FR924449A - Aircraft aileron control device - Google Patents
Aircraft aileron control deviceInfo
- Publication number
- FR924449A FR924449A FR924449DA FR924449A FR 924449 A FR924449 A FR 924449A FR 924449D A FR924449D A FR 924449DA FR 924449 A FR924449 A FR 924449A
- Authority
- FR
- France
- Prior art keywords
- control device
- aileron control
- aircraft aileron
- aircraft
- control
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR924449T | 1946-03-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR924449A true FR924449A (en) | 1947-08-05 |
Family
ID=9439402
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR924449D Expired FR924449A (en) | 1946-03-26 | 1946-03-26 | Aircraft aileron control device |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR924449A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0052240A1 (en) * | 1980-11-13 | 1982-05-26 | Rockwell International Corporation | Actuation system for a control surface of an aircraft |
FR2909637A1 (en) * | 2006-12-12 | 2008-06-13 | Michel Kieffer | Control system for e.g. elevator of glider, has main and aileron tubes arranged in vertical planes so that rotation of handle generates rotation of main tube to drive translation of aileron tube whose end is connected to main tube |
-
1946
- 1946-03-26 FR FR924449D patent/FR924449A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0052240A1 (en) * | 1980-11-13 | 1982-05-26 | Rockwell International Corporation | Actuation system for a control surface of an aircraft |
FR2909637A1 (en) * | 2006-12-12 | 2008-06-13 | Michel Kieffer | Control system for e.g. elevator of glider, has main and aileron tubes arranged in vertical planes so that rotation of handle generates rotation of main tube to drive translation of aileron tube whose end is connected to main tube |
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