GB885908A - Improvements in intakes for compressible fluids - Google Patents
Improvements in intakes for compressible fluidsInfo
- 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
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
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.
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)
| 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 |
-
1957
- 1957-08-30 GB GB2747057A patent/GB885908A/en not_active Expired
Cited By (10)
| 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 |
| US12037940B2 (en) | 2020-10-08 | 2024-07-16 | Safran Nacelles | Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing method |
| 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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