
Wei Lee
Examiner (ID: 15342, Phone: (571)270-3760 , Office: P/3714 )
| Most Active Art Unit | 3714 |
| Art Unit(s) | 3718, 3714, 3715 |
| Total Applications | 506 |
| Issued Applications | 226 |
| Pending Applications | 52 |
| Abandoned Applications | 229 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 3851604
[patent_doc_number] => 05836549
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-17
[patent_title] => 'Airfoil leading edge with cavity'
[patent_app_type] => 1
[patent_app_number] => 8/781237
[patent_app_country] => US
[patent_app_date] => 1997-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 1659
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/836/05836549.pdf
[firstpage_image] =>[orig_patent_app_number] => 781237
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/781237 | Airfoil leading edge with cavity | Jan 9, 1997 | Issued |
Array
(
[id] => 3797253
[patent_doc_number] => 05788184
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-04
[patent_title] => 'Aircraft passenger safety enhanced fuselage insulation blanket'
[patent_app_type] => 1
[patent_app_number] => 8/778744
[patent_app_country] => US
[patent_app_date] => 1997-01-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 13
[patent_no_of_words] => 11074
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/788/05788184.pdf
[firstpage_image] =>[orig_patent_app_number] => 778744
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/778744 | Aircraft passenger safety enhanced fuselage insulation blanket | Jan 3, 1997 | Issued |
Array
(
[id] => 3965791
[patent_doc_number] => 05904317
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-18
[patent_title] => 'Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module'
[patent_app_type] => 1
[patent_app_number] => 8/770478
[patent_app_country] => US
[patent_app_date] => 1996-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 3223
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/904/05904317.pdf
[firstpage_image] =>[orig_patent_app_number] => 770478
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/770478 | Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module | Dec 19, 1996 | Issued |
Array
(
[id] => 3892547
[patent_doc_number] => 05897080
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-04-27
[patent_title] => 'Externally mountable spacecraft equipment module'
[patent_app_type] => 1
[patent_app_number] => 8/771086
[patent_app_country] => US
[patent_app_date] => 1996-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 3001
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/897/05897080.pdf
[firstpage_image] =>[orig_patent_app_number] => 771086
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/771086 | Externally mountable spacecraft equipment module | Dec 19, 1996 | Issued |
Array
(
[id] => 4034810
[patent_doc_number] => 05931418
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-03
[patent_title] => 'Functionally independent spacecraft module'
[patent_app_type] => 1
[patent_app_number] => 8/771084
[patent_app_country] => US
[patent_app_date] => 1996-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 23
[patent_no_of_words] => 4798
[patent_no_of_claims] => 10
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/931/05931418.pdf
[firstpage_image] =>[orig_patent_app_number] => 771084
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/771084 | Functionally independent spacecraft module | Dec 19, 1996 | Issued |
Array
(
[id] => 4070839
[patent_doc_number] => 06024328
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-15
[patent_title] => 'Satellite control method using single species of bipropellant'
[patent_app_type] => 1
[patent_app_number] => 8/768736
[patent_app_country] => US
[patent_app_date] => 1996-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 2789
[patent_no_of_claims] => 23
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/024/06024328.pdf
[firstpage_image] =>[orig_patent_app_number] => 768736
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/768736 | Satellite control method using single species of bipropellant | Dec 17, 1996 | Issued |
Array
(
[id] => 3965804
[patent_doc_number] => 05904318
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-18
[patent_title] => 'Passive reduction of aircraft fuselage noise'
[patent_app_type] => 1
[patent_app_number] => 8/770737
[patent_app_country] => US
[patent_app_date] => 1996-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 7
[patent_no_of_words] => 4822
[patent_no_of_claims] => 14
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[patent_words_short_claim] => 230
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/904/05904318.pdf
[firstpage_image] =>[orig_patent_app_number] => 770737
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/770737 | Passive reduction of aircraft fuselage noise | Dec 17, 1996 | Issued |
Array
(
[id] => 3826013
[patent_doc_number] => 05771185
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-23
[patent_title] => 'Signal processor capable of sharing common hardware in a plural processing system'
[patent_app_type] => 1
[patent_app_number] => 8/768085
[patent_app_country] => US
[patent_app_date] => 1996-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 12389
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/771/05771185.pdf
[firstpage_image] =>[orig_patent_app_number] => 768085
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/768085 | Signal processor capable of sharing common hardware in a plural processing system | Dec 15, 1996 | Issued |
Array
(
[id] => 3945890
[patent_doc_number] => 05899410
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-04
[patent_title] => 'Aerodynamic body having coplanar joined wings'
[patent_app_type] => 1
[patent_app_number] => 8/764201
[patent_app_country] => US
[patent_app_date] => 1996-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 20
[patent_no_of_words] => 6892
[patent_no_of_claims] => 7
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/899/05899410.pdf
[firstpage_image] =>[orig_patent_app_number] => 764201
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/764201 | Aerodynamic body having coplanar joined wings | Dec 12, 1996 | Issued |
Array
(
[id] => 3797309
[patent_doc_number] => 05788188
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-04
[patent_title] => 'Control of the attitude of a satellite in low orbit involving solar acquisition'
[patent_app_type] => 1
[patent_app_number] => 8/760249
[patent_app_country] => US
[patent_app_date] => 1996-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3441
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/788/05788188.pdf
[firstpage_image] =>[orig_patent_app_number] => 760249
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/760249 | Control of the attitude of a satellite in low orbit involving solar acquisition | Dec 4, 1996 | Issued |
Array
(
[id] => 3851618
[patent_doc_number] => 05836550
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-17
[patent_title] => 'Mechanism for streamwise fowler deployment of the wing trailing or leading edge'
[patent_app_type] => 1
[patent_app_number] => 8/757145
[patent_app_country] => US
[patent_app_date] => 1996-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/836/05836550.pdf
[firstpage_image] =>[orig_patent_app_number] => 757145
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/757145 | Mechanism for streamwise fowler deployment of the wing trailing or leading edge | Nov 26, 1996 | Issued |
Array
(
[id] => 3871623
[patent_doc_number] => 05833172
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-10
[patent_title] => 'Arrangement of outlet devices'
[patent_app_type] => 1
[patent_app_number] => 8/749736
[patent_app_country] => US
[patent_app_date] => 1996-11-15
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/833/05833172.pdf
[firstpage_image] =>[orig_patent_app_number] => 749736
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/749736 | Arrangement of outlet devices | Nov 14, 1996 | Issued |
Array
(
[id] => 3757368
[patent_doc_number] => 05806804
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-15
[patent_title] => 'Adaptive harmonic disturbance compensation system'
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[patent_app_number] => 8/748037
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/806/05806804.pdf
[firstpage_image] =>[orig_patent_app_number] => 748037
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/748037 | Adaptive harmonic disturbance compensation system | Nov 11, 1996 | Issued |
Array
(
[id] => 3783396
[patent_doc_number] => 05826824
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-27
[patent_title] => 'Emergency egress system for aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/745351
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/826/05826824.pdf
[firstpage_image] =>[orig_patent_app_number] => 745351
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/745351 | Emergency egress system for aircraft | Nov 7, 1996 | Issued |
Array
(
[id] => 4395365
[patent_doc_number] => 06264355
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-07-24
[patent_title] => 'Audio console with motorized joystick panning system'
[patent_app_type] => 1
[patent_app_number] => 8/745016
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[pdf_file] => patents/06/264/06264355.pdf
[firstpage_image] =>[orig_patent_app_number] => 745016
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/745016 | Audio console with motorized joystick panning system | Nov 6, 1996 | Issued |
Array
(
[id] => 3797337
[patent_doc_number] => 05788190
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-04
[patent_title] => 'Slotted cruise trailing edge flap'
[patent_app_type] => 1
[patent_app_number] => 8/735233
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[patent_app_date] => 1996-10-22
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/788/05788190.pdf
[firstpage_image] =>[orig_patent_app_number] => 735233
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/735233 | Slotted cruise trailing edge flap | Oct 21, 1996 | Issued |
Array
(
[id] => 3755341
[patent_doc_number] => 05755404
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-26
[patent_title] => 'Forced air aircraft de-icer system'
[patent_app_type] => 1
[patent_app_number] => 8/729634
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/755/05755404.pdf
[firstpage_image] =>[orig_patent_app_number] => 729634
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/729634 | Forced air aircraft de-icer system | Sep 29, 1996 | Issued |
Array
(
[id] => 3749282
[patent_doc_number] => 05740985
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[patent_kind] => NA
[patent_issue_date] => 1998-04-21
[patent_title] => 'Low earth orbit payload launch system'
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[pdf_file] => patents/05/740/05740985.pdf
[firstpage_image] =>[orig_patent_app_number] => 716807
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/716807 | Low earth orbit payload launch system | Sep 15, 1996 | Issued |
Array
(
[id] => 3766417
[patent_doc_number] => 05820071
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[patent_issue_date] => 1998-10-13
[patent_title] => 'Mechanical coupler/decoupler'
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[pdf_file] => patents/05/820/05820071.pdf
[firstpage_image] =>[orig_patent_app_number] => 711450
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/711450 | Mechanical coupler/decoupler | Sep 4, 1996 | Issued |
Array
(
[id] => 3842506
[patent_doc_number] => 05791596
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-11
[patent_title] => 'Process and device for the control of the rudder of an aircraft'
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[pdf_file] => patents/05/791/05791596.pdf
[firstpage_image] =>[orig_patent_app_number] => 708698
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/708698 | Process and device for the control of the rudder of an aircraft | Sep 4, 1996 | Issued |