Adaptive fluid mount
AssigneeLord Corporation
InventorsPeter J. Jones, Marshall W. Downing
Life of this patent
Estimating the term…
Abstract
A double pumper mount useful as a front mount for an aircraft engine. A pair of fluid chambers are selectively interconnectable by one of a plurality of inertia tracks by use of an adjustable cylindrical member which has the tracks formed as generally helical grooves extending about the periphery of the cylindrical member. These inertia tracks have different flow characteristics so as to produce differing notch frequencies so as to attenuate different vibrational frequencies. A second embodiment has a single inertia track whose length can be altered by rotating the cylindrical member to change the point at which the ingress/egress port of the fluid chamber engages the circumferential portion of the inertia track.
Claims15
A resilient hydraulic mount for use as a component in a system for connecting a vibrating member such as an engine to a support, said resilient mount comprising:
- a) a rigid frame member adapted to be attached to said support;
- b) a rigid connector for supporting said vibrating member;
- c) an elastomeric element for isolating said rigid connector from said rigid frame member, said elastomeric element including
- i) a first fluid chamber having a first ingress/egress port;
- ii) a second fluid chamber having a second ingress/egress port;
- iii) a plurality of fluid inertia tracks which can be selectively interconnected between said first and second ingress/egress ports, each of said fluid inertia tracks including a first terminal end portion connectable with said first ingress/egress port and a second terminal end portion which is simultaneously connectable with said second ingress/egress port;
- and
- d) means to select which of said plurality of fluid inertia tracks is interconnected with said first and second ingress/egress ports without a need to break down the system into its components thereby avoiding a resultant loss of hydraulic fluid.
A resilient hydraulic mount for use as a component in a system for connecting a vibrating member such as an aircraft engine to a support, said resilient mount comprising:
- a) a rigid frame member adapted to be attached to said support;
- b) a rigid connector for supporting said vibrating member;
- c) an elastomeric element for isolating said rigid connector from said rigid frame member, said elastomeric element including
- i) a first fluid chamber having a first ingress/egress port;
- ii) a second fluid chamber having a second ingress/egress port;
- iii) a cylindrical adjustable member having a passageway for interconnecting said first and second fluid chambers, said passageway including an inertia track formed as a groove extending about the periphery of said cylindrical adjustable member, said groove having a first circumferential portion and a second helical portion, said circumferential portion affording a means of adjusting a point of connection of said first ingress/egress port with said passageway of said adjustable member, and a large annular groove extending about the cylindrical adjustable member at an opposite end of said helical portion, said large circumferential groove being of sufficient dimension to substantially eliminate its contribution to the fluid inertia of said passageway interconnecting said first and second ingress/egress ports;
- d) means for adjusting said adjustable member to alter the point of connection of said first ingress/egress port to said passageway.
A resilient hydraulic mount for use as a component in a system for connecting a vibrating member such as an aircraft engine to a support, said resilient mount comprising:
- a) a rigid frame member adapted to be attached to said support;
- b) a rigid connector for supporting said vibrating member;
- c) an elastomeric element for isolating said rigid connector from said rigid frame member, said elastomeric element including
- i) a first fluid chamber having a first ingress/egress port at a first position;
- ii) a second fluid chamber having a second ingress/egress port at a second position which is laterally and angularly displaced from said first position;
- iii) a cylindrical adjustable member having at least one passageway for interconnecting said first and second fluid chambers, said at least one passageway including at least one inertia track formed as a groove extending about the periphery of said cylindrical adjustable member, said groove including a helical portion, a first terminal end portion for connecting to said first ingress/egress port and a second terminal end portion for connecting to said second ingress/egress port;
- d) means for adjusting a length to area ratio of said inertia track to thereby alter the characteristics of said at least one inertia track, wherein said means for adjusting said length to area ratio comprises means for rotating said adjustable cylindrical member to vary a position at which said first ingress/egress port engages said first terminal end portion and to vary a position at which said second ingress/egress port engages said second terminal end portion.
Dependencies are inferred from the claim text.