GB757818A - Improvements relating to turbojet propulsion power units - Google Patents

Improvements relating to turbojet propulsion power units

Info

Publication number
GB757818A
GB757818A GB1001154A GB1001154A GB757818A GB 757818 A GB757818 A GB 757818A GB 1001154 A GB1001154 A GB 1001154A GB 1001154 A GB1001154 A GB 1001154A GB 757818 A GB757818 A GB 757818A
Authority
GB
United Kingdom
Prior art keywords
compressor
turbine
passes
burners
engine
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
GB1001154A
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.)
DEVENDRA NATH SHARMA
Original Assignee
DEVENDRA NATH SHARMA
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 DEVENDRA NATH SHARMA filed Critical DEVENDRA NATH SHARMA
Priority to GB1001154A priority Critical patent/GB757818A/en
Publication of GB757818A publication Critical patent/GB757818A/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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

757,818. Gas turbine jet propulsion plant. SHARMA, D. N. April 6th, 1954, No. 10011/54. Addition to 706,841. Class 110(3) A jet propulsion gas turbine engine has a compressor the discharge of which passes into two paths which lead to an axial common exhaust, one path supplies compressed air to burners and the second path passes along the axis of the turbine and includes further burners. The engine shown comprises an axial flow compressor 5, 6, feeding a combustion chamber 18 supplying combustion gases to a turbine 19, 20 driving the compressor through a universal joint 17. A part of the air discharged from the compressor passes through the channels A, B, and acts on turbine blades. 25. Fuel supplied through burners or heat generating sources 23 heat this air before it passes to the exhaust pipe 24. Shutters. 16 are provided to shut off the intake of the compressor in the event of engine failure. The compressor may be of any type. The turbine may drive a propeller through reduction gearing. Atomic energy may be used for heat generation.
GB1001154A 1954-04-06 1954-04-06 Improvements relating to turbojet propulsion power units Expired GB757818A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1001154A GB757818A (en) 1954-04-06 1954-04-06 Improvements relating to turbojet propulsion power units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1001154A GB757818A (en) 1954-04-06 1954-04-06 Improvements relating to turbojet propulsion power units

Publications (1)

Publication Number Publication Date
GB757818A true GB757818A (en) 1956-09-26

Family

ID=9959755

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1001154A Expired GB757818A (en) 1954-04-06 1954-04-06 Improvements relating to turbojet propulsion power units

Country Status (1)

Country Link
GB (1) GB757818A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2289504A (en) * 1994-05-11 1995-11-22 British Aerospace Gas turbine propulsion unit
GB2425572A (en) * 2005-04-29 2006-11-01 Gen Electric Gas turbine starter-generator
US7424805B2 (en) 2005-04-29 2008-09-16 General Electric Company Supersonic missile turbojet engine
US7475545B2 (en) 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
US7509797B2 (en) 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2289504A (en) * 1994-05-11 1995-11-22 British Aerospace Gas turbine propulsion unit
GB2289504B (en) * 1994-05-11 1998-01-14 British Aerospace Gas turbine propulsion unit
GB2425572A (en) * 2005-04-29 2006-11-01 Gen Electric Gas turbine starter-generator
US7424805B2 (en) 2005-04-29 2008-09-16 General Electric Company Supersonic missile turbojet engine
US7448199B2 (en) 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
US7475545B2 (en) 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
US7509797B2 (en) 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
GB2425572B (en) * 2005-04-29 2010-06-30 Gen Electric Self powered missile turbojet

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