GB201917783D0 - Geared gas turbine engine - Google Patents
Geared gas turbine engineInfo
- Publication number
- GB201917783D0 GB201917783D0 GBGB1917783.1A GB201917783A GB201917783D0 GB 201917783 D0 GB201917783 D0 GB 201917783D0 GB 201917783 A GB201917783 A GB 201917783A GB 201917783 D0 GB201917783 D0 GB 201917783D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- geared gas
- geared
- engine
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/08—General details of gearing of gearings with members having orbital motion
- F16H57/082—Planet carriers
-
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
- F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/2809—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears
- F16H1/2827—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears by allowing limited movement of the planet carrier, e.g. relative to its shaft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/2809—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears
- F16H1/2836—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears by allowing limited movement of the planet gears relative to the planet carrier or by using free floating planet gears
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Retarders (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1917783.1A GB201917783D0 (en) | 2019-12-05 | 2019-12-05 | Geared gas turbine engine |
| DE102020131802.2A DE102020131802A1 (en) | 2019-12-05 | 2020-12-01 | GEAR-GAS TURBINE ENGINE |
| FR2012450A FR3104203A1 (en) | 2019-12-05 | 2020-12-01 | Gear gas turbine engine |
| CN202022871955.8U CN216381626U (en) | 2019-12-05 | 2020-12-04 | Gas turbine engine and propeller for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1917783.1A GB201917783D0 (en) | 2019-12-05 | 2019-12-05 | Geared gas turbine engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB201917783D0 true GB201917783D0 (en) | 2020-01-22 |
Family
ID=69172031
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GBGB1917783.1A Ceased GB201917783D0 (en) | 2019-12-05 | 2019-12-05 | Geared gas turbine engine |
Country Status (4)
| Country | Link |
|---|---|
| CN (1) | CN216381626U (en) |
| DE (1) | DE102020131802A1 (en) |
| FR (1) | FR3104203A1 (en) |
| GB (1) | GB201917783D0 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114962427B (en) * | 2022-06-30 | 2023-09-26 | 中国航发贵阳发动机设计研究所 | Structure for realizing multidirectional transmission of engine rotor by double transmission shafts |
| FR3163980A1 (en) * | 2024-06-28 | 2026-01-02 | Safran Aircraft Engines | AIRCRAFT TURBOMACHINE MECHANICAL REDUCTION GEAR |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9631558B2 (en) * | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
| US9145830B2 (en) * | 2012-06-04 | 2015-09-29 | United Technologies Corporation | Turbomachine geared architecture support assembly |
| EP3882448B1 (en) * | 2013-03-12 | 2024-07-10 | RTX Corporation | Flexible coupling for geared turbine engine |
| US9739170B2 (en) * | 2014-12-30 | 2017-08-22 | General Electric Company | Flexibly damped mounting assemblies for power gear box transmissions in geared aircraft engine architectures |
| IT201800005822A1 (en) * | 2018-05-29 | 2019-11-29 | ATTACHMENT OF A GEAR GROUP FOR A GAS TURBINE ENGINE | |
| GB201917781D0 (en) * | 2019-12-05 | 2020-01-22 | Rolls Royce Plc | Reliable gearbox for gas turbine engine |
-
2019
- 2019-12-05 GB GBGB1917783.1A patent/GB201917783D0/en not_active Ceased
-
2020
- 2020-12-01 DE DE102020131802.2A patent/DE102020131802A1/en active Pending
- 2020-12-01 FR FR2012450A patent/FR3104203A1/en not_active Ceased
- 2020-12-04 CN CN202022871955.8U patent/CN216381626U/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| DE102020131802A1 (en) | 2021-06-10 |
| FR3104203A1 (en) | 2021-06-11 |
| CN216381626U (en) | 2022-04-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AT | Applications terminated before publication under section 16(1) |