1. A spindle removal tool which comprises:
(a.) a flat semicircular plate with symmetrically spaced openings extending through said plate as a top section;
(b.) a transitional plate securely attached to the lowest segment of said semicircular plate as a middle section;
(c.) a support bar securely attached to said transitional plate as a bottom section; and
(d.) whereby the top, middle, and bottom sections are aligned on a vertical axis in a nearly Y-shape structure.
2. The tool as claimed in claim 1, wherein said semicircular plate is provided with five openings to accommodate a semi truck’s lug bolts.
3. The tool as claimed in claim 1, wherein said transitional plate is offset approximately 45 degrees from the vertical axis.
4. The tool as claimed in claim 1, wherein a narrow end of said support bar is milled down to fit a standard floor jack.
5. The tool as claimed in claim 1, wherein a narrow end of said support bar is milled down to fit a standard floor jack.
6. A spindle removal tool which comprises:
(a.) a flat semicircular plate with five symmetrically spaced openings extending through said plate as a top section;
(b.) a transitional plate welded to the lowest segment of said semicircular plate as a middle section;
(c.) a support bar welded to said transitional plate as a bottom section; and
(d.) whereby the top, middle, and bottom sections are aligned on a vertical axis in a nearly Y-shape structure.
7. The tool as claimed in claim 6, wherein lug bolts fasten said semicircular plate securely against a hub.
8. The tool as claimed in claim 6, wherein said transitional plate is offset approximately 45 degrees from the vertical axis.
9. The tool as claimed in claim 6, wherein a narrow end of said support bar is milled down to fit a standard floor jack.
10. The tool as claimed in claim 6, wherein a narrow end of said support bar is milled down to fit a standard floor jack.
11. A spindle removal tool which comprises:
(a.) a top section comprising a flat semicircular plate with symmetrically spaced openings extending through said plate;
(b.) a middle section comprising a means to securely attach the lowest segment of said top section to a bottom section;
(c.) a bottom section comprising a support bar; and
(d.) whereby the top, middle, and bottom sections are aligned on a vertical axis in a nearly Y-shape structure.
12. The tool as claimed in claim 11, wherein lug bolts fasten said semicircular plate securely against a hub.
13. The tool as claimed in claim 11, wherein said transitional plate is offset approximately 45 degrees from the vertical axis.
14. The tool as claimed in claim 11, wherein a narrow end of said support bar is milled down to fit a standard floor jack.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. An aircraft door actuator, including:
a pneumatic cylinder comprising:
a piston moving between first and second extreme positions in a body of the cylinder, corresponding respectively to the closing and the opening of the door,
a variable volume chamber into which a pressurized gas is injected via a first port for the displacement of the piston from the position closing the door to the position opening it,
one of two elements, the piston and the body of the cylinder, being connected to the door, the other to the frame,
means for supplying said chamber of the cylinder with pressurized gas, via a supply pipe connected to the chamber by said first port,
means for setting the chamber to atmospheric pressure when the piston is in the position for opening the door, so as to allow said door to be moved into the closed position,
in which door actuator said means for setting the chamber to atmospheric pressure include:
a pressurized gas exhaust pipe, one end of which is connected to said chamber via said first port, and the opposite end of which is connected to atmospheric pressure,
a gate-valve, a body of which is arranged in series over said exhaust pipe, and an obturator of which adopts at least the two following positions:
a position for closing the exhaust pipe,
a position for opening the exhaust pipe,
means for guiding the obturator of the gate-valve, comprising a principal fluid pipe for controlling the displacement of the obturator from the position for closing the exhaust pipe toward its position for opening, one end of which is connected to the body of the gate-valve in such a manner that the fluid located in said principal fluid pipe exerts a force on the obturator, and the other end of which is connected to a second port formed in the chamber of the cylinder and arranged in such a manner that said second port is situated outside the chamber when the piston is in the position for closing the door, or is in the process of opening said latter, and is situated in the chamber when the door is in the position for opening so as to actuate, in said second position of the piston, the obturator of the gate-valve by means of the compressed gas present in the chamber and in this way to open said exhaust pipe so as to set the chamber of the cylinder to atmospheric pressure in a rapid manner once the door has been opened.
2. The aircraft door actuator as claimed in claim 1, in which said means for guiding the obturator of the gate-valve also include a secondary fluid pipe for continuing the guiding of the obturator of the gate-valve, a first end of which is connected to a port opening out into a chamber of the gate-valve, defined between the gate-valve body and the obturator, with variable volume, which is formed when the obturator has started to move from the position for closing the exhaust pipe toward the position for opening said exhaust pipe in such a manner that the gas contained in said secondary fluid pipe exerts a force on the obturator in order to hold said latter in the position for opening the exhaust pipe, and the second end of which is connected to means for supplying said chamber of the cylinder with pressurized gas.
3. The aircraft door actuator as claimed in claim 2, also including a device for expanding the pressurized gas originating from said means for supplying the chamber of the cylinder with pressurized gas, disposed in series over said supply pipe.
4. The aircraft door actuator as claimed in claim 3, in which said secondary fluid pipe for continuing the guiding of the obturator of the gate-valve is connected to said pipe for supplying pressurized gas, upstream of said device for expanding the pressurized gas.
5. The aircraft door actuator as claimed in claim 1, in which said pressurized gas exhaust pipe comprises a fluid part which is shared with said supply pipe.
6. The aircraft door actuator as claimed in claim 1, in which said gate-valve of the means for setting the chamber to atmospheric pressure comprises a resilient means for resetting the obturator, with the exhaust pipe in the closed position.
7. The aircraft door actuator as claimed in claim 1, in which said means for supplying the chamber of the cylinder with pressurized gas include a pressurized gas tank.
8. The aircraft door actuator as claimed in claim 1, in which said means for supplying the chamber of the cylinder with pressurized gas include a pyrotechnic gas generator.
9. The aircraft door actuator as claimed in claim 2, in which said pressurized gas exhaust pipe comprises a fluid part which is shared with said supply pipe.
10. The aircraft door actuator as claimed in claim 3, in which said pressurized gas exhaust pipe comprises a fluid part which is shared with said supply pipe.
11. The aircraft door actuator as claimed in claim 4, in which said pressurized gas exhaust pipe comprises a fluid part which is shared with said supply pipe.
12. The aircraft door actuator as claimed in claim 2, in which said gate-valve of the means for setting the chamber to atmospheric pressure comprises a resilient means for resetting the obturator, with the exhaust pipe in the closed position.
13. The aircraft door actuator as claimed in claim 3, in which said gate-valve of the means for setting the chamber to atmospheric pressure comprises a resilient means for resetting the obturator, with the exhaust pipe in the closed position.
14. The aircraft door actuator as claimed in claim 4, in which said gate-valve of the means for setting the chamber to atmospheric pressure comprises a resilient means for resetting the obturator, with the exhaust pipe in the closed position.
15. The aircraft door actuator as claimed in claim 5, in which said gate-valve of the means for setting the chamber to atmospheric pressure comprises a resilient means for resetting the obturator, with the exhaust pipe in the closed position.
16. The aircraft door actuator as claimed in claim 2, in which said means for supplying the chamber of the cylinder with pressurized gas include a pressurized gas tank.
17. The aircraft door actuator as claimed in claim 3, in which said means for supplying the chamber of the cylinder with pressurized gas include a pressurized gas tank.
18. The aircraft door actuator as claimed in claim 4, in which said means for supplying the chamber of the cylinder with pressurized gas include a pressurized gas tank.