RU2012102839A - HYBRID DOUBLE GAS TURBINE ENGINE - Google Patents
HYBRID DOUBLE GAS TURBINE ENGINE Download PDFInfo
- Publication number
- RU2012102839A RU2012102839A RU2012102839/06A RU2012102839A RU2012102839A RU 2012102839 A RU2012102839 A RU 2012102839A RU 2012102839/06 A RU2012102839/06 A RU 2012102839/06A RU 2012102839 A RU2012102839 A RU 2012102839A RU 2012102839 A RU2012102839 A RU 2012102839A
- Authority
- RU
- Russia
- Prior art keywords
- turbine
- gas turbine
- air
- sent
- hybrid double
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 239000000203 mixture Substances 0.000 claims abstract 6
- 238000002485 combustion reaction Methods 0.000 claims abstract 2
- 239000012530 fluid Substances 0.000 claims abstract 2
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Гибридный двойной газотурбинный двигатель является аналогом воздушно-реактивного двигателя и газовой турбины, и представляет из себя турбину в турбине, расположенную соосно, главным отличием которого является то, что воздух (рабочее тело) в конфузорной части не сжимается, а разгоняется и направляется в сопла, где установлена или установлены камера сгорания и где полученная воздушная смесь или смеси расширяются и смешиваются между собой и направляются на лопатки ротора, на одном валу с которым может быть установлена дополнительная турбина или генератор.A hybrid double gas turbine engine is an analogue of an air-jet engine and a gas turbine, and is a turbine in a turbine located coaxially, the main difference of which is that the air (working fluid) in the confuser part is not compressed, but accelerated and sent to the nozzles, where the combustion chamber is installed or installed and where the resulting air mixture or mixtures expand and mix with each other and are sent to the rotor blades, on the same shaft with which an additional turbine can be installed on or generator.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012102839/06A RU2497004C2 (en) | 2012-01-24 | 2012-01-24 | Hybrid twin gas turbine engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012102839/06A RU2497004C2 (en) | 2012-01-24 | 2012-01-24 | Hybrid twin gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2012102839A true RU2012102839A (en) | 2013-07-27 |
| RU2497004C2 RU2497004C2 (en) | 2013-10-27 |
Family
ID=49155481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012102839/06A RU2497004C2 (en) | 2012-01-24 | 2012-01-24 | Hybrid twin gas turbine engine |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2497004C2 (en) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB573399A (en) * | 1941-01-22 | 1945-11-20 | Frank Bernard Halford | Improvements in or relating to aircraft propulsion |
| SU956351A1 (en) * | 1979-05-10 | 1982-09-07 | Предприятие П/Я М-5147 | Water-jet propeller ejection device |
| RU2024796C1 (en) * | 1991-01-09 | 1994-12-15 | Вадим Николаевич Пикуль | Two-dimensional pulse gas generator |
| RU2009148052A (en) * | 2009-12-24 | 2011-06-27 | Владимир Тарасович Шведов (RU) | METHOD FOR CRAWLING FOR A VEHICLE INTENDED FOR MOVEMENT IN A FLUID |
| RU109233U1 (en) * | 2011-03-23 | 2011-10-10 | Борис Андреевич Шахов | TURBINE |
-
2012
- 2012-01-24 RU RU2012102839/06A patent/RU2497004C2/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2497004C2 (en) | 2013-10-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20140125 |