BE692212A - - Google Patents
Info
- Publication number
- BE692212A BE692212A BE692212DA BE692212A BE 692212 A BE692212 A BE 692212A BE 692212D A BE692212D A BE 692212DA BE 692212 A BE692212 A BE 692212A
- Authority
- BE
- Belgium
Links
Classifications
-
- 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
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US54094566A | 1966-04-07 | 1966-04-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE692212A true BE692212A (US20100012521A1-20100121-C00001.png) | 1967-06-16 |
Family
ID=24157551
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE692212D BE692212A (US20100012521A1-20100121-C00001.png) | 1966-04-07 | 1967-01-05 |
Country Status (6)
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112589379A (zh) * | 2020-11-10 | 2021-04-02 | 中国航发贵州黎阳航空动力有限公司 | 带波棱的v型槽双层结构钣金组合件的加工方法及装置 |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1138763B (it) * | 1981-05-04 | 1986-09-17 | Nuovo Pignone Spa | Perfezionamenti in una turbina a gas di potenza |
| US4987736A (en) * | 1988-12-14 | 1991-01-29 | General Electric Company | Lightweight gas turbine engine frame with free-floating heat shield |
| CA3013015C (en) * | 2012-06-15 | 2020-06-02 | United Technologies Corporation | High durability turbine exhaust case |
| DE102016213810A1 (de) | 2016-07-27 | 2018-02-01 | MTU Aero Engines AG | Verkleidungselement für ein Turbinenzwischengehäuse |
| GB2559351B (en) * | 2017-02-01 | 2020-03-18 | Rolls Royce Plc | A geared gas turbine engine |
| CN114178790B (zh) * | 2021-12-08 | 2023-03-17 | 中国航发南方工业有限公司 | 发动机排气段制作工艺 |
-
1966
- 1966-12-14 GB GB5599366A patent/GB1137940A/en not_active Expired
- 1966-12-22 NL NL6618002A patent/NL6618002A/xx unknown
-
1967
- 1967-01-04 FR FR89945A patent/FR1507471A/fr not_active Expired
- 1967-01-04 DE DE1967G0048929 patent/DE1601548B2/de active Granted
- 1967-01-05 BE BE692212D patent/BE692212A/xx unknown
- 1967-01-06 CH CH17567A patent/CH478340A/de not_active IP Right Cessation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112589379A (zh) * | 2020-11-10 | 2021-04-02 | 中国航发贵州黎阳航空动力有限公司 | 带波棱的v型槽双层结构钣金组合件的加工方法及装置 |
Also Published As
| Publication number | Publication date |
|---|---|
| NL6618002A (US20100012521A1-20100121-C00001.png) | 1967-10-09 |
| DE1601548A1 (de) | 1970-02-12 |
| CH478340A (de) | 1969-09-15 |
| GB1137940A (en) | 1968-12-27 |
| FR1507471A (fr) | 1967-12-29 |
| DE1601548B2 (de) | 1976-10-28 |
