カンパニイ Combined cycle pulse detonation turbine engine

Also Published As

Publication number Publication date
ES175320A1 (en) 1946-11-16

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