GB774756A - - Google Patents
Info
- Publication number
- GB774756A GB774756A GB774756DA GB774756A GB 774756 A GB774756 A GB 774756A GB 774756D A GB774756D A GB 774756DA GB 774756 A GB774756 A GB 774756A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ejectors
- duct
- pulse
- air
- injectors
- 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.)
- Active
Links
- 239000007789 gas Substances 0.000 abstract 5
- 239000000446 fuel Substances 0.000 abstract 3
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 238000011144 upstream manufacturing Methods 0.000 abstract 2
- 238000000889 atomisation Methods 0.000 abstract 1
- 238000010276 construction Methods 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 230000000087 stabilizing effect Effects 0.000 abstract 1
Landscapes
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB774756A true GB774756A (enrdf_load_stackoverflow) |
Family
ID=1751899
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB774756D Active GB774756A (enrdf_load_stackoverflow) |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB774756A (enrdf_load_stackoverflow) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2416374A (en) * | 2004-07-21 | 2006-01-25 | Gen Electric | Ducted gas turbine engine with pulse detonation tube(s) |
| WO2017100922A1 (en) | 2015-12-17 | 2017-06-22 | ARLANXEO Canada Inc. | Process for epoxidation of unsaturated polymer |
-
0
- GB GB774756D patent/GB774756A/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2416374A (en) * | 2004-07-21 | 2006-01-25 | Gen Electric | Ducted gas turbine engine with pulse detonation tube(s) |
| US7228683B2 (en) | 2004-07-21 | 2007-06-12 | General Electric Company | Methods and apparatus for generating gas turbine engine thrust using a pulse detonator |
| GB2416374B (en) * | 2004-07-21 | 2009-04-01 | Gen Electric | Methods and apparatus for generating gas turbine engine thrust |
| WO2017100922A1 (en) | 2015-12-17 | 2017-06-22 | ARLANXEO Canada Inc. | Process for epoxidation of unsaturated polymer |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10641169B2 (en) | Hybrid combustor assembly and method of operation | |
| US6442930B1 (en) | Combined cycle pulse detonation turbine engine | |
| US7225623B2 (en) | Trapped vortex cavity afterburner | |
| GB757496A (en) | Improvements in arrangement for controlling the air-intake orifices of jet propulsion units | |
| US6666018B2 (en) | Combined cycle pulse detonation turbine engine | |
| US8677731B2 (en) | Hybrid slinger combustion system | |
| US7509797B2 (en) | Thrust vectoring missile turbojet | |
| US20040216463A1 (en) | Combustor system for an expendable gas turbine engine | |
| CN112902225A (zh) | 一种带外环旋转爆震增压燃烧室的多级加力燃烧室 | |
| US2712218A (en) | Gas turbine apparatus | |
| US5341640A (en) | Turbojet engine with afterburner and thrust augmentation ejectors | |
| EP2400221B1 (en) | Ejector purge of cavity adjacent exhaust flowpath | |
| CN116906212A (zh) | 用于高超音速飞行的联合循环推进系统 | |
| US6981366B2 (en) | Turbineless jet engine | |
| RU95108829A (ru) | Комбинированный прямоточный воздушно-реактивный двигатель | |
| GB774059A (en) | Improvements in or relating to combined gas turbine plant and ram-jet units | |
| US8991189B2 (en) | Side-initiated augmentor for engine applications | |
| GB774756A (enrdf_load_stackoverflow) | ||
| GB805418A (en) | Jet propulsion plant | |
| US12442331B2 (en) | High shear fuel distributor | |
| US4896501A (en) | Turbojet engine with sonic injection afterburner | |
| JPH0672575B2 (ja) | ターボラムロケット結合の推進機関のためのガス噴射装置 | |
| GB861095A (en) | A ram-jet unit | |
| US2840986A (en) | After-burner fuel supply system for gas-turbine engines | |
| CN114109650A (zh) | 一种整体式液体火箭冲压组合动力装置 |