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] => 3755369 [patent_doc_number] => 05755406 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-26 [patent_title] => 'Modular, independent subsystem design satellite bus and variable communication payload configurations and missions' [patent_app_type] => 1 [patent_app_number] => 8/577441 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 18 [patent_no_of_words] => 3672 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/755/05755406.pdf [firstpage_image] =>[orig_patent_app_number] => 577441 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/577441
Modular, independent subsystem design satellite bus and variable communication payload configurations and missions Dec 21, 1995 Issued
Array ( [id] => 3771831 [patent_doc_number] => 05735485 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-04-07 [patent_title] => 'Variable slot airbrake for aircraft wing' [patent_app_type] => 1 [patent_app_number] => 8/577834 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4129 [patent_no_of_claims] => 13 [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/05/735/05735485.pdf [firstpage_image] =>[orig_patent_app_number] => 577834 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/577834
Variable slot airbrake for aircraft wing Dec 21, 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] => 3684123 [patent_doc_number] => 05676334 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-10-14 [patent_title] => 'Cyclic minimizer through alignment of the center of gravity and direction of flight vectors' [patent_app_type] => 1 [patent_app_number] => 8/576603 [patent_app_country] => US [patent_app_date] => 1995-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6941 [patent_no_of_claims] => 38 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 184 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/676/05676334.pdf [firstpage_image] =>[orig_patent_app_number] => 576603 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/576603
Cyclic minimizer through alignment of the center of gravity and direction of flight vectors Dec 20, 1995 Issued
Array ( [id] => 3811952 [patent_doc_number] => 05730394 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-24 [patent_title] => 'Vertical performance limit compensator' [patent_app_type] => 1 [patent_app_number] => 8/575452 [patent_app_country] => US [patent_app_date] => 1995-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4954 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/730/05730394.pdf [firstpage_image] =>[orig_patent_app_number] => 575452 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/575452
Vertical performance limit compensator Dec 19, 1995 Issued
Array ( [id] => 3755430 [patent_doc_number] => 05732907 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-31 [patent_title] => 'Ejection seat buckle' [patent_app_type] => 1 [patent_app_number] => 8/574381 [patent_app_country] => US [patent_app_date] => 1995-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1498 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/732/05732907.pdf [firstpage_image] =>[orig_patent_app_number] => 574381 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/574381
Ejection seat buckle Dec 17, 1995 Issued
Array ( [id] => 3775104 [patent_doc_number] => 05779169 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-14 [patent_title] => 'Aircraft engine inlet hot gas and foreign object ingestion reduction and pitch control system' [patent_app_type] => 1 [patent_app_number] => 8/573047 [patent_app_country] => US [patent_app_date] => 1995-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 7917 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 311 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/779/05779169.pdf [firstpage_image] =>[orig_patent_app_number] => 573047 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/573047
Aircraft engine inlet hot gas and foreign object ingestion reduction and pitch control system Dec 14, 1995 Issued
Array ( [id] => 3775495 [patent_doc_number] => 05779196 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-14 [patent_title] => 'Ram air drive laminar flow control system' [patent_app_type] => 1 [patent_app_number] => 8/569907 [patent_app_country] => US [patent_app_date] => 1995-12-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4331 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/779/05779196.pdf [firstpage_image] =>[orig_patent_app_number] => 569907 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/569907
Ram air drive laminar flow control system Dec 7, 1995 Issued
Array ( [id] => 4046971 [patent_doc_number] => 05865397 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-02-02 [patent_title] => 'Method and apparatus for creating detail surfaces on composite aircraft structures' [patent_app_type] => 1 [patent_app_number] => 8/567542 [patent_app_country] => US [patent_app_date] => 1995-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 4635 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/865/05865397.pdf [firstpage_image] =>[orig_patent_app_number] => 567542 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/567542
Method and apparatus for creating detail surfaces on composite aircraft structures Dec 4, 1995 Issued
Array ( [id] => 3874564 [patent_doc_number] => 05722621 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-03 [patent_title] => 'Bipod load support' [patent_app_type] => 1 [patent_app_number] => 8/567621 [patent_app_country] => US [patent_app_date] => 1995-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2417 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 366 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/722/05722621.pdf [firstpage_image] =>[orig_patent_app_number] => 567621 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/567621
Bipod load support Dec 4, 1995 Issued
Array ( [id] => 3861314 [patent_doc_number] => 05803410 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-08 [patent_title] => 'Skin friction reduction by micro-blowing technique' [patent_app_type] => 1 [patent_app_number] => 8/566211 [patent_app_country] => US [patent_app_date] => 1995-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 16 [patent_no_of_words] => 3446 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/803/05803410.pdf [firstpage_image] =>[orig_patent_app_number] => 566211 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/566211
Skin friction reduction by micro-blowing technique Nov 30, 1995 Issued
Array ( [id] => 3801722 [patent_doc_number] => 05709356 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-01-20 [patent_title] => 'Anti-spark structure, in particular for aircraft' [patent_app_type] => 1 [patent_app_number] => 8/549670 [patent_app_country] => US [patent_app_date] => 1995-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2814 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 242 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/709/05709356.pdf [firstpage_image] =>[orig_patent_app_number] => 549670 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/549670
Anti-spark structure, in particular for aircraft Nov 29, 1995 Issued
Array ( [id] => 3775439 [patent_doc_number] => 05779192 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-14 [patent_title] => 'Thrust reverser with improved forward thrust efficiency' [patent_app_type] => 1 [patent_app_number] => 8/566433 [patent_app_country] => US [patent_app_date] => 1995-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 2090 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 169 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/779/05779192.pdf [firstpage_image] =>[orig_patent_app_number] => 566433 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/566433
Thrust reverser with improved forward thrust efficiency Nov 29, 1995 Issued
Array ( [id] => 3874494 [patent_doc_number] => 05722616 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-03 [patent_title] => 'Conical rotary actuator and its application to the control of a rudder' [patent_app_type] => 1 [patent_app_number] => 8/562761 [patent_app_country] => US [patent_app_date] => 1995-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4698 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/722/05722616.pdf [firstpage_image] =>[orig_patent_app_number] => 562761 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/562761
Conical rotary actuator and its application to the control of a rudder Nov 26, 1995 Issued
Array ( [id] => 3775412 [patent_doc_number] => 05779190 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-14 [patent_title] => 'Portable unmanned aerial vehicle' [patent_app_type] => 1 [patent_app_number] => 8/561929 [patent_app_country] => US [patent_app_date] => 1995-11-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 3042 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/779/05779190.pdf [firstpage_image] =>[orig_patent_app_number] => 561929 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/561929
Portable unmanned aerial vehicle Nov 21, 1995 Issued
08/553124 SYSTEM FOR PROGRAMMING PROGRAMMABLE HEARING AIDS AND UPDATING DATABASE OF PATIENT INFORMATION Nov 6, 1995 Abandoned
Array ( [id] => 3847200 [patent_doc_number] => 05794892 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-08-18 [patent_title] => 'Critical nutation dampling on spinning bodies via momentum wheels or similar devices' [patent_app_type] => 1 [patent_app_number] => 8/548158 [patent_app_country] => US [patent_app_date] => 1995-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 12 [patent_no_of_words] => 3852 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/794/05794892.pdf [firstpage_image] =>[orig_patent_app_number] => 548158 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/548158
Critical nutation dampling on spinning bodies via momentum wheels or similar devices Oct 24, 1995 Issued
Array ( [id] => 3860545 [patent_doc_number] => 05746395 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-05 [patent_title] => 'Helicopter seat safety system' [patent_app_type] => 1 [patent_app_number] => 8/546073 [patent_app_country] => US [patent_app_date] => 1995-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 3970 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/746/05746395.pdf [firstpage_image] =>[orig_patent_app_number] => 546073 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/546073
Helicopter seat safety system Oct 19, 1995 Issued
Array ( [id] => 3608670 [patent_doc_number] => 05687933 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-11-18 [patent_title] => 'Attitude control for spacecraft with movable appendages such as solar panels' [patent_app_type] => 1 [patent_app_number] => 8/543733 [patent_app_country] => US [patent_app_date] => 1995-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2481 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 449 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/687/05687933.pdf [firstpage_image] =>[orig_patent_app_number] => 543733 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/543733
Attitude control for spacecraft with movable appendages such as solar panels Oct 15, 1995 Issued
Array ( [id] => 3843096 [patent_doc_number] => 05704567 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-01-06 [patent_title] => 'Blade de-icer for rotary wing aircraft' [patent_app_type] => 1 [patent_app_number] => 8/543688 [patent_app_country] => US [patent_app_date] => 1995-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 2351 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/704/05704567.pdf [firstpage_image] =>[orig_patent_app_number] => 543688 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/543688
Blade de-icer for rotary wing aircraft Oct 15, 1995 Issued
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