BR8103330A - Eixo acionador de metal composto e seu respectivo processso de fabricacao - Google Patents
Eixo acionador de metal composto e seu respectivo processso de fabricacaoInfo
- Publication number
- BR8103330A BR8103330A BR8103330A BR8103330A BR8103330A BR 8103330 A BR8103330 A BR 8103330A BR 8103330 A BR8103330 A BR 8103330A BR 8103330 A BR8103330 A BR 8103330A BR 8103330 A BR8103330 A BR 8103330A
- Authority
- BR
- Brazil
- Prior art keywords
- drive shaft
- manufacturing process
- composite metal
- respective manufacturing
- metal drive
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000002184 metal Substances 0.000 title 1
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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Ocean & Marine Engineering (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16303780A | 1980-06-26 | 1980-06-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BR8103330A true BR8103330A (pt) | 1982-02-16 |
Family
ID=22588199
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR8103330A BR8103330A (pt) | 1980-06-26 | 1981-05-28 | Eixo acionador de metal composto e seu respectivo processso de fabricacao |
Country Status (8)
| Country | Link |
|---|---|
| JP (1) | JPS5715114A (enExample) |
| BR (1) | BR8103330A (enExample) |
| CA (1) | CA1146372A (enExample) |
| DE (1) | DE3108318A1 (enExample) |
| FR (1) | FR2485659A1 (enExample) |
| GB (1) | GB2078338B (enExample) |
| IT (1) | IT1137947B (enExample) |
| SE (1) | SE8101237L (enExample) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3800913A1 (de) * | 1988-01-14 | 1989-08-03 | Emitec Emissionstechnologie | Mehrschichtenantriebswelle |
| GB2220595B (en) * | 1988-07-13 | 1992-10-21 | Secr Defence | Hard surface composite parts. |
| GB2247492B (en) * | 1990-09-01 | 1995-01-11 | Rolls Royce Plc | A method of making a fibre reinforced metal component |
| US5305520A (en) * | 1990-09-01 | 1994-04-26 | Rolls-Royce Plc | Method of making fibre reinforced metal component |
| US8225481B2 (en) * | 2003-05-19 | 2012-07-24 | Pratt & Whitney Rocketdyne, Inc. | Diffusion bonded composite material and method therefor |
| US6897578B1 (en) * | 2003-12-08 | 2005-05-24 | Ingersoll-Rand Energy Systems Corporation | Integrated microturbine gearbox generator assembly |
| GB2438633B (en) * | 2006-05-31 | 2010-12-01 | Tisics Ltd | Reinforced splines and their manufacture |
| US20080148708A1 (en) | 2006-12-20 | 2008-06-26 | General Electric Company | Turbine engine system with shafts for improved weight and vibration characteristic |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1548099A (enExample) * | 1966-12-22 | 1968-11-29 | ||
| DE1750523B1 (de) * | 1968-05-10 | 1971-12-09 | Augsburg Nuernberg Ag Zweignie | Verfahren zur herstellung einer trommel oder welle |
| US3651661A (en) * | 1970-02-02 | 1972-03-28 | United Aircraft Corp | Composite shaft with integral end flange |
| CA1098329A (en) * | 1977-12-02 | 1981-03-31 | Richard L. Vanauken | Composite tubular element and methods for making same |
| US4272971A (en) * | 1979-02-26 | 1981-06-16 | Rockwell International Corporation | Reinforced tubular structure |
-
1981
- 1981-02-25 SE SE8101237A patent/SE8101237L/ not_active Application Discontinuation
- 1981-03-02 GB GB8106563A patent/GB2078338B/en not_active Expired
- 1981-03-02 DE DE19813108318 patent/DE3108318A1/de not_active Withdrawn
- 1981-03-17 JP JP3733781A patent/JPS5715114A/ja active Pending
- 1981-03-27 CA CA000373994A patent/CA1146372A/en not_active Expired
- 1981-04-23 FR FR8108090A patent/FR2485659A1/fr active Granted
- 1981-05-28 BR BR8103330A patent/BR8103330A/pt unknown
- 1981-06-26 IT IT22601/81A patent/IT1137947B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| IT1137947B (it) | 1986-09-10 |
| SE8101237L (sv) | 1981-12-27 |
| CA1146372A (en) | 1983-05-17 |
| FR2485659A1 (fr) | 1981-12-31 |
| GB2078338B (en) | 1983-08-10 |
| GB2078338A (en) | 1982-01-06 |
| DE3108318A1 (de) | 1982-01-21 |
| FR2485659B1 (enExample) | 1984-12-28 |
| JPS5715114A (en) | 1982-01-26 |
| IT8122601A0 (it) | 1981-06-26 |
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