RU2004117516A - AIRCRAFT ENGINE CHANNEL - Google Patents
AIRCRAFT ENGINE CHANNEL Download PDFInfo
- Publication number
- RU2004117516A RU2004117516A RU2004117516/11A RU2004117516A RU2004117516A RU 2004117516 A RU2004117516 A RU 2004117516A RU 2004117516/11 A RU2004117516/11 A RU 2004117516/11A RU 2004117516 A RU2004117516 A RU 2004117516A RU 2004117516 A RU2004117516 A RU 2004117516A
- Authority
- RU
- Russia
- Prior art keywords
- aircraft engine
- honeycomb
- gap
- panels
- layer
- Prior art date
Links
Landscapes
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2004117516/11A RU2297369C2 (en) | 2004-06-08 | 2004-06-08 | Air intake passage for flying vehicle engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2004117516/11A RU2297369C2 (en) | 2004-06-08 | 2004-06-08 | Air intake passage for flying vehicle engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2004117516A true RU2004117516A (en) | 2005-11-20 |
RU2297369C2 RU2297369C2 (en) | 2007-04-20 |
Family
ID=35866916
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2004117516/11A RU2297369C2 (en) | 2004-06-08 | 2004-06-08 | Air intake passage for flying vehicle engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2297369C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2537998C2 (en) * | 2008-05-16 | 2015-01-10 | Эрсель | Aircraft power plant and its air intake |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2925118B1 (en) * | 2007-12-14 | 2009-12-25 | Snecma | ABRADABLE SUPPORT PANEL IN A TURBOMACHINE |
FR2949820B1 (en) * | 2009-09-04 | 2011-10-14 | Aircelle Sa | STRUCTURING ASSEMBLY FOR AN EJECTION TUBE. |
DE102012001571A1 (en) * | 2012-01-26 | 2013-08-01 | Rolls-Royce Deutschland Ltd & Co Kg | Engine casing of an aircraft gas turbine with sound attenuation elements in the fan inflow area |
RU2522661C1 (en) * | 2012-11-23 | 2014-07-20 | Государственный научный центр Российской Федерации-федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" | Air intake power unit device of hypersonic aircraft |
RU180269U1 (en) * | 2017-08-29 | 2018-06-07 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Gas turbine engine intake duct |
-
2004
- 2004-06-08 RU RU2004117516/11A patent/RU2297369C2/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2537998C2 (en) * | 2008-05-16 | 2015-01-10 | Эрсель | Aircraft power plant and its air intake |
Also Published As
Publication number | Publication date |
---|---|
RU2297369C2 (en) | 2007-04-20 |
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