RU2003115178A - METHOD FOR DETERMINING FLOW PARAMETERS IN A COMPRESSOR AND A DEVICE FOR ITS IMPLEMENTATION - Google Patents
METHOD FOR DETERMINING FLOW PARAMETERS IN A COMPRESSOR AND A DEVICE FOR ITS IMPLEMENTATIONInfo
- Publication number
- RU2003115178A RU2003115178A RU2003115178/06A RU2003115178A RU2003115178A RU 2003115178 A RU2003115178 A RU 2003115178A RU 2003115178/06 A RU2003115178/06 A RU 2003115178/06A RU 2003115178 A RU2003115178 A RU 2003115178A RU 2003115178 A RU2003115178 A RU 2003115178A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- unit
- determining
- static pressure
- instantaneous
- Prior art date
Links
- 230000003068 static effect Effects 0.000 claims 9
- 230000010349 pulsation Effects 0.000 claims 6
- 238000005259 measurement Methods 0.000 claims 5
- 230000002093 peripheral effect Effects 0.000 claims 3
- 238000012800 visualization Methods 0.000 claims 3
- 230000001360 synchronised effect Effects 0.000 claims 2
- 230000036592 analgesia Effects 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 claims 1
- 238000000034 method Methods 0.000 claims 1
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2003115178/06A RU2246711C1 (en) | 2003-05-23 | 2003-05-23 | Method and device for measuring parameters of flow in compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2003115178/06A RU2246711C1 (en) | 2003-05-23 | 2003-05-23 | Method and device for measuring parameters of flow in compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2003115178A true RU2003115178A (en) | 2004-11-20 |
| RU2246711C1 RU2246711C1 (en) | 2005-02-20 |
Family
ID=35218813
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2003115178/06A RU2246711C1 (en) | 2003-05-23 | 2003-05-23 | Method and device for measuring parameters of flow in compressor |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2246711C1 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2285244C1 (en) * | 2005-02-21 | 2006-10-10 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Device for measuring parameters of pulsing current |
| RU2309390C1 (en) * | 2006-04-18 | 2007-10-27 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Method and device for determining parameters of flow in compressor |
| RU2347110C1 (en) * | 2007-08-10 | 2009-02-20 | Открытое акционерное общество "Авиадвигатель" | Axial compressor stage |
| RU2561783C1 (en) * | 2014-04-30 | 2015-09-10 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Method of determining attack angle of flow-separation from smooth surfaces of models |
| RU2656083C1 (en) * | 2017-06-21 | 2018-05-30 | Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Method of operation of gas turbine engine |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4595340A (en) * | 1984-07-30 | 1986-06-17 | General Electric Company | Gas turbine bladed disk assembly |
| USH1006H (en) * | 1990-03-27 | 1991-12-03 | The United States Of America As Represented By The Secretary Of The Air Force | Multilevel classifier structure for gas turbine engines |
| RU2098669C1 (en) * | 1995-08-21 | 1997-12-10 | Открытое акционерное общество "Кировский завод" | Method of stabilization of gas dynamic stability margin for turbocomplex |
-
2003
- 2003-05-23 RU RU2003115178/06A patent/RU2246711C1/en not_active IP Right Cessation
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