GB710376A - Improved lever and cable assemblies - Google Patents
Improved lever and cable assembliesInfo
- Publication number
- GB710376A GB710376A GB2530151A GB2530151A GB710376A GB 710376 A GB710376 A GB 710376A GB 2530151 A GB2530151 A GB 2530151A GB 2530151 A GB2530151 A GB 2530151A GB 710376 A GB710376 A GB 710376A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- nipple
- hole
- lug
- slot
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C1/00—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
- F16C1/10—Means for transmitting linear movement in a flexible sheathing, e.g. "Bowden-mechanisms"
- F16C1/12—Arrangements for transmitting movement to or from the flexible member
- F16C1/16—Arrangements for transmitting movement to or from the flexible member in which the end-piece is guided rectilinearly
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Mechanical Engineering (AREA)
- Mechanical Control Devices (AREA)
Abstract
710,376. Control lever mechanism. DUNLOP RUBBER CO., Ltd., and TREVASKIS, H. W. Sept. 2, 1952 [Oct. 30, 1951], No. 25301/51. Class 136(1) [Also in Group XXXIII] A control mechanism comprises a control handle 1, a lever 2 pivotally mounted on the handle 1, a nipple 10 rotatably fitted in a hole in the lever, an operating wire cable 9 having one end secured to the nipple and passing through a hole in a lug 3 projecting from the control handle, and a guide arm 13 provided at one end with a slot 14 which fits over diametrically opposite flats on an extension 11 of the nipple and at the other end with an inturned portion 17 slidable in a slot 18 in the lug 3, the slot being parallel to the hole in the lug. The guide arm 13 is retained on the nipple 10 by a split pin 15 which passes through a hole 16 extending between the flats. The guide arm, the flats on the nipple and the slot 18 in the lug 3 are all in axial alignment with the adjacent end of the wire 9. On angular displacement of the lever 2 the cable 9 is tensioned and the nipple is rotated relative to the hole in the lever. The maximum angular motion of the lever may be varied by means of an adjustable stop 6.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2530151A GB710376A (en) | 1951-10-30 | 1951-10-30 | Improved lever and cable assemblies |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2530151A GB710376A (en) | 1951-10-30 | 1951-10-30 | Improved lever and cable assemblies |
Publications (1)
Publication Number | Publication Date |
---|---|
GB710376A true GB710376A (en) | 1954-06-09 |
Family
ID=10225480
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2530151A Expired GB710376A (en) | 1951-10-30 | 1951-10-30 | Improved lever and cable assemblies |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB710376A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2152450A (en) * | 1984-01-10 | 1985-08-07 | Kenneth Horatio Wallis | Improvements in or relating to rotary winged aircraft |
EP1255061A2 (en) * | 2001-04-28 | 2002-11-06 | ArvinMeritor Light Vehicle Systems (UK) Ltd | Cable linkage |
FR2903659A1 (en) * | 2006-07-12 | 2008-01-18 | Airbus France Sas | Aircraft flight and brake control system i.e. stick controller, has sensors generating steering control, from movement of handle, acting on aerodynamic surfaces, and spring associated to brake lever to act on brake system of landing gear |
-
1951
- 1951-10-30 GB GB2530151A patent/GB710376A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2152450A (en) * | 1984-01-10 | 1985-08-07 | Kenneth Horatio Wallis | Improvements in or relating to rotary winged aircraft |
EP1255061A2 (en) * | 2001-04-28 | 2002-11-06 | ArvinMeritor Light Vehicle Systems (UK) Ltd | Cable linkage |
EP1255061A3 (en) * | 2001-04-28 | 2004-07-14 | ArvinMeritor Light Vehicle Systems (UK) Ltd | Cable linkage |
FR2903659A1 (en) * | 2006-07-12 | 2008-01-18 | Airbus France Sas | Aircraft flight and brake control system i.e. stick controller, has sensors generating steering control, from movement of handle, acting on aerodynamic surfaces, and spring associated to brake lever to act on brake system of landing gear |
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