FR1123553A - Pneumatic bearing surface for flying machine - Google Patents
Pneumatic bearing surface for flying machineInfo
- Publication number
- FR1123553A FR1123553A FR1123553DA FR1123553A FR 1123553 A FR1123553 A FR 1123553A FR 1123553D A FR1123553D A FR 1123553DA FR 1123553 A FR1123553 A FR 1123553A
- Authority
- FR
- France
- Prior art keywords
- bearing surface
- flying machine
- pneumatic bearing
- pneumatic
- flying
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
- B64C27/021—Rotor or rotor head construction
- B64C27/023—Construction of the blades; Coating of the blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1123553XA | 1954-10-14 | 1954-10-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1123553A true FR1123553A (en) | 1956-09-24 |
Family
ID=22343455
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1123553D Expired FR1123553A (en) | 1954-10-14 | 1955-05-06 | Pneumatic bearing surface for flying machine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1123553A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5439353A (en) * | 1992-02-06 | 1995-08-08 | United Technologies Corporation | Composite blade with reinforced leading edge |
-
1955
- 1955-05-06 FR FR1123553D patent/FR1123553A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5439353A (en) * | 1992-02-06 | 1995-08-08 | United Technologies Corporation | Composite blade with reinforced leading edge |
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