GB885908A - Improvements in intakes for compressible fluids - Google Patents

Improvements in intakes for compressible fluids

Info

Publication number
GB885908A
GB885908A GB2747057A GB2747057A GB885908A GB 885908 A GB885908 A GB 885908A GB 2747057 A GB2747057 A GB 2747057A GB 2747057 A GB2747057 A GB 2747057A GB 885908 A GB885908 A GB 885908A
Authority
GB
United Kingdom
Prior art keywords
fuel
combustion zone
combustion
air
mixed
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
GB2747057A
Inventor
Raymond Frederick Sargent
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines 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 Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Priority to GB2747057A priority Critical patent/GB885908A/en
Publication of GB885908A publication Critical patent/GB885908A/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
    • 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

Abstract

885,908. Generating combustion products under pressure. BRISTOL SIDDELEY ENGINES Ltd. Sept. 1, 1958 [Aug. 30, 1957; Dec. 3, 1957], Nos. 27470/57 and 37701/57. Class 51(1). [Also in Group XXVI] Combustion equipment for a ram jet comprises a flame tube 26 forming a pilot combustion zone 27 at its upstream end into which fuel is discharged through a sprayer 28 mixed with air entering through swirl vanes 29 Further fuel is sprayed into the main duct through sprayers 30, the fuel, mixed with air, passing through holes in the flame tube and being maintained in combustion by the pilot combustion zone. An additional intake may be provided in the ram jet to convey air to the pilot combustion zone so that conditions therein are independent of those in the main duct. Specification 762,179 is referred to.
GB2747057A 1957-08-30 1957-08-30 Improvements in intakes for compressible fluids Expired GB885908A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2747057A GB885908A (en) 1957-08-30 1957-08-30 Improvements in intakes for compressible fluids

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2747057A GB885908A (en) 1957-08-30 1957-08-30 Improvements in intakes for compressible fluids

Publications (1)

Publication Number Publication Date
GB885908A true GB885908A (en) 1962-01-03

Family

ID=10260118

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2747057A Expired GB885908A (en) 1957-08-30 1957-08-30 Improvements in intakes for compressible fluids

Country Status (1)

Country Link
GB (1) GB885908A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2212532A2 (en) * 2007-10-24 2010-08-04 Gulfstream Aerospace Corporation Low shock strength inlet
WO2022073889A1 (en) 2020-10-08 2022-04-14 Safran Nacelles Supersonic air intake of an aircraft propulsion assembly comprising a device for de-icing the support arms and de-icing method
US11396888B1 (en) 2017-11-09 2022-07-26 Williams International Co., L.L.C. System and method for guiding compressible gas flowing through a duct
WO2024022304A1 (en) * 2022-07-26 2024-02-01 中国航发商用航空发动机有限责任公司 Inlet cone and aeroengine comprising same

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2212532A2 (en) * 2007-10-24 2010-08-04 Gulfstream Aerospace Corporation Low shock strength inlet
EP2212532A4 (en) * 2007-10-24 2012-10-24 Gulfstream Aerospace Corp Low shock strength inlet
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
US8739514B2 (en) 2007-10-24 2014-06-03 Gulfstream Aerospace Corporation Low shock strength propulsion system
US8783039B2 (en) 2007-10-24 2014-07-22 Gulfstream Aerospace Corporation Low shock strength propulsion system
US11396888B1 (en) 2017-11-09 2022-07-26 Williams International Co., L.L.C. System and method for guiding compressible gas flowing through a duct
WO2022073889A1 (en) 2020-10-08 2022-04-14 Safran Nacelles Supersonic air intake of an aircraft propulsion assembly comprising a device for de-icing the support arms and de-icing method
FR3115070A1 (en) * 2020-10-08 2022-04-15 Safran Nacelles Supersonic air intake of an aircraft propulsion system comprising a device for de-icing the support arms and method for de-icing
WO2024022304A1 (en) * 2022-07-26 2024-02-01 中国航发商用航空发动机有限责任公司 Inlet cone and aeroengine comprising same

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