GB416879A - Improvements in or relating to the control of aircraft - Google Patents
Improvements in or relating to the control of aircraftInfo
- Publication number
- GB416879A GB416879A GB29736/33A GB2973633A GB416879A GB 416879 A GB416879 A GB 416879A GB 29736/33 A GB29736/33 A GB 29736/33A GB 2973633 A GB2973633 A GB 2973633A GB 416879 A GB416879 A GB 416879A
- Authority
- GB
- United Kingdom
- Prior art keywords
- slats
- slot
- rudder
- rods
- bell
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Blinds (AREA)
Abstract
416,879. Controlling aircraft. FAIREY, C. R., Cranford Lane, Hayes, Middlesex. Oct. 26, 1933, No. 29736. [Class 4.] In means for controlling aircraft, slotforming slats 12 situated one at each end of the wings 11 are controlled by means interconnected with the rudder, or the actuating-means therefor, so that operation of the rudder 22 may bring about the opening or closing of either slot as required or prevent either slot from opening. The slats may be spring controlled or free and the motion transmitted thereto may be damped by a dashpot or like device. In one form, one or other of the slot-forming slats 12 is actuated to form a slot on movement of the rudder bar 20 through a rod 15, a bell-crank lever 16 and a cable 17 which includes a tensioning-device 18 which permits the slats to be operated under normal circumstances by the usual means (not shown). The slats 12 are connected by links 13 and radius rods 14, pivoted at one end to the wing, to the rods 15. In a modification, one or other of the slot-forming slats 12, Fig. 3, is held closed according to the direction in which the rudder bar 20 is operated on depression of a pedal 25 which actuates a friction clutch to cause a drum 23 to move with the rudder bar. A cable 17 including a tensioning-device 18 wound around the drum 23 has its ends connected to bell-crank levers 16, the other arms of which are connected to the slats by rods 15. The slots in this case are formed automatically due to the aerodynamic forces acting on the wing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB29736/33A GB416879A (en) | 1933-10-26 | 1933-10-26 | Improvements in or relating to the control of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB29736/33A GB416879A (en) | 1933-10-26 | 1933-10-26 | Improvements in or relating to the control of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB416879A true GB416879A (en) | 1934-09-24 |
Family
ID=10296322
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29736/33A Expired GB416879A (en) | 1933-10-26 | 1933-10-26 | Improvements in or relating to the control of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB416879A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5100081A (en) * | 1986-10-08 | 1992-03-31 | Dieter Thomas | Aircraft control system |
CN111284728A (en) * | 2018-12-06 | 2020-06-16 | 波音公司 | Flight control cable sensor for aircraft |
-
1933
- 1933-10-26 GB GB29736/33A patent/GB416879A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5100081A (en) * | 1986-10-08 | 1992-03-31 | Dieter Thomas | Aircraft control system |
CN111284728A (en) * | 2018-12-06 | 2020-06-16 | 波音公司 | Flight control cable sensor for aircraft |
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