FR1596504A - - Google Patents
Info
- Publication number
- FR1596504A FR1596504A FR1596504DA FR1596504A FR 1596504 A FR1596504 A FR 1596504A FR 1596504D A FR1596504D A FR 1596504DA FR 1596504 A FR1596504 A FR 1596504A
- Authority
- FR
- France
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H3/00—Propeller-blade pitch changing
- B63H3/02—Propeller-blade pitch changing actuated by control element coaxial with propeller shaft, e.g. the control element being rotary
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR159442 | 1968-07-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1596504A true FR1596504A (en) | 1970-06-22 |
Family
ID=8652663
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1596504D Expired FR1596504A (en) | 1968-07-17 | 1968-07-17 |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR1596504A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2126109A1 (en) * | 1971-02-25 | 1972-10-06 | Snecma | |
| FR2942645A1 (en) * | 2009-02-27 | 2010-09-03 | Snecma | Fan part for turbofan engine of aircraft, has strip whose geometry permits application of displacement parallel to axis, during its rotary movement with respect to stator part, to assure variation of blade incidence based on setting law |
| FR2942644A1 (en) * | 2009-02-27 | 2010-09-03 | Snecma | Fan part for turbofan engine of aircraft, has incidence setting system configured such that incidence of blade varies, according to cyclic setting law, based on angular position of blade along axis, where law is periodic of specific period |
| WO2010097438A3 (en) * | 2009-02-27 | 2010-12-02 | Snecma | Fan blades with cyclic setting |
-
1968
- 1968-07-17 FR FR1596504D patent/FR1596504A/fr not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2126109A1 (en) * | 1971-02-25 | 1972-10-06 | Snecma | |
| FR2942645A1 (en) * | 2009-02-27 | 2010-09-03 | Snecma | Fan part for turbofan engine of aircraft, has strip whose geometry permits application of displacement parallel to axis, during its rotary movement with respect to stator part, to assure variation of blade incidence based on setting law |
| FR2942644A1 (en) * | 2009-02-27 | 2010-09-03 | Snecma | Fan part for turbofan engine of aircraft, has incidence setting system configured such that incidence of blade varies, according to cyclic setting law, based on angular position of blade along axis, where law is periodic of specific period |
| WO2010097438A3 (en) * | 2009-02-27 | 2010-12-02 | Snecma | Fan blades with cyclic setting |
| CN102333962A (en) * | 2009-02-27 | 2012-01-25 | 斯奈克玛 | Fan blades with cyclic setting |
| US9200594B2 (en) | 2009-02-27 | 2015-12-01 | Snecma | Gas turbine engine having fan blades of adjustable pitch with cyclic setting |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |