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] => 4030349 [patent_doc_number] => 05873544 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-02-23 [patent_title] => 'Slidable duct assembly for aircraft anti-icing conduit systems' [patent_app_type] => 1 [patent_app_number] => 8/664704 [patent_app_country] => US [patent_app_date] => 1996-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 2797 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/873/05873544.pdf [firstpage_image] =>[orig_patent_app_number] => 664704 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/664704
Slidable duct assembly for aircraft anti-icing conduit systems Jun 16, 1996 Issued
Array ( [id] => 4047012 [patent_doc_number] => 05865400 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-02-02 [patent_title] => 'Multipiece, slidable duct assembly for aircraft anit-icing conduit systems' [patent_app_type] => 1 [patent_app_number] => 8/668433 [patent_app_country] => US [patent_app_date] => 1996-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2456 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/865/05865400.pdf [firstpage_image] =>[orig_patent_app_number] => 668433 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/668433
Multipiece, slidable duct assembly for aircraft anit-icing conduit systems Jun 16, 1996 Issued
Array ( [id] => 3987352 [patent_doc_number] => 06003814 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-12-21 [patent_title] => 'Double-walled duct assembly for aircraft anti-icing conduit systems' [patent_app_type] => 1 [patent_app_number] => 8/668434 [patent_app_country] => US [patent_app_date] => 1996-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2545 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 41 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/003/06003814.pdf [firstpage_image] =>[orig_patent_app_number] => 668434 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/668434
Double-walled duct assembly for aircraft anti-icing conduit systems Jun 16, 1996 Issued
Array ( [id] => 3772459 [patent_doc_number] => 05839700 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-11-24 [patent_title] => 'Articulated fin' [patent_app_type] => 1 [patent_app_number] => 8/668605 [patent_app_country] => US [patent_app_date] => 1996-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2493 [patent_no_of_claims] => 11 [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/05/839/05839700.pdf [firstpage_image] =>[orig_patent_app_number] => 668605 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/668605
Articulated fin Jun 2, 1996 Issued
Array ( [id] => 3746874 [patent_doc_number] => 05720452 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-02-24 [patent_title] => 'Solar panel parallel mounting configuration' [patent_app_type] => 1 [patent_app_number] => 8/655110 [patent_app_country] => US [patent_app_date] => 1996-05-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 5506 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 331 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/720/05720452.pdf [firstpage_image] =>[orig_patent_app_number] => 655110 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/655110
Solar panel parallel mounting configuration May 28, 1996 Issued
Array ( [id] => 3810601 [patent_doc_number] => 05758844 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-06-02 [patent_title] => 'Vertical/short take-off and landing (V/STOL) air vehicle capable of providing high speed horizontal flight' [patent_app_type] => 1 [patent_app_number] => 8/654133 [patent_app_country] => US [patent_app_date] => 1996-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 1641 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/758/05758844.pdf [firstpage_image] =>[orig_patent_app_number] => 654133 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/654133
Vertical/short take-off and landing (V/STOL) air vehicle capable of providing high speed horizontal flight May 27, 1996 Issued
Array ( [id] => 3771878 [patent_doc_number] => 05735488 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-04-07 [patent_title] => 'Method and apparatus for coupling space vehicles' [patent_app_type] => 1 [patent_app_number] => 8/654460 [patent_app_country] => US [patent_app_date] => 1996-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 3661 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 176 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/735/05735488.pdf [firstpage_image] =>[orig_patent_app_number] => 654460 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/654460
Method and apparatus for coupling space vehicles May 27, 1996 Issued
Array ( [id] => 3792720 [patent_doc_number] => 05810287 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-22 [patent_title] => 'Aircraft support pylon' [patent_app_type] => 1 [patent_app_number] => 8/652965 [patent_app_country] => US [patent_app_date] => 1996-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3535 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/810/05810287.pdf [firstpage_image] =>[orig_patent_app_number] => 652965 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/652965
Aircraft support pylon May 23, 1996 Issued
Array ( [id] => 3755297 [patent_doc_number] => 05755403 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-26 [patent_title] => 'Aircraft motor pod including a pivotable pod cowling' [patent_app_type] => 1 [patent_app_number] => 8/652002 [patent_app_country] => US [patent_app_date] => 1996-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 3967 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 199 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/755/05755403.pdf [firstpage_image] =>[orig_patent_app_number] => 652002 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/652002
Aircraft motor pod including a pivotable pod cowling May 22, 1996 Issued
Array ( [id] => 4031268 [patent_doc_number] => 05868351 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-02-09 [patent_title] => 'Rotor blade stowing system' [patent_app_type] => 1 [patent_app_number] => 8/653731 [patent_app_country] => US [patent_app_date] => 1996-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 35 [patent_no_of_words] => 8541 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 269 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/868/05868351.pdf [firstpage_image] =>[orig_patent_app_number] => 653731 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/653731
Rotor blade stowing system May 22, 1996 Issued
Array ( [id] => 3857058 [patent_doc_number] => 05823479 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-20 [patent_title] => 'Landing attitude modifier for airplane' [patent_app_type] => 1 [patent_app_number] => 8/650413 [patent_app_country] => US [patent_app_date] => 1996-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 12 [patent_no_of_words] => 6906 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/823/05823479.pdf [firstpage_image] =>[orig_patent_app_number] => 650413 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/650413
Landing attitude modifier for airplane May 19, 1996 Issued
Array ( [id] => 3717508 [patent_doc_number] => 05692703 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-12-02 [patent_title] => 'Multiple application wheel well design' [patent_app_type] => 1 [patent_app_number] => 8/644353 [patent_app_country] => US [patent_app_date] => 1996-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2058 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 265 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/692/05692703.pdf [firstpage_image] =>[orig_patent_app_number] => 644353 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/644353
Multiple application wheel well design May 9, 1996 Issued
Array ( [id] => 3721335 [patent_doc_number] => 05697579 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-12-16 [patent_title] => 'Aircraft having inflatable tubular support structure' [patent_app_type] => 1 [patent_app_number] => 8/642984 [patent_app_country] => US [patent_app_date] => 1996-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 27 [patent_no_of_words] => 2024 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/697/05697579.pdf [firstpage_image] =>[orig_patent_app_number] => 642984 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/642984
Aircraft having inflatable tubular support structure May 5, 1996 Issued
Array ( [id] => 3775481 [patent_doc_number] => 05779195 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-14 [patent_title] => 'Satellite assembly having modular common bus components' [patent_app_type] => 1 [patent_app_number] => 8/642713 [patent_app_country] => US [patent_app_date] => 1996-05-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 13 [patent_no_of_words] => 3262 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 33 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/779/05779195.pdf [firstpage_image] =>[orig_patent_app_number] => 642713 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/642713
Satellite assembly having modular common bus components May 2, 1996 Issued
Array ( [id] => 3778226 [patent_doc_number] => 05725181 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-10 [patent_title] => 'Aircraft engine thrust mount' [patent_app_type] => 1 [patent_app_number] => 8/640698 [patent_app_country] => US [patent_app_date] => 1996-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4215 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 227 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/725/05725181.pdf [firstpage_image] =>[orig_patent_app_number] => 640698 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/640698
Aircraft engine thrust mount Apr 30, 1996 Issued
Array ( [id] => 3798677 [patent_doc_number] => 05769362 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-06-23 [patent_title] => 'Aircraft control mechanism for a speed brake' [patent_app_type] => 1 [patent_app_number] => 8/639521 [patent_app_country] => US [patent_app_date] => 1996-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2986 [patent_no_of_claims] => 9 [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/05/769/05769362.pdf [firstpage_image] =>[orig_patent_app_number] => 639521 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/639521
Aircraft control mechanism for a speed brake Apr 30, 1996 Issued
Array ( [id] => 3732510 [patent_doc_number] => 05716032 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-02-10 [patent_title] => 'Unmanned aerial vehicle automatic landing system' [patent_app_type] => 1 [patent_app_number] => 8/641133 [patent_app_country] => US [patent_app_date] => 1996-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 4457 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 306 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/716/05716032.pdf [firstpage_image] =>[orig_patent_app_number] => 641133 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/641133
Unmanned aerial vehicle automatic landing system Apr 21, 1996 Issued
Array ( [id] => 3861261 [patent_doc_number] => 05803406 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-08 [patent_title] => 'Integrated thermal insulation system for spacecraft' [patent_app_type] => 1 [patent_app_number] => 8/656144 [patent_app_country] => US [patent_app_date] => 1996-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 3728 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/803/05803406.pdf [firstpage_image] =>[orig_patent_app_number] => 656144 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/656144
Integrated thermal insulation system for spacecraft Apr 21, 1996 Issued
08/634931 MULTI-AXIS UNFOLDING MECHANISM WITH RATE CONTROLLED SYNCHRONIZED MOVEMENT Apr 18, 1996 Abandoned
Array ( [id] => 3783358 [patent_doc_number] => 05826822 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-27 [patent_title] => 'System and method for providing cyclic and collective pitch control in a rotary wing aircraft' [patent_app_type] => 1 [patent_app_number] => 8/634970 [patent_app_country] => US [patent_app_date] => 1996-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 13 [patent_no_of_words] => 4115 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/826/05826822.pdf [firstpage_image] =>[orig_patent_app_number] => 634970 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/634970
System and method for providing cyclic and collective pitch control in a rotary wing aircraft Apr 18, 1996 Issued
Menu