GB777694A - Improvements relating to internal combustion turbines in combination with ram-jet engines - Google Patents

Improvements relating to internal combustion turbines in combination with ram-jet engines

Info

Publication number
GB777694A
GB777694A GB951052A GB951052A GB777694A GB 777694 A GB777694 A GB 777694A GB 951052 A GB951052 A GB 951052A GB 951052 A GB951052 A GB 951052A GB 777694 A GB777694 A GB 777694A
Authority
GB
United Kingdom
Prior art keywords
jet
turbine
ram
compressor
icing
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
GB951052A
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 GB951052A priority Critical patent/GB777694A/en
Publication of GB777694A publication Critical patent/GB777694A/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines

Abstract

777,694. Gas turbine jet propulsion plant. SHARMA, D. N. April 16, 1953 [April 16, 1952], No. 9510/52. Class 110 (3). [Also in Group XII] In a jet power plant, having a turbo-jet and a ram-jet duct in combination, ambient air is introduced along the length of the frame following the turbine section. As shown, ambient air is admitted to section 5A, 6A through such apertures as 38, 39 under control of flaps 41, 43, 45, 46, 47, 48. In addition to the intake of air through the compressor 10, 11, air is also urged through the hollow interior of the compressor, past the spokes 15 by the pump 24, 25. For de-icing purposes, hot gases from the turbine pass forward through the hollow shaft 26 to the de-icing hood 28. Gases from the turbine pass through 5A into the after burner 6A. Additional fuel is admitted at 49 and through nozzles 56, 57, fired by a burner 50 and discharged through the ram-jet section 7A under the control of the adjustable shutters 8A. In a further embodiment, not shown, de-icing is effected by moving hot gas from the turbine both to the deicing hood and to the front sections of the compressor spider. Specifications 655,871, 693,682, 706,841 and 737,081 are referred to in the Provisional Specification.
GB951052A 1952-04-16 1952-04-16 Improvements relating to internal combustion turbines in combination with ram-jet engines Expired GB777694A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB951052A GB777694A (en) 1952-04-16 1952-04-16 Improvements relating to internal combustion turbines in combination with ram-jet engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB951052A GB777694A (en) 1952-04-16 1952-04-16 Improvements relating to internal combustion turbines in combination with ram-jet engines

Publications (1)

Publication Number Publication Date
GB777694A true GB777694A (en) 1957-06-26

Family

ID=9873353

Family Applications (1)

Application Number Title Priority Date Filing Date
GB951052A Expired GB777694A (en) 1952-04-16 1952-04-16 Improvements relating to internal combustion turbines in combination with ram-jet engines

Country Status (1)

Country Link
GB (1) GB777694A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2389772A1 (en) * 1977-05-05 1978-12-01 Mordellet Roger Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream
FR2605679A1 (en) * 1986-10-24 1988-04-29 Culica Georges Francois Multi-spool multi-bypass turbo jet engine with a drum rotor
GB2231092A (en) * 1989-02-08 1990-11-07 Mtu Muenchen Gmbh Jet engine
WO2011078740A1 (en) * 2009-12-24 2011-06-30 Shvedov Vladimir Tarasovich Method for generating thrust for a vehicle
US10087840B2 (en) 2013-04-03 2018-10-02 United Technologies Corporation Gas turbine engine de-icing system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2389772A1 (en) * 1977-05-05 1978-12-01 Mordellet Roger Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream
FR2605679A1 (en) * 1986-10-24 1988-04-29 Culica Georges Francois Multi-spool multi-bypass turbo jet engine with a drum rotor
GB2231092A (en) * 1989-02-08 1990-11-07 Mtu Muenchen Gmbh Jet engine
WO2011078740A1 (en) * 2009-12-24 2011-06-30 Shvedov Vladimir Tarasovich Method for generating thrust for a vehicle
US10087840B2 (en) 2013-04-03 2018-10-02 United Technologies Corporation Gas turbine engine de-icing system
US10815884B2 (en) 2013-04-03 2020-10-27 Raytheon Technologies Corporation Gas turbine engine de-icing system

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