RU2006114247A - METHOD FOR GAS-TURBINE ENGINE CONTROL - Google Patents
METHOD FOR GAS-TURBINE ENGINE CONTROL Download PDFInfo
- Publication number
- RU2006114247A RU2006114247A RU2006114247/06A RU2006114247A RU2006114247A RU 2006114247 A RU2006114247 A RU 2006114247A RU 2006114247/06 A RU2006114247/06 A RU 2006114247/06A RU 2006114247 A RU2006114247 A RU 2006114247A RU 2006114247 A RU2006114247 A RU 2006114247A
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- RU
- Russia
- Prior art keywords
- engine
- value
- pressure
- inlet
- air
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- Feedback Control In General (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2006114247/06A RU2319025C1 (en) | 2006-04-27 | 2006-04-27 | Gas-turbine engine control method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2006114247/06A RU2319025C1 (en) | 2006-04-27 | 2006-04-27 | Gas-turbine engine control method |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2006114247A true RU2006114247A (en) | 2007-12-10 |
RU2319025C1 RU2319025C1 (en) | 2008-03-10 |
Family
ID=38903124
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2006114247/06A RU2319025C1 (en) | 2006-04-27 | 2006-04-27 | Gas-turbine engine control method |
Country Status (1)
Country | Link |
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RU (1) | RU2319025C1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2446300C1 (en) * | 2010-10-27 | 2012-03-27 | Федеральное государственное унитарное предприятие "Научно-производственный центр газотурбостроения "Салют" (ФГУП "НПЦ газотурбостроения "Салют") | Method of controlling low-pressure rotor rpm in bypass gas turbine engine |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITCO20110028A1 (en) * | 2011-07-21 | 2013-01-22 | Nuovo Pignone Spa | SYSTEM AND METHOD FOR THE SELF-ADJUSTMENT OF A GAS TURBINE COMBUSTION SYSTEM |
RU2501964C1 (en) * | 2012-04-27 | 2013-12-20 | Открытое акционерное общество "Концерн Кизлярский электромеханический завод" (ОАО "Концерн КЭМЗ") | System of gas turbine engine control |
RU2623707C1 (en) * | 2016-09-07 | 2017-06-28 | Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") | Method for controlling aircraft turbojet engine with afterburner combustion |
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2006
- 2006-04-27 RU RU2006114247/06A patent/RU2319025C1/en not_active IP Right Cessation
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2446300C1 (en) * | 2010-10-27 | 2012-03-27 | Федеральное государственное унитарное предприятие "Научно-производственный центр газотурбостроения "Салют" (ФГУП "НПЦ газотурбостроения "Салют") | Method of controlling low-pressure rotor rpm in bypass gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
RU2319025C1 (en) | 2008-03-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PC4A | Invention patent assignment |
Effective date: 20091217 |
|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20100428 |