GB678318A - Improvements relating to flight conveyors - Google Patents
Improvements relating to flight conveyorsInfo
- Publication number
- GB678318A GB678318A GB2474/50A GB247450A GB678318A GB 678318 A GB678318 A GB 678318A GB 2474/50 A GB2474/50 A GB 2474/50A GB 247450 A GB247450 A GB 247450A GB 678318 A GB678318 A GB 678318A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- conduit
- conveyer
- pressure
- flights
- 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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K7/00—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves
- F16K7/02—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with tubular diaphragm
- F16K7/04—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with tubular diaphragm constrictable by external radial force
- F16K7/07—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with tubular diaphragm constrictable by external radial force by means of fluid pressure
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Gasket Seals (AREA)
Abstract
678,318. Endless conveyers. HAPMAN, H. W. Jan. 31, 1950. [March 23, 1949] No. 2474/50. Class 78 (i). Also in Group XXVI] The invention relates to a pressure sealing device for insertion in a flight conveyer conduit for sealing the flights against the escape of pressure as the flights pass through the sealing device, thereby preventing air from getting into a chamber in communication with the conduit and through which the conveyer travels, the chamber being under a vacuum or partial vacuum, or preventing the escape of fluid from the chamber when this is under pressure. According to the invention the device comprises an outer tubular casing attachable in said conduit and an inner contractible tubular member adapted to be contracted into pressure-tight relationship with the conveyer flights, the space between the casing and the inner tubular member forming an n inflatable chamber, said tubular member comprising a .plurality of spaced longitudinal bars arranged in ring formation with strips of elastic deformable material mounted in the spaces between the bars. In the embodiment shown in Figs. 1, 2 the sealing device 10 is inserted in a gap between portions 11, 12 of a conveyer conduit. It consists of a tubular member 19 and a deformable member 36 builtup of metal and rubber strips 37, 38 surrounded by a, rubber tube 39 and spaced from the member 19 to form a chamber 50 into which fluidpressure is introduced to force the member 36 into contact with the peripheral edges of the conveyer flights. The member 19 is welded at 20, 21, 22 to flanges 17, 18 which are bolted at 15, 16 to flanges 13, 14 on the conduit portions 11, 12, whilst the member 36 is provided at its ends with rings 34, 44 secured within recesses 30, 31 in the member 10 and provided with sealing rings 48, 49. The ends of the bars 37, 38 are provided with projections 40, 42 which engage in recesses 41, 43 in the rings 34, 44. The member 19 is provided with coupling members 25, 26 for connecting inlet and outlet pipes for pressure fluid introduced into the chamber 50. This fluid may comprise steam, compressed air or a cooling liquid. In a modification, Fig. 3, the deformable member 62 is provided with a rubber sleeve 64 formed with a securing flange 63, the sleeve preventing exposure of the metal strips 37 to the conveyed material.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US678318XA | 1949-03-23 | 1949-03-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB678318A true GB678318A (en) | 1952-09-03 |
Family
ID=22078703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2474/50A Expired GB678318A (en) | 1949-03-23 | 1950-01-31 | Improvements relating to flight conveyors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB678318A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0175028A1 (en) * | 1984-09-19 | 1986-03-26 | Mil Mutzarim Techniim (1971) B.M. | Hydraulic cut-off or throttling valve |
EP0436241A2 (en) * | 1989-12-11 | 1991-07-10 | Johannes Bernadus Ratelband | Diaphragm valve comprising a sleeve-shaped elastic diaphragm |
-
1950
- 1950-01-31 GB GB2474/50A patent/GB678318A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0175028A1 (en) * | 1984-09-19 | 1986-03-26 | Mil Mutzarim Techniim (1971) B.M. | Hydraulic cut-off or throttling valve |
EP0436241A2 (en) * | 1989-12-11 | 1991-07-10 | Johannes Bernadus Ratelband | Diaphragm valve comprising a sleeve-shaped elastic diaphragm |
EP0436241A3 (en) * | 1989-12-11 | 1991-12-18 | Johannes Bernadus Ratelband | Diaphragm valve comprising a sleeve-shaped elastic diaphragm |
US5090660A (en) * | 1989-12-11 | 1992-02-25 | Ratelband Johannes B | Diaphragm valve comprising a sleeve-shaped elastic diaphragm |
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