GB0525365D0 - The hypersonic ram/scramjet - Google Patents
The hypersonic ram/scramjetInfo
- Publication number
- GB0525365D0 GB0525365D0 GBGB0525365.3A GB0525365A GB0525365D0 GB 0525365 D0 GB0525365 D0 GB 0525365D0 GB 0525365 A GB0525365 A GB 0525365A GB 0525365 D0 GB0525365 D0 GB 0525365D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- scramjet
- hypersonic
- ram
- hypersonic ram
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
-
- 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
- F02K7/12—Injection-induction jet engines
-
- 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
- F02K7/14—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 with external combustion, e.g. scram-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/51—Inlet
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0524265.6A GB0524265D0 (en) | 2005-11-29 | 2005-11-29 | The hypersonic ram/scramjet |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0525365D0 true GB0525365D0 (en) | 2006-01-18 |
GB2432887A GB2432887A (en) | 2007-06-06 |
GB2432887B GB2432887B (en) | 2009-05-20 |
Family
ID=35601414
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB0524265.6A Ceased GB0524265D0 (en) | 2005-11-29 | 2005-11-29 | The hypersonic ram/scramjet |
GB0525365A Active GB2432887B (en) | 2005-11-29 | 2005-12-13 | The hypersonic ram/scramjet |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB0524265.6A Ceased GB0524265D0 (en) | 2005-11-29 | 2005-11-29 | The hypersonic ram/scramjet |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB0524265D0 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2483643A (en) * | 2010-09-14 | 2012-03-21 | Stephen Desmond Lewis | A cooled afterburner |
GB201503540D0 (en) * | 2015-02-28 | 2015-04-15 | Lewis Stephen D | Pre-cooling for aerospace engines |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3357191A (en) * | 1964-10-20 | 1967-12-12 | Berner Felix | Propulsion means |
JPH08312462A (en) * | 1995-05-16 | 1996-11-26 | Ishikawajima Harima Heavy Ind Co Ltd | Bypass channel variable nozzle for supersonic aircraft |
US6907724B2 (en) * | 2002-09-13 | 2005-06-21 | The Boeing Company | Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance |
-
2005
- 2005-11-29 GB GBGB0524265.6A patent/GB0524265D0/en not_active Ceased
- 2005-12-13 GB GB0525365A patent/GB2432887B/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB2432887A (en) | 2007-06-06 |
GB0524265D0 (en) | 2006-01-04 |
GB2432887B (en) | 2009-05-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
746 | Register noted 'licences of right' (sect. 46/1977) |
Effective date: 20091113 |