FR983430A - New overhead propeller hub and its construction method - Google Patents
New overhead propeller hub and its construction methodInfo
- Publication number
- FR983430A FR983430A FR983430DA FR983430A FR 983430 A FR983430 A FR 983430A FR 983430D A FR983430D A FR 983430DA FR 983430 A FR983430 A FR 983430A
- Authority
- FR
- France
- Prior art keywords
- construction method
- propeller hub
- new overhead
- overhead propeller
- new
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/02—Hub construction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR983430T | 1943-08-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR983430A true FR983430A (en) | 1951-06-22 |
Family
ID=9536028
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR983430D Expired FR983430A (en) | 1943-08-20 | 1943-08-20 | New overhead propeller hub and its construction method |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR983430A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2943984A1 (en) * | 2009-04-07 | 2010-10-08 | Airbus France | Propeller for turbine engine e.g. open rotor type turbine engine, of aircraft, has hub comprising two annular type portions that are fixed to each other and defining part of recess opening |
-
1943
- 1943-08-20 FR FR983430D patent/FR983430A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2943984A1 (en) * | 2009-04-07 | 2010-10-08 | Airbus France | Propeller for turbine engine e.g. open rotor type turbine engine, of aircraft, has hub comprising two annular type portions that are fixed to each other and defining part of recess opening |
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