RU97108163A - OIL COOLING EJECTOR SYSTEM FOR AUXILIARY AIRCRAFT ENGINE - Google Patents
OIL COOLING EJECTOR SYSTEM FOR AUXILIARY AIRCRAFT ENGINEInfo
- Publication number
- RU97108163A RU97108163A RU97108163/28A RU97108163A RU97108163A RU 97108163 A RU97108163 A RU 97108163A RU 97108163/28 A RU97108163/28 A RU 97108163/28A RU 97108163 A RU97108163 A RU 97108163A RU 97108163 A RU97108163 A RU 97108163A
- Authority
- RU
- Russia
- Prior art keywords
- aircraft
- air
- mounting compartment
- auxiliary
- oil cooling
- Prior art date
Links
- 238000001816 cooling Methods 0.000 claims 2
- 210000003491 Skin Anatomy 0.000 claims 1
Claims (3)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19619535A DE19619535C1 (en) | 1996-05-15 | 1996-05-15 | Ejector oil cooling system for an aircraft auxiliary engine |
DE19619535.7 | 1996-05-15 |
Publications (2)
Publication Number | Publication Date |
---|---|
RU97108163A true RU97108163A (en) | 1999-04-27 |
RU2131380C1 RU2131380C1 (en) | 1999-06-10 |
Family
ID=7794356
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU97108163A RU2131380C1 (en) | 1996-05-15 | 1997-05-14 | Ejector-type oil cooling system for auxiliary aircraft engine |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0807576B1 (en) |
DE (2) | DE19619535C1 (en) |
ES (1) | ES2180839T3 (en) |
RU (1) | RU2131380C1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6092360A (en) * | 1998-07-01 | 2000-07-25 | The Boeing Company | Auxiliary power unit passive cooling system |
US6615576B2 (en) * | 2001-03-29 | 2003-09-09 | Honeywell International Inc. | Tortuous path quiet exhaust eductor system |
US6651929B2 (en) | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
US20060163425A1 (en) * | 2005-01-27 | 2006-07-27 | Honeywell International, Inc. | Aircraft inlet assembly for reducing auxiliary power unit noise |
DE102007061588B4 (en) | 2007-12-20 | 2011-07-21 | Airbus Operations GmbH, 21129 | Aircraft cooling system |
US8444083B2 (en) | 2011-06-30 | 2013-05-21 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet |
FR2986275B1 (en) * | 2012-02-01 | 2016-07-01 | Turbomeca | GAS TURBINE EXHAUST GAS EJECTION METHOD AND OPTIMIZED CONFIGURATION EXHAUST ASSEMBLY |
CN102673793B (en) * | 2012-06-08 | 2015-04-29 | 中国航空工业集团公司西安飞机设计研究所 | Exhaust ejector system of airplane auxiliary power unit |
RU2587733C1 (en) * | 2015-01-13 | 2016-06-20 | Открытое акционерное общество "Научно-производственное предприятие "Аэросила" | Ejector oil cooling system in power plant |
RU2632561C2 (en) * | 2016-02-15 | 2017-10-05 | Владимир Леонидович Письменный | Air-to-air radiator and method for efficiency increase |
RU2696521C1 (en) * | 2018-05-17 | 2019-08-02 | Общество с ограниченной ответственностью "Газпром трансгаз Ухта" | Method of reducing air temperature in cavity between conical housing of power turbine of engine al-31stn and internal housing of volute of gas transfer unit c1-16l/76-1.44 |
WO2023002132A1 (en) * | 2021-07-21 | 2023-01-26 | Flying Whales | System for the thermal management of an external electric-power-generating nacelle equipping an electrically powered airship, nacelle and airship equipped with said system |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1803156A (en) * | 1930-03-24 | 1931-04-28 | Wagner Rudolf | Air-cooled condenser for steam-driven vehicles |
DE733564C (en) * | 1938-03-17 | 1943-03-29 | Ettore Bugatti | Radiator arrangement on aircraft |
GB723406A (en) * | 1952-12-29 | 1955-02-09 | Northrop Aircraft Inc | Improvements in or relating to aircraft jet engine cooling system |
US4504030A (en) * | 1982-12-06 | 1985-03-12 | United Technologies Corporation | Cooling means |
US5265408A (en) * | 1992-02-13 | 1993-11-30 | Allied-Signal Inc. | Exhaust eductor cooling system |
US5655359A (en) * | 1995-05-15 | 1997-08-12 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airplane |
-
1996
- 1996-05-15 DE DE19619535A patent/DE19619535C1/en not_active Expired - Lifetime
-
1997
- 1997-03-21 DE DE59707946T patent/DE59707946D1/en not_active Expired - Lifetime
- 1997-03-21 ES ES97104818T patent/ES2180839T3/en not_active Expired - Lifetime
- 1997-03-21 EP EP97104818A patent/EP0807576B1/en not_active Expired - Lifetime
- 1997-05-14 RU RU97108163A patent/RU2131380C1/en active
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