Arrow indicates the locations of the thrust puck and the catcher thrust puck on the extended strut which are behind where the conventional thrust box strut would end. Traditionally, weight is added to the fire apparatus e. Get more of what you love Follow more accounts to get instant updates about topics you care about. The rear torque box is designed to "box in" the area just in front of the rear leaf spring front hanger. The apparatus according to claim 1wherein the at least one active forward link comprises first and second active forward links for constraining vertical load forces and roll moment, and wherein the at least one forward link catcher comprises a forward link catcher positioned between the first and second active forward links. According to the exemplary embodiment shown in FIGS. According to an exemplary embodiment, the aerial ladder assembly of the quint configuration fire apparatus is operable at a vertical extension height of at least 95 feet e. Torque box struts having an extension of the aft mount have been proposed.
While speaking with BCFD members while picking up donations, Box asked what more it could provide to further assist firefighters and the overwhelming.
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Go watch a high horsepower leaf spring Mopar launch at the drag strip and you will see the rear body separation over the rear tires; there is a lot of "up" force!
Aircraft can be implemented as aircraft in FIG. In alternative embodiments, the engine 60 is another type of device e.
USA1 Fail safe extended torque box struttowing mount Google Patents
In one embodiment, the first side wall of the torque box is flush with the laterally-outward facing surface of the first frame rail 11 and the second side wall of the torque box is flush with the laterally-outward facing surface of the second frame rail In one advantageous embodiment of the present disclosure, an apparatus for mounting an aircraft engine to a wing comprises a torque box strut for supporting the aircraft engine, and a strut-to-wing mounting system for attaching the torque box strut to the wing of an aircraft.
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|The apparatus according to claim 1wherein the aft link catcher and the forward link catcher do not attach the torque box strut to the wing during the normal aircraft operation.
Stay tuned. Reach may include the horizontal distance from the point of rotation e. The aerial ladder assembly is supported by the cylinders 56 and by the turntable at the first end Such loading transfer may convey the loading into stability devices e.
Torque Box. that is similar to a fluid coupling but that produces, by means of additional turbine blades, variable torque multiplication. NFPA, ed.
USB2 Pedestal and torque box assembly for a fire apparatus Google Patents
The torque box extends along the longitudinal direction and spans the single rear The plate includes a first walla first legand a second leg
If, however, thrust puck should fail, strut will move forward slightly to cause thrust puck to engage recess and become active and take up the thrust and side load forces normally taken up by thrust puck About Search query Search Twitter. JPA en. Tweets Tweets, current page.
The actuator may be a linear actuator, a rotary actuator, or still another type of device and may be powered hydraulically, electrically, or still otherwise powered. The method according to claim 14wherein the aft link catcher and the forward link catcher do not attach the torque box strut to the wing during the normal aircraft operation, and wherein the catcher thrust puck is inactive during the normal aircraft operation.
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