產品概況:
Master cylinders are located in the cockpit on each of the pilot’s rudder pedals. They are used to turn a force into a pressure to actuate the brakes on an aircraft. By integrating the reservoir directly into the master cylinder housing, Parker has eliminated the need for a separate, remotely mounted reservoir.
There are several advantages to this fewer fittings translates into fewer possible leak paths and the elimination of the need to find a remote location for a reservoir in a space-limited aircraft. This also means there are fewer parts to inspect and maintain, no need for a hydraulic line between the remote reservoir and the master cylinder, and weight savings.
Parker offers a version with a reservoir designed into the cylinder. It eliminates the need for a remote reservoir located in the firewall area, giving easier control over the system and less line from the brake assembly.
The reservoir capacity ranges from 2 to 3.4 cubic inches with strokes from 1.2 to 1.75 inches. Total volumetric output is 0.36 to 0.77 cubic inches. Ports are 1/8-27 NPT thread, which is common in the general aviation market.
APPLICATIONS:
General aviation, light jets, turboprop passenger and cargo aircraft.
FEATURES AND ATTRIBUTES:
? Fewer fittings, meaning fewer leak paths
? Space-saving advantage, no need for a remote reservoir
? Fewer parts to inspect and maintain
? Aluminum housing offers weight savings
? Anodized housing and stainless steel rod provides corrosion protection
? No hydraulic line required connecting remote reservoir and master cylinder
? Adjustable clevis allows length adjustment for ease of installation on aircraft
? Nitrile seals accommodate multiple fluids
? American made
OPTIONAL FEATURES:
? Rod ends
? Fitting types
? Bore sizes
? Strokes
? Reservoir volume
性能特點:
滿足工業標準
| |
MIL-PRF-5606, MIL-PRF-83282 and MIL-PRF-87257 |
重量(磅)
| |
0.32 to 1.05 |
殼體材料
| |
Aluminum |
桿子類型
| |
Stainless steel |
排量(cu in/rev)
| |
0.42 to 1.015 |
長度(英寸)
| |
5.25 to 11.535 |