Hilton Bonneted Knife Gate Valves (H-200-B)
Hilton Bonneted Knife Gate Valves provide performance, economy and rugged construction for a broad range of water and industrial applications including Water, Wastewater, Paper, Mining, Power and Hydro Dams. A leader in fabricated valve technology, Hilton offers standard Bonneted Knife Gate Valves in sizes 2-96", and custom fabricated valves to 144" with higher pressures and temperature capabilities to meet particular application requirements.
Bonneted Knife Gate Valves can be built to U.S. or international standards, and are available with wafer or special extended face-to-face dimensions for replacement of existing valves. Bonnets can be pressurized or un-pressurized, and can be specified with optional flushing or drain ports. A back seat seal ring on all bonneted valves allows valves to be repacked without valve disassembly and with the valve in the pipeline under pressure.
Bonneted Knife Gate Valves (H-200-B) Specifications
Standard designs to 96” (2400mm)
Custom designs through 144" (3600mm)
Standard designs to 400°F (204°C)
Custom designs from -40 to 2000°F (-40 to 1093°C)
2-24” (50-600mm) = 150 psi CWP (1030 kPa)
30-96” (750-2400mm) = 50 psi CWP (340 kPa)
Custom designs up to 400 psi (2800 kPa)
Metal or Resilient, uni-directional or bi-directional with options for removable seat, inflatable seal or grease seal
Standard valves are available in Carbon Steel or 304 Stainless Steel. Custom designs are available with solid or wetted parts construction in any weldable alloy, including Stainless Steel, Hastelloy, Inconel, Monel and Titanium.
Optional abrasion and corrosion resistant materials available including hard facing available in cobalt-chromium alloy, tungsten carbide, pulse fusion
H-200, MSS SP-81, TAPPI TIS 405-9
H-240-B, Narrow Face to Face (Canadian Standard)
H-260-B, ANSI Face to Face
Non-Standard Face to Face
Application Solutions (English)
- Hilton Compact Designed Bonneted Knife Gate Valve Application Solution 207
- Hilton Cooling Water Isolation Valves at NASA Rocket Test Facility Application Solution 210