ES2059238R - - Google Patents
Info
- Publication number
- ES2059238R ES2059238R ES9201381A ES9201381A ES2059238R ES 2059238 R ES2059238 R ES 2059238R ES 9201381 A ES9201381 A ES 9201381A ES 9201381 A ES9201381 A ES 9201381A ES 2059238 R ES2059238 R ES 2059238R
- Authority
- ES
- Spain
- Prior art keywords
- flange
- variable
- divergent
- revolution
- axle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 abstract 1
Landscapes
- Supercharger (AREA)
- Control Of Turbines (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES9201381A ES2059238B1 (es) | 1992-07-03 | 1992-07-03 | Tobera orientable de geometria variable para propulsores de turbina de gas. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES9201381A ES2059238B1 (es) | 1992-07-03 | 1992-07-03 | Tobera orientable de geometria variable para propulsores de turbina de gas. |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| ES2059238A2 ES2059238A2 (es) | 1994-11-01 |
| ES2059238R true ES2059238R (ro) | 1997-01-01 |
| ES2059238B1 ES2059238B1 (es) | 1997-07-01 |
Family
ID=8277532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES9201381A Expired - Fee Related ES2059238B1 (es) | 1992-07-03 | 1992-07-03 | Tobera orientable de geometria variable para propulsores de turbina de gas. |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES2059238B1 (ro) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1381397A (en) * | 1971-02-26 | 1975-01-22 | Mtu Muenchen Gmbh | Jet pipe arrangement for a jet-propulsion engine |
| GB1499887A (en) * | 1974-03-02 | 1978-02-01 | Mtu Muenchen Gmbh | Device for varying the gas exit area of an exhaust nozzle in a jet deflecting device |
| US3989193A (en) * | 1974-03-02 | 1976-11-02 | Motoren- Und Turbinen-Union Munchen Gmbh M.A.N. Maybach Mercedes-Benz | Device for varying the gas exit area of an exhaust nozzle for a jet deflecting device |
| GB2196587B (en) * | 1980-10-31 | 1988-08-24 | Rolls Royce | Jet pipe for jet propulsion in aircraft |
| US4550877A (en) * | 1982-08-03 | 1985-11-05 | Rolls-Royce Inc. | Streamlined nozzle for turbomachines |
-
1992
- 1992-07-03 ES ES9201381A patent/ES2059238B1/es not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| ES2059238A2 (es) | 1994-11-01 |
| ES2059238B1 (es) | 1997-07-01 |
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| ES2105928B1 (es) | Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas. | |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EC2A | Search report published |
Date of ref document: 19941101 Kind code of ref document: R Effective date: 19941101 |
|
| FD1A | Patent lapsed |
Effective date: 20050704 |