EP2841718A4 - Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen - Google Patents
Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionenInfo
- Publication number
- EP2841718A4 EP2841718A4 EP13822569.3A EP13822569A EP2841718A4 EP 2841718 A4 EP2841718 A4 EP 2841718A4 EP 13822569 A EP13822569 A EP 13822569A EP 2841718 A4 EP2841718 A4 EP 2841718A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- high speed
- low pressure
- bearing support
- speed low
- support features
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/06—Arrangements of bearings; Lubricating
-
- 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
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP20162850.0A EP3708792A1 (de) | 2012-04-25 | 2013-04-23 | Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/455,235 US20130192191A1 (en) | 2012-01-31 | 2012-04-25 | Gas turbine engine with high speed low pressure turbine section and bearing support features |
US13/558,605 US9540948B2 (en) | 2012-01-31 | 2012-07-26 | Gas turbine engine with high speed low pressure turbine section and bearing support features |
PCT/US2013/037675 WO2014018142A2 (en) | 2012-04-25 | 2013-04-23 | Gas turbine engine with high speed low pressure turbine section and bearing support features |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20162850.0A Division EP3708792A1 (de) | 2012-04-25 | 2013-04-23 | Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2841718A2 EP2841718A2 (de) | 2015-03-04 |
EP2841718A4 true EP2841718A4 (de) | 2016-03-02 |
Family
ID=49997943
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13822569.3A Withdrawn EP2841718A4 (de) | 2012-04-25 | 2013-04-23 | Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen |
EP20162850.0A Withdrawn EP3708792A1 (de) | 2012-04-25 | 2013-04-23 | Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20162850.0A Withdrawn EP3708792A1 (de) | 2012-04-25 | 2013-04-23 | Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen |
Country Status (2)
Country | Link |
---|---|
EP (2) | EP2841718A4 (de) |
WO (1) | WO2014018142A2 (de) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10287914B2 (en) | 2012-01-31 | 2019-05-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
US9816442B2 (en) | 2012-01-31 | 2017-11-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
US9845726B2 (en) | 2012-01-31 | 2017-12-19 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
US10240526B2 (en) | 2012-01-31 | 2019-03-26 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
US10125693B2 (en) | 2012-04-02 | 2018-11-13 | United Technologies Corporation | Geared turbofan engine with power density range |
EP3032084A1 (de) * | 2014-12-12 | 2016-06-15 | United Technologies Corporation | Gasturbinenmotor mit einem hochgeschwindigkeits-niederdruck-turbinenabschnitt |
EP3034849A1 (de) * | 2014-12-17 | 2016-06-22 | United Technologies Corporation | Gasturbinenmotor mit einem hochgeschwindigkeits-niederdruck-turbinenabschnitt |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4809498A (en) * | 1987-07-06 | 1989-03-07 | General Electric Company | Gas turbine engine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4916894A (en) * | 1989-01-03 | 1990-04-17 | General Electric Company | High bypass turbofan engine having a partially geared fan drive turbine |
US6619030B1 (en) * | 2002-03-01 | 2003-09-16 | General Electric Company | Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
DE102005018139A1 (de) * | 2005-04-20 | 2006-10-26 | Mtu Aero Engines Gmbh | Stahltriebwerk |
US7762086B2 (en) * | 2008-03-12 | 2010-07-27 | United Technologies Corporation | Nozzle extension assembly for ground and flight testing |
-
2013
- 2013-04-23 EP EP13822569.3A patent/EP2841718A4/de not_active Withdrawn
- 2013-04-23 EP EP20162850.0A patent/EP3708792A1/de not_active Withdrawn
- 2013-04-23 WO PCT/US2013/037675 patent/WO2014018142A2/en active Application Filing
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4809498A (en) * | 1987-07-06 | 1989-03-07 | General Electric Company | Gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
EP2841718A2 (de) | 2015-03-04 |
EP3708792A1 (de) | 2020-09-16 |
WO2014018142A3 (en) | 2014-05-01 |
WO2014018142A2 (en) | 2014-01-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SG11201403615QA (en) | Gas turbine engine with high speed low pressure turbine section and bearing support features | |
SG10201706005SA (en) | Gas turbine engine with high speed low pressure turbine section | |
EP2809575A4 (de) | Gasturbinenmotor mit einem hochgeschwindigkeits-niederdruck-turbinenabschnitt | |
EP2809914A4 (de) | Konfiguration eines wellenlagers für eine gasturbine | |
EP2809890B8 (de) | Lageranordnung für einen gasturbinenmotor | |
SG11201405143XA (en) | Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections | |
SG11201403614VA (en) | Gas turbine engine with high speed low pressure turbine section and bearing support features | |
EP3049642A4 (de) | Gasturbinenmotor mit geteiltem schmiersystem | |
SG11201402972XA (en) | Gas turbine engine with variable overall pressure ratio | |
EP2815079A4 (de) | Gasturbinenmotorkomponente mit prall- und diffusionskühlung | |
SG11201404761TA (en) | Gas turbine engine with fan-tied inducer section | |
SG11201402940PA (en) | Gas turbine engine mid turbine frame bearing support | |
EP2776318A4 (de) | Gasturbinenmotor mit niederdruckturbine mit niedrigstufenzählung | |
EP2920445A4 (de) | Gasturbinenmotor mit halterung für niederdruck-turbinenabschnitt | |
SG11201403679SA (en) | Gas turbine engine component with diffusive cooling hole | |
EP2659109A4 (de) | Flugzeug und gasturbinenmotor | |
EP2841718A4 (de) | Gasturbinenmotor mit schnellem niederdruckturbinenabschnitt und lagerträgerfunktionen | |
EP2598737A4 (de) | Gasturbinenmotor mit ejektor | |
EP2809902A4 (de) | Lageranordnung für einen gasturbinenmotor | |
SG11201402663XA (en) | Gas turbine engine with geared architecture | |
SG11201404966QA (en) | Gas turbine engine geared architecture axial retention arrangement | |
EP3049655A4 (de) | Lageranordnung für einen gasturbinenmotor | |
EP2752553A4 (de) | Rotorvorrichtung, turbinenrotorvorrichtung und gasturbine sowie turbinenmotor damit | |
SG11201402895RA (en) | Gas turbine engine with low fan pressure ratio | |
EP3027864A4 (de) | Konfiguration eines wellenlagers für eine gasturbine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20141029 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAX | Request for extension of the european patent (deleted) | ||
A4 | Supplementary search report drawn up and despatched |
Effective date: 20160128 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F02C 7/06 20060101ALI20160122BHEP Ipc: F01D 25/16 20060101AFI20160122BHEP |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: UNITED TECHNOLOGIES CORPORATION |
|
TPAC | Observations filed by third parties |
Free format text: ORIGINAL CODE: EPIDOSNTIPA |
|
17Q | First examination report despatched |
Effective date: 20180927 |
|
TPAC | Observations filed by third parties |
Free format text: ORIGINAL CODE: EPIDOSNTIPA |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN |
|
18W | Application withdrawn |
Effective date: 20200312 |