GB549211A - Improvements in or relating to fluid pressure remote control systems - Google Patents
Improvements in or relating to fluid pressure remote control systemsInfo
- Publication number
- GB549211A GB549211A GB593841A GB593841A GB549211A GB 549211 A GB549211 A GB 549211A GB 593841 A GB593841 A GB 593841A GB 593841 A GB593841 A GB 593841A GB 549211 A GB549211 A GB 549211A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- pipes
- valves
- flow
- jacks
- 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
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
Abstract
549,211. Hydraulic machines ; valves. CLEVELAND, F. J. (Bendix Aviation Corporation). May 7, 1941, No. 5938. [A Specification was laid open to inspection under Sect. 91 of the Acts, Nov. 8, 1941.] [Classes 69 (ii) and 135] [Also in Group XXXIII] For synchronizing the movements of two or more elements of an aircraft control or a landing gear a self-adjusting valve described below is inserted between the pump and the power cylinders of a hydraulic servomotor to secure equality of flow to the cylinders. A system is described comprising two double-acting jacks fed through two reversing valves from pipes 38, 39 leading from a valve casing 22 supplied with pressure fluid through a pipe 21. Passages 23, 24, 25 are formed in the walls of the casing which has a cylindrical liner 27 in which slides a grooved piston 26. Holes 33, 34 in the liner admit pressure fluid to the grooves in the piston, the fluid issuing through longitudinally arranged narrow slits 36, 37 in the liner to the passages 24, 25 and the pipes 38, 39. Any increase of flow through one slit or the other causes a fall of pressure in the passages 24 or 25 and consequently on the corresponding end of the piston which then moves to correct the inequality. This subject-matter appears also in the Specification, corresponding to the Provisional Specification, placed open to inspection under Sect. 91 on the 8th November, 1941. The following subjectmatter appears only in the Specification as accepted. Fig. 4 shows a modified valve in which pressure fluid through a pipe 21a can flow directly to a passage 60 and past non-return valves 54 55 to the pipes 38a, 39a, but return flow through the two pipes 38a, 39a, is equalized by the valve 26 which is similar to that shown in Fig. 1 except that it has a single central groove 49. Two such valve devices are shown in Fig. 6 connected to opposite ends of two jacks 13, 14 the two inlets 21a being connected by pipes 66, 67 to a valve 65. This valve places the two pipes alternatively into communication with the pressure and reservoir sides 64, 68 of a pump system including an accumulator 62 and in either case the return flow from the jacks is controlled by one of the valves 26 while the pressure fluid has free access through the valves 54, 55 to the appropriate ends of the two jacks. Should unequal but proportionate flow through the two branches be required the slits 36, 37 are made of different shapes or sizes or the areas of the valve ends exposed to the fluid pressure may differ.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB593841A GB549211A (en) | 1941-05-07 | 1941-05-07 | Improvements in or relating to fluid pressure remote control systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB593841A GB549211A (en) | 1941-05-07 | 1941-05-07 | Improvements in or relating to fluid pressure remote control systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB549211A true GB549211A (en) | 1942-11-11 |
Family
ID=9805435
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB593841A Expired GB549211A (en) | 1941-05-07 | 1941-05-07 | Improvements in or relating to fluid pressure remote control systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB549211A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2415603A (en) * | 1943-08-26 | 1947-02-11 | Hydraulic Dev Corp Inc | Hydraulic constant speed control system for parallel-connected hydraulic motors |
US2423264A (en) * | 1943-04-28 | 1947-07-01 | Hydraulic Control Engineering | Equalizing valve |
US3015338A (en) * | 1958-10-07 | 1962-01-02 | Bendix Corp | Flow divider |
US3305037A (en) * | 1964-08-21 | 1967-02-21 | Int Harvester Co | Control valve for track laying tractor |
CN103527540A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | Pressure selector valve applied to undercarriage |
CN104482105A (en) * | 2014-12-30 | 2015-04-01 | 哈尔滨通航科技开发有限公司 | Air inflation device for high-pressure chamber and low-pressure chamber of buffering strut of aircraft landing gear |
-
1941
- 1941-05-07 GB GB593841A patent/GB549211A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423264A (en) * | 1943-04-28 | 1947-07-01 | Hydraulic Control Engineering | Equalizing valve |
US2415603A (en) * | 1943-08-26 | 1947-02-11 | Hydraulic Dev Corp Inc | Hydraulic constant speed control system for parallel-connected hydraulic motors |
US3015338A (en) * | 1958-10-07 | 1962-01-02 | Bendix Corp | Flow divider |
US3305037A (en) * | 1964-08-21 | 1967-02-21 | Int Harvester Co | Control valve for track laying tractor |
CN103527540A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | Pressure selector valve applied to undercarriage |
CN104482105A (en) * | 2014-12-30 | 2015-04-01 | 哈尔滨通航科技开发有限公司 | Air inflation device for high-pressure chamber and low-pressure chamber of buffering strut of aircraft landing gear |
CN104482105B (en) * | 2014-12-30 | 2016-03-09 | 哈尔滨通航科技开发有限公司 | Undercarriage damper leg high low pressure chamber charger |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2643664A (en) | Flow dividing valve | |
US2651491A (en) | Shuttle valve | |
GB1092422A (en) | A piston and cylinder arrangement with three stable positions | |
GB909953A (en) | Hydraulic selector valve | |
US2286880A (en) | Hydraulic control system | |
GB1306886A (en) | Hydraulic motor control circuit | |
ES356164A1 (en) | Pressure vessel | |
US2466485A (en) | Valve | |
GB549211A (en) | Improvements in or relating to fluid pressure remote control systems | |
US2940262A (en) | Hydraulic cross-regenerative circuit | |
US2445781A (en) | Control system for multiple hydraulic hoists | |
US2577999A (en) | Reversing valve | |
US2501661A (en) | Apparatus and system for fluid control | |
GB634362A (en) | Improvements in and relating to fluid valve constructions | |
GB583198A (en) | Improvement in shuttle valve | |
GB1182037A (en) | Improvements in or relating to fluid control valves | |
US2642087A (en) | Valve mechanism | |
GB701513A (en) | Hydraulic control valve | |
US2985190A (en) | Pilot valves having circular outlet ports modified to have the gain characteristics of square ports | |
GB559656A (en) | Improvements in or relating to valves | |
US2232467A (en) | Compound valve | |
US3003478A (en) | Pilot-operated selector valve | |
GB598279A (en) | Volume compensator for hydraulic systems | |
GB1175213A (en) | Draw Off Device for Viscous Materials. | |
GB536018A (en) | Improvements in and relating to hydraulic power transmission systems |