ES2322317A1 - Turbopropulsor aeronautico. - Google Patents
Turbopropulsor aeronautico. Download PDFInfo
- Publication number
- ES2322317A1 ES2322317A1 ES200701797A ES200701797A ES2322317A1 ES 2322317 A1 ES2322317 A1 ES 2322317A1 ES 200701797 A ES200701797 A ES 200701797A ES 200701797 A ES200701797 A ES 200701797A ES 2322317 A1 ES2322317 A1 ES 2322317A1
- Authority
- ES
- Spain
- Prior art keywords
- turboprop
- low pressure
- combustion
- pressure turbine
- combustion chamber
- 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
- 239000007789 gas Substances 0.000 claims abstract description 6
- 238000002485 combustion reaction Methods 0.000 claims description 40
- 239000000446 fuel Substances 0.000 claims description 5
- 238000001816 cooling Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/115—Heating the by-pass flow by means of indirect heat exchange
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
Description
Claims (6)
radialmente.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES200701797A ES2322317B1 (es) | 2007-06-20 | 2007-06-20 | Turbopropulsor aeronautico. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES200701797A ES2322317B1 (es) | 2007-06-20 | 2007-06-20 | Turbopropulsor aeronautico. |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2322317A1 true ES2322317A1 (es) | 2009-06-18 |
ES2322317B1 ES2322317B1 (es) | 2010-03-31 |
Family
ID=40739904
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES200701797A Expired - Fee Related ES2322317B1 (es) | 2007-06-20 | 2007-06-20 | Turbopropulsor aeronautico. |
Country Status (1)
Country | Link |
---|---|
ES (1) | ES2322317B1 (es) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4254618A (en) * | 1977-08-18 | 1981-03-10 | General Electric Company | Cooling air cooler for a gas turbofan engine |
FR2482196A1 (fr) * | 1980-05-07 | 1981-11-13 | Snecma | Echangeur de chaleur pour moteur a reaction a double flux |
WO2000022350A1 (de) * | 1998-10-12 | 2000-04-20 | Rolls-Royce Deutschland Gmbh | Brennstoffeinspritzsystem für eine radial- oder slinger-brennkammer einer kleingasturbine |
US6134880A (en) * | 1997-12-31 | 2000-10-24 | Concepts Eti, Inc. | Turbine engine with intercooler in bypass air passage |
-
2007
- 2007-06-20 ES ES200701797A patent/ES2322317B1/es not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4254618A (en) * | 1977-08-18 | 1981-03-10 | General Electric Company | Cooling air cooler for a gas turbofan engine |
FR2482196A1 (fr) * | 1980-05-07 | 1981-11-13 | Snecma | Echangeur de chaleur pour moteur a reaction a double flux |
US6134880A (en) * | 1997-12-31 | 2000-10-24 | Concepts Eti, Inc. | Turbine engine with intercooler in bypass air passage |
WO2000022350A1 (de) * | 1998-10-12 | 2000-04-20 | Rolls-Royce Deutschland Gmbh | Brennstoffeinspritzsystem für eine radial- oder slinger-brennkammer einer kleingasturbine |
Also Published As
Publication number | Publication date |
---|---|
ES2322317B1 (es) | 2010-03-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EC2A | Search report published |
Date of ref document: 20090618 Kind code of ref document: A1 |
|
FG2A | Definitive protection |
Ref document number: 2322317B1 Country of ref document: ES |
|
PC2A | Transfer of patent |
Owner name: JOSE LUIS BECERRIL RUIZ Effective date: 20130503 |
|
PC2A | Transfer of patent |
Owner name: JOSE ANTONIO JALDO ROPERO Effective date: 20130507 |
|
PC2A | Transfer of patent |
Owner name: AERO ENGINEERING, S.L. Effective date: 20130619 |
|
FD2A | Announcement of lapse in spain |
Effective date: 20211122 |