IT1242998B - Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozione - Google Patents
Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozioneInfo
- Publication number
- IT1242998B IT1242998B IT02133690A IT2133690A IT1242998B IT 1242998 B IT1242998 B IT 1242998B IT 02133690 A IT02133690 A IT 02133690A IT 2133690 A IT2133690 A IT 2133690A IT 1242998 B IT1242998 B IT 1242998B
- Authority
- IT
- Italy
- Prior art keywords
- fan
- transport
- removal
- ultra high
- derivation engine
- Prior art date
Links
- 238000009795 derivation Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings or cowlings
- B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US40397489A | 1989-09-07 | 1989-09-07 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| IT9021336A0 IT9021336A0 (it) | 1990-08-30 |
| IT9021336A1 IT9021336A1 (it) | 1992-03-01 |
| IT1242998B true IT1242998B (it) | 1994-05-23 |
Family
ID=23597620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT02133690A IT1242998B (it) | 1989-09-07 | 1990-08-30 | Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozione |
Country Status (6)
| Country | Link |
|---|---|
| JP (1) | JPH03141829A (it) |
| CA (1) | CA2021087A1 (it) |
| DE (1) | DE4025775A1 (it) |
| FR (1) | FR2651537A1 (it) |
| GB (1) | GB2238082A (it) |
| IT (1) | IT1242998B (it) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2866070B1 (fr) * | 2004-02-05 | 2008-12-05 | Snecma Moteurs | Turboreacteur a fort taux de dilution |
| GB0520850D0 (en) | 2005-10-14 | 2005-11-23 | Rolls Royce Plc | Fan static structure |
| US20100047077A1 (en) * | 2007-12-28 | 2010-02-25 | General Electric Company | Ferry Flight Engine Fairing Kit |
| US20100043228A1 (en) * | 2007-12-28 | 2010-02-25 | James Lloyd Daniels | Method of Preparing an Engine for Ferry Flight |
| US8469309B2 (en) * | 2008-12-24 | 2013-06-25 | General Electric Company | Monolithic structure for mounting aircraft engine |
| US8814512B2 (en) | 2011-07-05 | 2014-08-26 | United Technologies Corporation | Fan disk apparatus and method |
| CN107738223B (zh) * | 2017-11-13 | 2023-11-10 | 山东太古飞机工程有限公司 | 飞机发动机第一级静子叶片整流罩的拆装辅助工装 |
| GB201810606D0 (en) * | 2018-06-28 | 2018-08-15 | Rolls Royce Plc | Gas turbine engine |
| GB201817935D0 (en) * | 2018-11-02 | 2018-12-19 | Rolls Royce Plc | Method of replacing a module |
| GB201817936D0 (en) * | 2018-11-02 | 2018-12-19 | Rolls Royce Plc | Method of upgrading a modular gas turbine engine |
| GB202001971D0 (en) * | 2020-02-13 | 2020-04-01 | Rolls Royce Plc | Nacelle for gas turbine engine and aircraft comprising the same |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1093050A (en) * | 1965-03-16 | 1967-11-29 | Rolls Royce | Aircraft engine mounting |
| US3398535A (en) * | 1966-05-25 | 1968-08-27 | Gen Electric | Engine supporting structure |
| FR2153787A5 (it) * | 1971-09-23 | 1973-05-04 | Inst Francais Du Petrole | |
| FR2096708B1 (it) * | 1970-06-22 | 1974-03-22 | Snecma | |
| US3703081A (en) * | 1970-11-20 | 1972-11-21 | Gen Electric | Gas turbine engine |
| JPS5022165U (it) * | 1973-06-23 | 1975-03-12 | ||
| GB1533551A (en) * | 1974-11-08 | 1978-11-29 | Gen Electric | Gas turbofan engines |
| JPS5268609A (en) * | 1975-12-04 | 1977-06-07 | Agency Of Ind Science & Technol | Fixing device for static wing in turbo-fan engine |
| US4825648A (en) * | 1987-03-02 | 1989-05-02 | General Electric Company | Turbofan engine having a split cowl |
| US4934140A (en) * | 1988-05-13 | 1990-06-19 | United Technologies Corporation | Modular gas turbine engine |
-
1990
- 1990-07-12 CA CA002021087A patent/CA2021087A1/en not_active Abandoned
- 1990-08-14 DE DE4025775A patent/DE4025775A1/de not_active Ceased
- 1990-08-22 FR FR9010566A patent/FR2651537A1/fr not_active Withdrawn
- 1990-08-28 JP JP2224523A patent/JPH03141829A/ja active Pending
- 1990-08-30 IT IT02133690A patent/IT1242998B/it active IP Right Grant
- 1990-09-05 GB GB9019356A patent/GB2238082A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| IT9021336A0 (it) | 1990-08-30 |
| GB2238082A (en) | 1991-05-22 |
| JPH03141829A (ja) | 1991-06-17 |
| IT9021336A1 (it) | 1992-03-01 |
| DE4025775A1 (de) | 1991-03-28 |
| GB9019356D0 (en) | 1990-10-17 |
| FR2651537A1 (fr) | 1991-03-08 |
| CA2021087A1 (en) | 1991-03-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 0001 | Granted |