1. A contra-rotating propeller unit including:
(a) a hollow outer shaft having a front propeller attached to a rear end thereof, and an inner shaft having a rear propeller attached to a rear end thereof and inserted into and supported in the outer shaft;
(b) a predetermined part on a rear side of the inner shaft that is supported by a contra-rotating rear bearing provided in a boss of the front propeller;
(c) an inner fixing tool that is detachably attached to a tip portion of the outer shaft to temporarily support the predetermined part on a front side of the inner shaft; and
(d) a contra-rotating thrust bearing provided in the boss of the front propeller to receive a thrust load from the outer shaft to transmit the thrust load to the inner shaft.
2. The contra-rotating propeller unit according to claim 1,
wherein the inner fixing tool has a guide body with an external diameter which is equal to or greater than the external diameter of the outer shaft and is smaller than the internal diameter of stern tube bearing parts, and the guide member is made of a material softer than the stern tube bearing part, and has a chamfered portion at the outer peripheral edge of the tip thereof.
3. The contra-rotating propeller unit according to claim 1, further comprising:
(c) an inner lifting tool detachably attached to a tip portion of the inner shaft and having a lifting piece provided at a tip or the tip portion.
4. The contra-rotating propeller unit according to claim 3,
wherein the inner shaft is formed in a hollow shape,
wherein lubricant oil passages of the same system are formed between the hollow portion of the inner shaft,
wherein the inner shaft and the outer shaft, a first seal member is provided between the inner fixing tool and the outer shaft, and a second seal member is provided between the inner fixing tool and the inner shaft,
wherein the third seal member is provided between the inner lifting tool and the inner shaft, and
wherein the inner lifting tool has an introduction oil passage for introducing lubricant oil into the hollow portion of the inner shaft.
5. The contra-rotating propeller unit according to claim 3,
wherein the contra-rotating propeller unit has a guide member with an external diameter which is greater than the external diameter of the tip portion of the inner shaft, and is smaller than the outer shaft, and the guide member is made of a material softer than the outer shaft, and has a chamfered portion at the outer peripheral edge of the tip thereof.
6. The contra-rotating propeller unit according to claim 1,
wherein the inner fixing tool has a construction that is radially splitable into a plurality of pieces.
7. The contra-rotating propeller unit according to claim 1, further comprising:
(e) a stern tube rear seal unit installed in the predetermined part on the rear side of the outer shaft, and a rear seal fixing tool attached to the outer shaft to temporarily fix the stern tube rear seal unit to the outer shaft.
8. The contra-rotating propeller unit according to claim 7,
wherein the rear seal fixing tool has a construction that is radially splitable into a plurality of pieces.
9. The contra-rotating propeller unit according to claim 1, further comprising:
(e) hollow stern tube inner cylinder that has stern tube bearing parts mounted thereon, has the outer shaft inserted thereinto, and supports the outer shaft;
(f) a stern tube rear seal unit attached to a rear end of the stern tube inner cylinder; and
(g) an outer fixing tool that is detachably attached to a tip portion of the stern tube inner cylinder, and temporarily supports the predetermined part on the front side of the outer shaft, and temporarily constrains the axial movement of the outer shaft with respect to the stern tube inner cylinder.
10. A method for assembling a contra-rotating propeller unit including a hollow outer shaft having a front propeller attached to a rear end thereof, and an inner shaft having a rear propeller attached to a rear end thereof and inserted into and supported in the outer shaft, wherein the method comprises the steps of:
(a) inserting the inner shaft into the outer shaft;
(b) assembling a contra-rotating thrust bearing for receiving a thrust load from the outer shaft to transmit the thrust load to the inner shaft into a boss of the front propeller, thereby constraining axial movement of the inner shaft with respect to the outer shaft;
(c) installing a contra-rotating rear bearing in the boss of the front propeller, and supporting a predetermined part on a rear side of the inner shaft by the contra-rotating rear bearing; and
(d) attaching an inner fixing tool to a tip portion of the outer shaft, and temporarily supporting the predetermined part on a front side of the inner shaft by the inner fixing tool.
11. A method for assembling a contra-rotating propeller unit including a hollow outer shaft having a front propeller attached to a rear end thereof, and an inner shaft having a rear propeller attached to a rear end thereof and inserted into and supported in the outer shaft, wherein the method comprises the steps of:
(a) inserting the outer shaft into a hollow stern tube inner cylinder mounted with stern tube bearing parts;
(b) attaching a stern tube rear seal unit to a rear end of the stern tube inner cylinder;
(c) attaching an outer shaft fixing tool to the stern tube inner cylinder, and temporarily supporting a predetermined part on a front side of the outer shaft by the outer fixing tool, and temporarily constraining axial movement of the outer shaft with respect to the stern tube inner cylinder;
(d) inserting the inner shaft into the outer shaft;
(c) assembling a contra-rotating thrust bearing for receiving the thrust load from the outer shaft to transmit the thrust load to the inner shaft into a boss of the front propeller, thereby constraining axial movement of the inner shaft with respect to the outer shaft;
(d) installing a contra-rotating rear bearing in the boss of the front propeller, and supporting the predetermined part on a rear side of the inner shaft by the contra-rotating rear bearing; and
(e) attaching an inner fixing tool to a tip portion of the outer shaft, and temporarily supporting the predetermined part on the front side of the inner shaft by the inner fixing tool.
12. The method for assembling a contra-rotating propeller unit according to claim 10, further comprising attaching an inner lifting tool having a lifting piece provided at the tip thereof, to a tip portion of the inner shaft.
13. The method for assembling a contra-rotating propeller unit according to claim 10, further comprising installing a stern tube rear seal unit in a predetermined part on the rear side of the outer shaft, and attaching a rear seal fixing tool to the outer shaft to temporarily fix the stern tube rear seal unit to the outer shaft.
14. The method for assembling a contra-rotating propeller unit according to claim 10,
wherein a contra-rotating propeller unit is assembled on a temporary placing base including an assembly lower base installed in an installation surface, and an upper receiving base detachably attached to the assembly lower base to support the outer shaft, and
wherein upper receiving bases with a plurality of kinds of sizes corresponding to the size of the outer shaft are allowed to be attached to the assembly lower base.
15. The method for assembling a contra-rotating propeller unit according to claim 11,
wherein a contra-rotating propeller unit is assembled on a temporary placing base including an assembly lower base installed in an installation surface, and an upper receiving base detachably attached to the assembly lower base to support the stern tube inner cylinder, and
wherein upper receiving bases with a plurality of kinds of sizes corresponding to the size of the stern tube inner cylinder are allowed to be attached to the assembly lower base.
16. A method for transporting the contra-rotating propeller unit according to claim 1,
wherein the contra-rotating propeller unit is assembled on a temporary placing base, and wherein the method comprises the steps of:
(a) placing the contra-rotating propeller unit and the temporary placing base on transportation means, wherein the assembled contra-rotating propeller unit is placed on the temporary placing base; and
(b) transporting the contra-rotating propeller unit and the temporary base by the transportation means.
17. The method for transporting the contra-rotating propeller unit according to claim 9,
wherein the contra-rotating propeller unit is assembled on a temporary placing base, and wherein the method comprises the steps of:
(a) placing the contra-rotating propeller unit and the temporary placing base on transportation means, wherein the assembled contra-rotating propeller unit is placed on the temporary placing base; and
(b) transporting the contra-rotating propeller unit and the temporary base by the transportation means.
18. A method for mounting on a mother ship the contra-rotating propeller unit transported by the method for transporting the contra-rotating propeller unit according to claim 16,
wherein the temporary placing base includes an assembly lower base installed in an installation surface, and an upper receiving base detachably attached to the assembly lower base to support the outer shaft,
wherein the fixation of the upper receiving base to the assembly lower base is released with the contra-rotating propeller unit supported by the upper receiving base, and the contra-rotating propeller unit is lifted parallel to the axial center of a stern tube by lifting the portion of the contra-rotating propeller unit behind a portion inserted into the stern tube inner cylinder of a mother ship, and the upper receiving base by the lifting means, and
wherein the lifted contra-rotating propeller unit is moved forward and inserted into the stern tube.
19. A method for mounting on a mother ship the contra-rotating propeller unit transported by the method for transporting the contra-rotating propeller unit according to claim 17,
wherein the temporary placing base includes an assembly lower base installed in an installation surface, and an upper receiving base detachably attached to the assembly lower base to support the outer shaft,
wherein the fixation of the upper receiving base to the assembly lower base is released with the contra-rotating propeller unit supported by the upper receiving base, and the contra-rotating propeller unit is lifted parallel to the axial center of a stern tube through hole by lifting the portion of the contra-rotating propeller unit behind the stern tube inner cylinder, and the upper receiving base by the lifting means, and
wherein the lifted contra-rotating propeller unit is moved forward and inserted into the stern tube through hole.
20. The contra-rotating propeller unit according to claim 2, further comprising:
(e) an inner lifting tool detachably attached to a tip portion of the inner shaft and having a lifting piece provided at a tip of the tip portion.
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. A method for forming a diode, the method comprising:
forming an oxide layer over a semiconductor substrate doped with a first type dopant;
forming a first recess in the oxide layer;
forming a silicon-containing plug in the first recess, the silicon-containing plug being doped with a second type dopant having a conductivity opposite to a conductivity of the first type dopant;
filling the first recess with a second silicon-containing material doped with the first type dopant;
forming a diode junction in the silicon-containing plug with diffused dopants from the second silicon-containing material silicon;
forming a second recess in an active region proximate the first recess, the second recess extending through the oxide layer to expose a portion of the active region of the doped semiconductor substrate;
filling the second recess with a third silicon-containing material doped with the second type dopant; and
forming a programmable resistor in contact with the second silicon-containing material.
2. The method of claim 1, wherein filling the first recess with a second silicon-containing material comprises filling the first recess with polysilicon.
3. The method of claim 1, wherein forming a diode junction comprises forming a diode junction by a heat treatment process.
4. The method of claim 1, further comprising forming a contact on the programmable resistor.
5. The method of claim 1, wherein forming a first recess in the oxide layer further comprises forming a first recess in a layer of material selected from the group consisting of silicon monoxide, silicon dioxide or silicon nitride.
6. The method of claim 1, wherein forming a silicon-containing plug further comprises growing an epitaxial silicon layer on an exposed surface of an active region of the doped semiconductor substrate.
7. The method of claim 6, wherein growing an epitaxial silicon layer comprises growing an epitaxial silicon layer having a thickness of about 1500 Angstroms to about 3000 Angstroms.
8. The method of claim 1, wherein forming a first recess in the oxide layer comprises simultaneously forming two adjacent holes within a P-minus active region of the doped semiconductor substrate.
9. The method of claim 1, further comprising forming metal row lines contacting the programmable resistor.
10. The method of claim 9, further comprising:
depositing a second oxide layer over doped metal row lines;
forming a channel in the second oxide layer to expose the third silicon-containing material;
depositing conductive material in the channel; and
depositing tungsten over the conductive material.
11. The method of claim 10, wherein the channel has a diameter larger than the second recess.
12. The method of claim 10, wherein the conductive material is a refractory metal.
13. The method of claim 10, wherein depositing tungsten further comprises:
depositing a first tungsten layer in the channel;
removing conductive material and the first tungsten layer from the second oxide layer; and
filling the channel with a second tungsten layer.