GB0007441D0 - A mounting for coupling a turbofan gas turbine engine to an aircraft structure - Google Patents
A mounting for coupling a turbofan gas turbine engine to an aircraft structureInfo
- Publication number
- GB0007441D0 GB0007441D0 GBGB0007441.9A GB0007441A GB0007441D0 GB 0007441 D0 GB0007441 D0 GB 0007441D0 GB 0007441 A GB0007441 A GB 0007441A GB 0007441 D0 GB0007441 D0 GB 0007441D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- coupling
- mounting
- gas turbine
- turbine engine
- aircraft structure
- 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- Withdrawn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
- 230000008878 coupling Effects 0.000 title 1
- 238000010168 coupling process Methods 0.000 title 1
- 238000005859 coupling reaction 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- 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
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0007441A GB2360749A (en) | 2000-03-28 | 2000-03-28 | Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0007441A GB2360749A (en) | 2000-03-28 | 2000-03-28 | Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0007441D0 true GB0007441D0 (en) | 2000-05-17 |
GB2360749A GB2360749A (en) | 2001-10-03 |
Family
ID=9888529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0007441A Withdrawn GB2360749A (en) | 2000-03-28 | 2000-03-28 | Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2360749A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2394991B (en) * | 2002-11-06 | 2006-02-15 | Rolls Royce Plc | Mounting arrangement |
CA2918320C (en) | 2013-07-26 | 2018-05-15 | Mra Systems, Inc. | Aircraft engine pylon |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8300748D0 (en) * | 1983-01-12 | 1983-02-16 | British Aerospace | Power plant attachment for aircraft wings |
US4917331A (en) * | 1988-11-10 | 1990-04-17 | The Boeing Company | Apparatus and methods for reducing aircraft lifting surface flutter |
-
2000
- 2000-03-28 GB GB0007441A patent/GB2360749A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2360749A (en) | 2001-10-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2303884B (en) | A mounting for coupling a turbofan gas turbine engine to an aircraft structure | |
GB2275308B (en) | A mounting for coupling a turbofan gas turbine engine to an aircraft structure | |
GB2361303B (en) | Wall structure for a gas turbine engine combustor | |
GB9921935D0 (en) | A nacelle assembly for a gas turbine engine | |
GB2385382B (en) | A cowl structure for a gas turbine engine | |
GB2375513B (en) | A mounting arrangement for a gas turbine engine | |
GB2382382B (en) | A fan for a turbofan gas turbine engine | |
GB9927425D0 (en) | A gas turbine engine mounting arrangement | |
GB0116988D0 (en) | A gas turbine engine blade containment assembly | |
GB9928242D0 (en) | Combustion chamber for a gas turbine engine | |
GB2365078B (en) | A gas turbine engine blade | |
GB0025878D0 (en) | Gas turbine engine combustion system | |
GB2361033B (en) | A gas turbine engine blade containment assembly | |
GB0206139D0 (en) | A variable position intake for an aircraft mounted gas turbine engine | |
EP1291581A3 (en) | Gas turbine engine combustor | |
GB0004696D0 (en) | Gas turbine engine | |
GB0008193D0 (en) | A gas turbine engine blade containment assembly | |
GB9922618D0 (en) | A gas turbine engine blade containment assembly | |
GB9925193D0 (en) | Gas turbine engine exhaust nozzle | |
EA199900537A3 (en) | A gas turbine engine combustion system | |
GB2346177B (en) | Gas turbine engine | |
AU6482100A (en) | Drag reduction for gas turbine engine components | |
GB9924120D0 (en) | A wall structure for a combustor of a gas turbine engine | |
GB0004694D0 (en) | Gas turbine engine | |
GB2365926B (en) | A gas turbine engine blade containment assembly |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |