Hydraulic piston pump/motor with non-cantilevered pistons
A hydraulic piston motor/pump includes a first rotor including a first cylinder, a second rotor opposing the first rotor and including a second cylinder that opposes the first cylinder, a first swashplate including a first angled face adjacent the first rotor, a second swashplate adjacent the second rotor and opposing the first swashplate. The hydraulic piston motor/pump further includes a first shoe cage including a first piston opening, a second shoe cage including a second piston opening, a piston configured to travel into and out of the first cylinder and the second cylinder, a piston shoe configured to engage the piston, the first shoe cage, and the second shoe cage, and a shaft engaging the first shoe cage and the second shoe cage. The shaft configured to rotate in response to a rotation of the first shoe cage and the second shoe cage.
1 . A hydraulic piston motor, comprising:
a first rotor including a first cylinder;
a second rotor opposing the first rotor, the second rotor including a second cylinder opposing the first cylinder;
a first swashplate adjacent the first rotor, the first swashplate including a first angled face;
a second swashplate adjacent the second rotor and opposing the first swashplate;
a first shoe cage including a first piston opening, the first shoe cage disposed adjacent the first angled face of the first swashplate;
a second shoe cage including a second piston opening, the second shoe cage adjacent the first shoe cage;
a piston configured to travel into and out the first cylinder and the second cylinder and to pass through the first piston opening and the second piston opening;
a piston shoe configured to engage the piston, the first shoe cage, and the second shoe cage; and
a shaft engaging the first shoe cage and the second shoe cage and configured to rotate in response to a rotation of the first shoe cage and the second shoe cage.
2 . The hydraulic piston motor of claim 1 , wherein the second swashplate includes a second angled face that is parallel to the first angled face of the first swashplate.
3 . The hydraulic piston motor of claim 2 , wherein the second shoe cage is disposed adjacent to and engages the second angled face of the second swashplate.
4 . The hydraulic piston motor of claim 1 , wherein the shaft includes a first cylindrical end, a second cylindrical end, and a spherical center between the first cylindrical end and the second cylindrical end, wherein the first shoe cage and the second shoe cage are configured to engage the spherical center.
5 . The hydraulic piston motor of claim 1 , wherein the piston includes a first cylindrical end, a second cylindrical end, and a spherical center between the first cylindrical end and the second cylindrical end, wherein the first shoe cage and the second shoe cage engage the spherical center of the piston via the piston shoe.
6 . The hydraulic piston motor of claim 1 , wherein the piston shoe includes a first piston shoe and a second piston shoe.
7 . The hydraulic piston motor of claim 1 , further comprising a plurality of bolts to couple the first shoe cage to the second shoe cage.
8 . The hydraulic piston motor of claim 1 , wherein the first rotor includes a first center opening, the second rotor includes a second center opening, the first shoe cage includes a first shaft opening, and the second shoe cage includes a second shaft opening, wherein the shaft passes through the first center opening, the first shaft opening, the second shaft opening, and the second center opening.
9 . The hydraulic piston motor of claim 1 , further comprising:
a first wear plate disposed on the first angled face and between the first angled face and the first shoe cage.
10 . The hydraulic piston motor of claim 9 , wherein the first swashplate includes a first material having a first weight and the first wear plate includes a second material having a second weight that is greater than the first weight.
11 . An aircraft, comprising:
a nose landing gear assembly including a hydraulic piston motor, the hydraulic piston motor including:
a first rotor including a first cylinder;
a second rotor opposing the first rotor, the second rotor including a second cylinder opposing the first cylinder;
a first swashplate adjacent the first rotor, the first swashplate including a first angled face;
a second swashplate adjacent the second rotor and opposing the first swashplate;
a first shoe cage including a first piston opening, the first shoe cage disposed adjacent the first angled face of the first swashplate;
a second shoe cage including a second piston opening, the second shoe cage adjacent the first shoe cage;
a piston configured to travel into and out of the first cylinder and the second cylinder and to pass through the first piston opening and the second piston opening;
a piston shoe configured to engage the piston, the first shoe cage, and the second shoe cage; and
a shaft engaging the first shoe cage and the second shoe cage and configured to rotate in response to a rotation of the first shoe cage and the second shoe cage.
12 . The aircraft of claim 11 , wherein the second swashplate includes a second angled face that is parallel to the first angled face of the first swashplate.
13 . The aircraft of claim 12 , wherein the second shoe cage is disposed adjacent to and engages the second angled face of the second swashplate.
14 . The aircraft of claim 11 , wherein the shaft includes a first cylindrical end, a second cylindrical end, and a spherical center between the first cylindrical end and the second cylindrical end, wherein the first shoe cage and the second shoe cage are configured to engage the spherical center.
15 . The aircraft of claim 11 , wherein the piston includes a first cylindrical end, a second cylindrical end, and a spherical center between the first cylindrical end and the second cylindrical end, wherein the first shoe cage and the second shoe cage engage the piston via the spherical center.
16 . The aircraft of claim 11 , wherein the piston shoe includes a first piston shoe and a second piston shoe, the first piston shoe configured to engage the second shoe cage via the second piston shoe, and the second piston shoe configured to engage the first shoe cage via the first piston shoe.
17 . The aircraft of claim 11 , wherein the hydraulic piston motor further comprises a plurality of bolts to couple the first shoe cage to the second shoe cage.
18 . The aircraft of claim 11 , wherein the first rotor includes a first center opening, the second rotor includes a second center opening, the first shoe cage includes a first shaft opening, and the second shoe cage includes a second shaft opening, wherein the shaft passes through the first center opening, the first shaft opening, the second shaft opening, and the second center opening.
19 . The aircraft of claim 11 , wherein the hydraulic piston motor further comprises:
a first wear plate disposed on the first angled face and between the first angled face and the first shoe cage.
20 . The aircraft of claim 19 , wherein the first swashplate includes a first material having a first weight and the first wear plate includes a second material having a second weight that is greater than the first weight.