US20020009122A1 - Thermocouple assembly - Google Patents
Thermocouple assembly Download PDFInfo
- Publication number
- US20020009122A1 US20020009122A1 US09/395,619 US39561999A US2002009122A1 US 20020009122 A1 US20020009122 A1 US 20020009122A1 US 39561999 A US39561999 A US 39561999A US 2002009122 A1 US2002009122 A1 US 2002009122A1
- Authority
- US
- United States
- Prior art keywords
- insulating jacket
- thermocouple
- wire
- internally sealed
- assembly
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000012530 fluid Substances 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 claims abstract description 9
- 239000000155 melt Substances 0.000 claims abstract description 4
- 238000010438 heat treatment Methods 0.000 claims abstract description 3
- 229920001296 polysiloxane Polymers 0.000 claims description 9
- 239000004593 Epoxy Substances 0.000 claims description 5
- 239000000314 lubricant Substances 0.000 claims description 3
- 239000003921 oil Substances 0.000 description 8
- 238000009434 installation Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000009413 insulation Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 229920006362 Teflon® Polymers 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
- G01K1/08—Protective devices, e.g. casings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S277/00—Seal for a joint or juncture
- Y10S277/931—Seal including temperature responsive feature
- Y10S277/933—Chemical reaction or physical change of state
Definitions
- thermocouple assemblies and particularly those that are used inside lubricated components such as turbine bearings.
- the invention relates to a unique insulating jacket and thermocouple lead arrangement which prevents leakage of lubricating medium through the thermocouple jacket.
- thermocouple During the installation and routing of a thermocouple in, for example, a gas turbine bearing housing, the insulating jacket of the thermocouple can be cut or skinned. Any opening in the insulation jacket during installation permits lubricant such as oil within the bearing housing to leak through the outer insulating jacket and along the internal wires or leads. The oil can flow all the way to a junction box where the thermocouple leads are connected to terminal boards. The oil leakage may even be sufficient to flood the board and cause malfunction of the thermocouple readings. While this problem can be fixed easily if the opening in the insulation jacket is located outside the bearing housing, repair proves problematic in the event the cut or tear is inside the bearing housing, requiring an expensive and time consuming tear-down of the bearing and attendant shut-down of the turbine.
- This invention solves the problem of internal leakage of fluid through the thermocouple insulating jacket by introducing a silicone (or other epoxy) “pseudo-wire” into the assembly process during manufacture of the thermocouple.
- the “pseudo-wire” (preferably silicone) extends through the insulated jacket along and among the thermocouple leads.
- the thermocouple is then locally heated to a temperature which melts the silicone wire inside the thermocouple jacket and fuses it to the inside wall of the jacket.
- These localized fused areas may be about 12 inches in length and spaced apart by intervals of about 24 inches. Each of these fused areas provides a blockage to potential oil leaks caused by a cut or tear in the outer insulating jacket of the thermocouple.
- thermocouple assembly comprising a thermocouple; a plurality of lead wires extending from the thermocouple; an insulating jacket extending along and enclosing the plurality of leads; and at least one internally sealed area within the insulating jacket to prevent fluid leakage along and within the insulating jacket.
- the invention in another aspect, relates to a machine component housing having a lubricant therein and a thermocouple assembly mounted in a wall of the housing, the thermocouple assembly comprising: a thermocouple; a plurality of lead wires extending from the thermocouple; an insulating jacket extending along and enclosing the plurality of leads; and at least one internally sealed area within the insulating jacket to prevent fluid leakage along and within the insulating jacket.
- the invention relates to a method of preventing leakage of a fluid along and through an insulating jacket of a thermocouple comprising the steps of: a) attaching a plurality of lead wires to a thermocouple; b) adding a heat sensitive pseudo-wire to extend along the plurality of lead wires; c) enclosing the lead wires and pseudo-wire inside an insulating jacket; d) locally heating axially spaced portions of the insulating jacket to a temperature which melts the pseudo-wire and fuses it with an interior surface of the jacket.
- FIG. 1 is a schematic diagram of a conventional thermocouple assembly
- FIG. 2 is a schematic diagram of a thermocouple assembly mounted in a wall or turbine bearing housing, with the thermocouple leads extending to a terminal board;
- FIG. 3 is an enlarged partial elevation of a thermocouple assembly in accordance with an exemplary embodiment of the invention.
- thermocouple assembly 10 includes a thermocouple 12 along with a plurality of leads 14 , 16 , 18 and 20 .
- the leads are enclosed within a flexible, extruded insulating jacket 22 which may be made of Teflon® or other suitable material.
- thermocouple leads which may be 60 feet or more
- FIG. 3 illustrates an exemplary embodiment of this invention where a silicone or other suitable epoxy pseudo-wire is added to the thermocouple assembly during manufacture.
- the thermocouple assembly 110 includes a thermocouple (not shown) and a plurality of leads 114 , 116 , 118 and 120 enclosed within an insulating jacket 122 .
- the silicone “pseudo-wire” 132 added during manufacture of the assembly runs along and between the thermocouple leads 114 , 116 , 118 and 120 , for substantially the entire length of the jacket.
- the jacket 122 is externally heated at spaced locations along its length to a temperature of about 200° F. to melt the wire 132 and fuse the melted material to the interior surface of the jacket 122 .
- a fused portion is shown at 134 in FIG. 3.
- an etching material can be added to the Teflon® jacket material as it is extruded to thereby enhance the bond between the melted “pseudo-wire” and the jacket.
- the fusing process results in adjacent areas ballooning slightly outwardly as shown at 136 and 138 .
- These localized fused areas 134 may be about 12 inches in length, and may be axially spaced by about 24 inches, but these dimensions may vary depending on the particular thermocouple application.
- Each fused area 134 provides an internally sealed area, blocking the potential flow of oil caused by skinning or tearing the outer insulating jacket during thermocouple installation.
- oil entering the jacket 122 from a tear 124 in the jacket 122 (flowing in the direction of arrow 128 ) will not be able to reach the terminal board 30 (FIG. 2) because of the multiple seals formed along the length of the jacket.
- thermocouple assembly design as described herein not only prohibits oil leaking between the outer insulation jacket and the internal wires from the bearing to the junction box, but also allows operators to easily strip the jacket and connect the wires to the terminal boards due to its unique “balloon” configuration, i.e., the diameters of the unsealed areas 136 , 138 are greater than the diameters of the sealed areas 134 .
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
Abstract
Description
- This invention relates to thermocouple assemblies and particularly those that are used inside lubricated components such as turbine bearings. Specifically, the invention relates to a unique insulating jacket and thermocouple lead arrangement which prevents leakage of lubricating medium through the thermocouple jacket.
- During the installation and routing of a thermocouple in, for example, a gas turbine bearing housing, the insulating jacket of the thermocouple can be cut or skinned. Any opening in the insulation jacket during installation permits lubricant such as oil within the bearing housing to leak through the outer insulating jacket and along the internal wires or leads. The oil can flow all the way to a junction box where the thermocouple leads are connected to terminal boards. The oil leakage may even be sufficient to flood the board and cause malfunction of the thermocouple readings. While this problem can be fixed easily if the opening in the insulation jacket is located outside the bearing housing, repair proves problematic in the event the cut or tear is inside the bearing housing, requiring an expensive and time consuming tear-down of the bearing and attendant shut-down of the turbine.
- This invention solves the problem of internal leakage of fluid through the thermocouple insulating jacket by introducing a silicone (or other epoxy) “pseudo-wire” into the assembly process during manufacture of the thermocouple. The “pseudo-wire” (preferably silicone) extends through the insulated jacket along and among the thermocouple leads. The thermocouple is then locally heated to a temperature which melts the silicone wire inside the thermocouple jacket and fuses it to the inside wall of the jacket. These localized fused areas may be about 12 inches in length and spaced apart by intervals of about 24 inches. Each of these fused areas provides a blockage to potential oil leaks caused by a cut or tear in the outer insulating jacket of the thermocouple.
- Accordingly, in its broader aspects, the present invention relates to a thermocouple assembly comprising a thermocouple; a plurality of lead wires extending from the thermocouple; an insulating jacket extending along and enclosing the plurality of leads; and at least one internally sealed area within the insulating jacket to prevent fluid leakage along and within the insulating jacket.
- In another aspect, the invention relates to a machine component housing having a lubricant therein and a thermocouple assembly mounted in a wall of the housing, the thermocouple assembly comprising: a thermocouple; a plurality of lead wires extending from the thermocouple; an insulating jacket extending along and enclosing the plurality of leads; and at least one internally sealed area within the insulating jacket to prevent fluid leakage along and within the insulating jacket.
- In still another aspect, the invention relates to a method of preventing leakage of a fluid along and through an insulating jacket of a thermocouple comprising the steps of: a) attaching a plurality of lead wires to a thermocouple; b) adding a heat sensitive pseudo-wire to extend along the plurality of lead wires; c) enclosing the lead wires and pseudo-wire inside an insulating jacket; d) locally heating axially spaced portions of the insulating jacket to a temperature which melts the pseudo-wire and fuses it with an interior surface of the jacket.
- FIG. 1 is a schematic diagram of a conventional thermocouple assembly;
- FIG. 2 is a schematic diagram of a thermocouple assembly mounted in a wall or turbine bearing housing, with the thermocouple leads extending to a terminal board; and
- FIG. 3 is an enlarged partial elevation of a thermocouple assembly in accordance with an exemplary embodiment of the invention.
- With reference to FIG. 1, a
conventional thermocouple assembly 10 includes athermocouple 12 along with a plurality of 14, 16, 18 and 20. The leads are enclosed within a flexible, extruded insulatingleads jacket 22 which may be made of Teflon® or other suitable material. - If a cut or
tear 24 is inadvertently made in the insulatingjacket 22 during installation of the thermocouple at a location within, for example, a lubricated bearing housing 26 (see FIG. 2), the lubricating oil within the bearing may enter the jacket and flow in the direction ofarrow 28. This oil may flow the entire length of the thermocouple leads (which may be 60 feet or more) and flood theterminal board 30, thus causing erroneous thermocouple readings, and requiring an expensive and time consuming shutdown. - FIG. 3 illustrates an exemplary embodiment of this invention where a silicone or other suitable epoxy pseudo-wire is added to the thermocouple assembly during manufacture. For convenience, reference numerals are used in FIG. 3 which correspond to those used in FIG. 1, but with the prefix “1” added. Thus, the
thermocouple assembly 110 includes a thermocouple (not shown) and a plurality of 114, 116, 118 and 120 enclosed within anleads insulating jacket 122. The silicone “pseudo-wire” 132 added during manufacture of the assembly runs along and between the thermocouple leads 114, 116, 118 and 120, for substantially the entire length of the jacket. After the introduction of thesilicone wire 132, thejacket 122 is externally heated at spaced locations along its length to a temperature of about 200° F. to melt thewire 132 and fuse the melted material to the interior surface of thejacket 122. One such fused portion is shown at 134 in FIG. 3. If necessary, an etching material can be added to the Teflon® jacket material as it is extruded to thereby enhance the bond between the melted “pseudo-wire” and the jacket. The fusing process results in adjacent areas ballooning slightly outwardly as shown at 136 and 138. These localized fusedareas 134 may be about 12 inches in length, and may be axially spaced by about 24 inches, but these dimensions may vary depending on the particular thermocouple application. Each fusedarea 134 provides an internally sealed area, blocking the potential flow of oil caused by skinning or tearing the outer insulating jacket during thermocouple installation. In other words, oil entering thejacket 122 from atear 124 in the jacket 122 (flowing in the direction of arrow 128) will not be able to reach the terminal board 30 (FIG. 2) because of the multiple seals formed along the length of the jacket. - It will be appreciated that the thermocouple assembly design as described herein not only prohibits oil leaking between the outer insulation jacket and the internal wires from the bearing to the junction box, but also allows operators to easily strip the jacket and connect the wires to the terminal boards due to its unique “balloon” configuration, i.e., the diameters of the
136, 138 are greater than the diameters of the sealedunsealed areas areas 134. - While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Claims (20)
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/395,619 US6352362B2 (en) | 1999-09-14 | 1999-09-14 | Method of preventing leakage of a fluid along and through an insulating jacket of a thermocouple |
| EP00306306A EP1085308A1 (en) | 1999-09-14 | 2000-07-24 | Thermocouple assembly |
| JP2000230114A JP2001091365A (en) | 1999-09-14 | 2000-07-31 | Thermocouple assembly |
| KR1020000044968A KR100671582B1 (en) | 1999-09-14 | 2000-08-03 | Thermocouple Assemblies and Fluid Suppression Methods |
| US09/832,124 US6354735B2 (en) | 1999-09-14 | 2001-04-11 | Thermocouple assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/395,619 US6352362B2 (en) | 1999-09-14 | 1999-09-14 | Method of preventing leakage of a fluid along and through an insulating jacket of a thermocouple |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/832,124 Division US6354735B2 (en) | 1999-09-14 | 2001-04-11 | Thermocouple assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20020009122A1 true US20020009122A1 (en) | 2002-01-24 |
| US6352362B2 US6352362B2 (en) | 2002-03-05 |
Family
ID=23563784
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/395,619 Expired - Fee Related US6352362B2 (en) | 1999-09-14 | 1999-09-14 | Method of preventing leakage of a fluid along and through an insulating jacket of a thermocouple |
| US09/832,124 Expired - Fee Related US6354735B2 (en) | 1999-09-14 | 2001-04-11 | Thermocouple assembly |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/832,124 Expired - Fee Related US6354735B2 (en) | 1999-09-14 | 2001-04-11 | Thermocouple assembly |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US6352362B2 (en) |
| EP (1) | EP1085308A1 (en) |
| JP (1) | JP2001091365A (en) |
| KR (1) | KR100671582B1 (en) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7361830B2 (en) * | 2002-03-21 | 2008-04-22 | Rtd Company | Polymer encapsulated micro-thermocouple |
| US6977575B2 (en) * | 2003-05-22 | 2005-12-20 | Rtd Company | Flexible averaging resistance temperature detector |
| US20060038988A1 (en) * | 2004-08-20 | 2006-02-23 | General Electric Company | Borescope assembly for detecting a condition of a rotating part |
| US7719400B1 (en) | 2005-08-02 | 2010-05-18 | Rtd Company | Method and apparatus for flexible temperature sensor having coiled element |
| US8251579B2 (en) * | 2007-07-16 | 2012-08-28 | Rtd Company | Robust stator winding temperature sensor |
| JP4747145B2 (en) * | 2007-09-21 | 2011-08-17 | 株式会社岡崎製作所 | Sheathed thermocouple |
| FR2926166B1 (en) * | 2008-01-08 | 2010-06-11 | Ge Energy Products France Snc | KIT OF TEMPERATURE SENSORS, IN PARTICULAR FOR COMBUSTION TURBINE. |
| KR100968890B1 (en) * | 2008-04-14 | 2010-07-09 | 주창영 | Waterproof remote controller |
| IT1393070B1 (en) * | 2008-10-24 | 2012-04-11 | Worgas Bruciatori Srl | SPECIAL THERMOCOUPLE FOR BURNERS |
| US20110026562A1 (en) * | 2009-07-31 | 2011-02-03 | Rtd Company | Temperature sensor using thin film resistance temperature detector |
| US8334749B1 (en) | 2009-09-28 | 2012-12-18 | General Electric Company | Temperature detection in a gas turbine |
| KR101754749B1 (en) | 2012-10-16 | 2017-07-10 | 메저먼트 스페셜티스, 인크. | Reinforced flexible temperature sensor |
| US9517369B2 (en) * | 2014-08-12 | 2016-12-13 | Stephen Samouhos | Fire stop conduit |
Family Cites Families (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1156383A (en) * | 1967-01-10 | 1969-06-25 | Bristol Aerojet Ltd | Improvements in and relating to Thermocouples |
| JPS5360680A (en) * | 1976-11-12 | 1978-05-31 | Yamatake Honeywell Co Ltd | Temperature detector for hot water supply apparatus |
| FR2385938A1 (en) | 1977-03-30 | 1978-10-27 | Fives Cail Babcock | LUBRICATION DEVICE FOR SKATE BEARINGS SUPPORTING A LARGE-DRIVEN ROTATING PART, SUCH AS A ROTARY GRINDER |
| JPS5612523A (en) * | 1979-07-13 | 1981-02-06 | Toho Denshi Kk | Manufacturing of thermosensor |
| JPS6145463Y2 (en) * | 1981-04-21 | 1986-12-20 | ||
| JPS5855727A (en) * | 1981-09-29 | 1983-04-02 | Toshiba Corp | Thermocouple device |
| JPS59185638U (en) * | 1983-05-28 | 1984-12-10 | 山里産業株式会社 | Multi-point temperature sensor |
| EP0153174A3 (en) * | 1984-02-17 | 1985-09-25 | RAYCHEM CORPORATION (a Delaware corporation) | Insulating multiple conductor cables |
| US4647716A (en) | 1984-11-06 | 1987-03-03 | Sigmaform Corporation | Article having heat expandable sealing member |
| JPS6372534U (en) * | 1986-10-29 | 1988-05-14 | ||
| JPH0748056B2 (en) * | 1989-04-26 | 1995-05-24 | 株式会社岡崎製作所 | Thermocouple manufacturing method |
| JPH0343691U (en) * | 1989-09-08 | 1991-04-24 | ||
| DE4002094A1 (en) | 1990-01-25 | 1991-08-01 | Kabelmetal Electro Gmbh | Waterproof multi-core insulated cable - has elastomer-insulated conductors and centre polymer thread core enveloped in flexible crosslinked sealing polymer |
| US5194692A (en) * | 1990-09-27 | 1993-03-16 | Amphenol Corporation | Uncased data bus coupler |
| US5145322A (en) * | 1991-07-03 | 1992-09-08 | Roy F. Senior, Jr. | Pump bearing overheating detection device and method |
| JP2643678B2 (en) * | 1991-08-30 | 1997-08-20 | 住友電装株式会社 | Grommet |
| US5348395A (en) * | 1992-12-11 | 1994-09-20 | General Electric Company | Aspirating pyrometer with platinum thermocouple and radiation shields |
| JPH06241913A (en) * | 1993-02-16 | 1994-09-02 | Chubu Sukegawa Kogyo Kk | Thermocouple temperature sensor |
| JPH08145809A (en) * | 1994-11-18 | 1996-06-07 | Kurabe Ind Co Ltd | Composite temperature detector |
| JPH109966A (en) * | 1996-06-26 | 1998-01-16 | Ishikawajima Harima Heavy Ind Co Ltd | Thermometer for piping |
| JP3550915B2 (en) * | 1996-10-25 | 2004-08-04 | いすゞ自動車株式会社 | Ceramic thermocouple for high temperature measurement |
| EP0818671A3 (en) * | 1996-07-12 | 1998-07-08 | Isuzu Ceramics Research Institute Co., Ltd. | A ceramic sheath type thermocouple |
| US6234488B1 (en) * | 1997-03-05 | 2001-05-22 | Trw Inc. | Heat shrinkable boot seal and method of installation |
| KR100228046B1 (en) * | 1997-03-19 | 1999-11-01 | 정명세 | High temperature platinum resistance thermometer |
| JPH1123374A (en) * | 1997-06-27 | 1999-01-29 | Tokyo Electron Ltd | Thermometer for heat treatment furnace |
| DE19754158A1 (en) | 1997-10-28 | 1999-05-12 | Marcel Hofsaes | Method for isolating an electrical component |
| DE19821773C1 (en) * | 1998-05-14 | 1999-10-07 | Reinhausen Maschf Scheubeck | Temperature measuring instrument esp. for oil in transformer and stepping switches |
-
1999
- 1999-09-14 US US09/395,619 patent/US6352362B2/en not_active Expired - Fee Related
-
2000
- 2000-07-24 EP EP00306306A patent/EP1085308A1/en not_active Withdrawn
- 2000-07-31 JP JP2000230114A patent/JP2001091365A/en active Pending
- 2000-08-03 KR KR1020000044968A patent/KR100671582B1/en not_active Expired - Fee Related
-
2001
- 2001-04-11 US US09/832,124 patent/US6354735B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US6352362B2 (en) | 2002-03-05 |
| KR20010087111A (en) | 2001-09-15 |
| US6354735B2 (en) | 2002-03-12 |
| JP2001091365A (en) | 2001-04-06 |
| US20010012314A1 (en) | 2001-08-09 |
| EP1085308A1 (en) | 2001-03-21 |
| KR100671582B1 (en) | 2007-01-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: GENERAL ELECTRIC COMPANY, NEW YORK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:THERMOS, ANTHONY CONSTANTINE;RAHAL, FADI ELIAS;REEL/FRAME:010362/0764 Effective date: 19991021 |
|
| AS | Assignment |
Owner name: ENERGY, UNITED STATES DEPARTMENT OF, DISTRICT OF C Free format text: CONFIRMATORY LICENSE;ASSIGNOR:GENERAL ELECTRIC COMPANY - GE POWER SYSTEMS;REEL/FRAME:011015/0853 Effective date: 19991028 |
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| FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
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| REMI | Maintenance fee reminder mailed | ||
| FPAY | Fee payment |
Year of fee payment: 4 |
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| SULP | Surcharge for late payment | ||
| REMI | Maintenance fee reminder mailed | ||
| LAPS | Lapse for failure to pay maintenance fees | ||
| STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
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| FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20100305 |