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] => 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 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 151 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [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 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 230 [patent_maintenance] => 1 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 183 [patent_maintenance] => 1 [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 [patent_figures_cnt] => 15 [patent_no_of_words] => 3273 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 1937 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 236 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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' [patent_app_type] => 1 [patent_app_number] => 8/748037 [patent_app_country] => US [patent_app_date] => 1996-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4177 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 187 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_date] => 1996-11-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 16 [patent_no_of_words] => 6142 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 239 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_country] => US [patent_app_date] => 1996-11-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3788 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_country] => US [patent_app_date] => 1996-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3332 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 1996-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 2665 [patent_no_of_claims] => 11 [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/05/755/05755404.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 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-04-21 [patent_title] => 'Low earth orbit payload launch system' [patent_app_type] => 1 [patent_app_number] => 8/716807 [patent_app_country] => US [patent_app_date] => 1996-09-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 2517 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-13 [patent_title] => 'Mechanical coupler/decoupler' [patent_app_type] => 1 [patent_app_number] => 8/711450 [patent_app_country] => US [patent_app_date] => 1996-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4888 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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' [patent_app_type] => 1 [patent_app_number] => 8/708698 [patent_app_country] => US [patent_app_date] => 1996-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 5081 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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
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