Search

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 numberTitle of the applicationFiling DateStatus
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
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