
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] => 3825373
[patent_doc_number] => 05743487
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-28
[patent_title] => 'Aircraft video monitor deployment and retraction apparatus'
[patent_app_type] => 1
[patent_app_number] => 8/631102
[patent_app_country] => US
[patent_app_date] => 1996-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 13
[patent_no_of_words] => 3696
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/743/05743487.pdf
[firstpage_image] =>[orig_patent_app_number] => 631102
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/631102 | Aircraft video monitor deployment and retraction apparatus | Apr 11, 1996 | Issued |
Array
(
[id] => 3759076
[patent_doc_number] => 05816535
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-06
[patent_title] => 'Emergency cargo extraction parachute jettison system'
[patent_app_type] => 1
[patent_app_number] => 8/631193
[patent_app_country] => US
[patent_app_date] => 1996-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 3392
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 204
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/816/05816535.pdf
[firstpage_image] =>[orig_patent_app_number] => 631193
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/631193 | Emergency cargo extraction parachute jettison system | Apr 9, 1996 | Issued |
Array
(
[id] => 3771904
[patent_doc_number] => 05735490
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-07
[patent_title] => 'Control device with a control stick, particularly a servo sidestick for aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/586893
[patent_app_country] => US
[patent_app_date] => 1996-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1900
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/735/05735490.pdf
[firstpage_image] =>[orig_patent_app_number] => 586893
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/586893 | Control device with a control stick, particularly a servo sidestick for aircraft | Apr 9, 1996 | Issued |
Array
(
[id] => 3791869
[patent_doc_number] => 05853149
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-29
[patent_title] => 'Stress-free dome mount missile design'
[patent_app_type] => 1
[patent_app_number] => 8/637193
[patent_app_country] => US
[patent_app_date] => 1996-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2210
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/853/05853149.pdf
[firstpage_image] =>[orig_patent_app_number] => 637193
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/637193 | Stress-free dome mount missile design | Apr 7, 1996 | Issued |
Array
(
[id] => 3714349
[patent_doc_number] => 05699981
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-23
[patent_title] => 'Aircraft cavity acoustic resonance suppression system'
[patent_app_type] => 1
[patent_app_number] => 8/617145
[patent_app_country] => US
[patent_app_date] => 1996-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1841
[patent_no_of_claims] => 5
[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/05/699/05699981.pdf
[firstpage_image] =>[orig_patent_app_number] => 617145
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/617145 | Aircraft cavity acoustic resonance suppression system | Mar 17, 1996 | Issued |
Array
(
[id] => 3950116
[patent_doc_number] => 05884869
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-03-23
[patent_title] => 'Satellite spin vector control with sun sensor'
[patent_app_type] => 1
[patent_app_number] => 8/617230
[patent_app_country] => US
[patent_app_date] => 1996-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 13
[patent_no_of_words] => 6998
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 197
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/884/05884869.pdf
[firstpage_image] =>[orig_patent_app_number] => 617230
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/617230 | Satellite spin vector control with sun sensor | Mar 17, 1996 | Issued |
| 08/617975 | METHOD AND APPARATUS FOR COMPUTER-AIDED DESIGN OF DIFFERENT-SIZED RF MODULAR HYBRID CIRCUITS | Mar 14, 1996 | Abandoned |
Array
(
[id] => 3828520
[patent_doc_number] => 05707029
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-01-13
[patent_title] => 'Aileron/elevators and body flap for roll, pitch, and yaw control'
[patent_app_type] => 1
[patent_app_number] => 8/611514
[patent_app_country] => US
[patent_app_date] => 1996-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 3480
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/707/05707029.pdf
[firstpage_image] =>[orig_patent_app_number] => 611514
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/611514 | Aileron/elevators and body flap for roll, pitch, and yaw control | Mar 6, 1996 | Issued |
Array
(
[id] => 3713325
[patent_doc_number] => 05671899
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-09-30
[patent_title] => 'Airborne vehicle with wing extension and roll control'
[patent_app_type] => 1
[patent_app_number] => 8/606928
[patent_app_country] => US
[patent_app_date] => 1996-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 3225
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 247
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/671/05671899.pdf
[firstpage_image] =>[orig_patent_app_number] => 606928
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/606928 | Airborne vehicle with wing extension and roll control | Feb 25, 1996 | Issued |
Array
(
[id] => 3778241
[patent_doc_number] => 05725182
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-10
[patent_title] => 'Turbo fan engine thrust reverser'
[patent_app_type] => 1
[patent_app_number] => 8/603448
[patent_app_country] => US
[patent_app_date] => 1996-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 1832
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 251
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/725/05725182.pdf
[firstpage_image] =>[orig_patent_app_number] => 603448
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/603448 | Turbo fan engine thrust reverser | Feb 19, 1996 | Issued |
Array
(
[id] => 3830920
[patent_doc_number] => 05765779
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-16
[patent_title] => 'Ice protection device'
[patent_app_type] => 1
[patent_app_number] => 8/602072
[patent_app_country] => US
[patent_app_date] => 1996-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2731
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/765/05765779.pdf
[firstpage_image] =>[orig_patent_app_number] => 602072
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/602072 | Ice protection device | Feb 14, 1996 | Issued |
Array
(
[id] => 3749353
[patent_doc_number] => 05740991
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-21
[patent_title] => 'Method and apparatus for optimizing the aerodynamic effect of an airfoil'
[patent_app_type] => 1
[patent_app_number] => 8/596653
[patent_app_country] => US
[patent_app_date] => 1996-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5236
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/740/05740991.pdf
[firstpage_image] =>[orig_patent_app_number] => 596653
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/596653 | Method and apparatus for optimizing the aerodynamic effect of an airfoil | Feb 4, 1996 | Issued |
Array
(
[id] => 3757208
[patent_doc_number] => 05806794
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-15
[patent_title] => 'Aircraft braking system with damped brake rod'
[patent_app_type] => 1
[patent_app_number] => 8/592816
[patent_app_country] => US
[patent_app_date] => 1996-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4787
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/806/05806794.pdf
[firstpage_image] =>[orig_patent_app_number] => 592816
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/592816 | Aircraft braking system with damped brake rod | Jan 25, 1996 | Issued |
Array
(
[id] => 3861232
[patent_doc_number] => 05803404
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-08
[patent_title] => 'Door actuation system having a variable damping device'
[patent_app_type] => 1
[patent_app_number] => 8/590121
[patent_app_country] => US
[patent_app_date] => 1996-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 10
[patent_no_of_words] => 3168
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/803/05803404.pdf
[firstpage_image] =>[orig_patent_app_number] => 590121
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/590121 | Door actuation system having a variable damping device | Jan 22, 1996 | Issued |
Array
(
[id] => 3842531
[patent_doc_number] => 05791598
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-11
[patent_title] => 'Dynamic bias for orbital yaw steering'
[patent_app_type] => 1
[patent_app_number] => 8/585954
[patent_app_country] => US
[patent_app_date] => 1996-01-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3848
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/791/05791598.pdf
[firstpage_image] =>[orig_patent_app_number] => 585954
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/585954 | Dynamic bias for orbital yaw steering | Jan 11, 1996 | Issued |
Array
(
[id] => 3874537
[patent_doc_number] => 05722619
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-03
[patent_title] => 'Parachute bridle and method of deploying a parachute'
[patent_app_type] => 1
[patent_app_number] => 8/582309
[patent_app_country] => US
[patent_app_date] => 1996-01-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3636
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/722/05722619.pdf
[firstpage_image] =>[orig_patent_app_number] => 582309
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/582309 | Parachute bridle and method of deploying a parachute | Jan 2, 1996 | Issued |
Array
(
[id] => 3778212
[patent_doc_number] => 05725180
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-10
[patent_title] => 'Aircraft engine pitot plenum intake'
[patent_app_type] => 1
[patent_app_number] => 8/581708
[patent_app_country] => US
[patent_app_date] => 1995-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2711
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/725/05725180.pdf
[firstpage_image] =>[orig_patent_app_number] => 581708
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/581708 | Aircraft engine pitot plenum intake | Dec 28, 1995 | Issued |
Array
(
[id] => 3749339
[patent_doc_number] => 05740989
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-21
[patent_title] => 'Lay down seat mechanism'
[patent_app_type] => 1
[patent_app_number] => 8/577120
[patent_app_country] => US
[patent_app_date] => 1995-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2032
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 122
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/740/05740989.pdf
[firstpage_image] =>[orig_patent_app_number] => 577120
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577120 | Lay down seat mechanism | Dec 25, 1995 | Issued |
Array
(
[id] => 3860586
[patent_doc_number] => 05746398
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-05
[patent_title] => 'Force-gradient cyclic stick system for a helicopter'
[patent_app_type] => 1
[patent_app_number] => 8/577130
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 5541
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 465
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/746/05746398.pdf
[firstpage_image] =>[orig_patent_app_number] => 577130
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577130 | Force-gradient cyclic stick system for a helicopter | Dec 21, 1995 | Issued |
Array
(
[id] => 3882982
[patent_doc_number] => 05893534
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-04-13
[patent_title] => 'Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads'
[patent_app_type] => 1
[patent_app_number] => 8/577319
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 9
[patent_no_of_words] => 1690
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/893/05893534.pdf
[firstpage_image] =>[orig_patent_app_number] => 577319
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577319 | Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads | Dec 21, 1995 | Issued |