Search

Hsien Ming Lee

Examiner (ID: 13650, Phone: (571)272-1863 , Office: P/2823 )

Most Active Art Unit
2823
Art Unit(s)
2823, 2814
Total Applications
2377
Issued Applications
2182
Pending Applications
27
Abandoned Applications
178

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 5599355 [patent_doc_number] => 20060289699 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-28 [patent_title] => 'CONTAINER APPARATUS FOR OBJECT TO BE DROPPED' [patent_app_type] => utility [patent_app_number] => 10/408272 [patent_app_country] => US [patent_app_date] => 2003-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4503 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0289/20060289699.pdf [firstpage_image] =>[orig_patent_app_number] => 10408272 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/408272
Container apparatus for object to be dropped Apr 6, 2003 Issued
Array ( [id] => 6803274 [patent_doc_number] => 20030230668 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-12-18 [patent_title] => 'Helicopter electric connecting unit, and helicopter equipped with such a connecting unit' [patent_app_type] => new [patent_app_number] => 10/407942 [patent_app_country] => US [patent_app_date] => 2003-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1314 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0230/20030230668.pdf [firstpage_image] =>[orig_patent_app_number] => 10407942 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/407942
Helicopter electric connecting unit, and helicopter equipped with such a connecting unit Apr 6, 2003 Issued
Array ( [id] => 7439956 [patent_doc_number] => 20040195462 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-10-07 [patent_title] => 'SURFACE PLASMA DISCHARGE FOR CONTROLLING LEADING EDGE CONTAMINATION AND CROSSFLOW INSTABILITIES FOR LAMINAR FLOW' [patent_app_type] => new [patent_app_number] => 10/406940 [patent_app_country] => US [patent_app_date] => 2003-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3294 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 12 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0195/20040195462.pdf [firstpage_image] =>[orig_patent_app_number] => 10406940 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/406940
Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow Apr 2, 2003 Issued
Array ( [id] => 1120308 [patent_doc_number] => 06793171 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-09-21 [patent_title] => 'Method and system for flying an aircraft' [patent_app_type] => B1 [patent_app_number] => 10/406047 [patent_app_country] => US [patent_app_date] => 2003-04-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2751 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/793/06793171.pdf [firstpage_image] =>[orig_patent_app_number] => 10406047 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/406047
Method and system for flying an aircraft Apr 1, 2003 Issued
Array ( [id] => 7455306 [patent_doc_number] => 20040118971 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-24 [patent_title] => 'TAIL BOOM SADDLE FOR MAINTAINING HELICOPTOR MAIN ROTOR BLADES IN A STOWED CONFIGURATION FOR HELICOPTER STOWAGE AND TRANSPORT' [patent_app_type] => new [patent_app_number] => 10/405780 [patent_app_country] => US [patent_app_date] => 2003-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5833 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 294 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0118/20040118971.pdf [firstpage_image] =>[orig_patent_app_number] => 10405780 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/405780
Tail boom saddle for maintaining helicoptor main rotor blades in a stowed configuration for helicopter stowage and transport Mar 31, 2003 Issued
Array ( [id] => 1149793 [patent_doc_number] => 06761332 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-07-13 [patent_title] => 'Multi-functional galley system' [patent_app_type] => B1 [patent_app_number] => 10/404856 [patent_app_country] => US [patent_app_date] => 2003-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4332 [patent_no_of_claims] => 52 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/761/06761332.pdf [firstpage_image] =>[orig_patent_app_number] => 10404856 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/404856
Multi-functional galley system Mar 31, 2003 Issued
Array ( [id] => 753985 [patent_doc_number] => 07014147 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-21 [patent_title] => 'Anti hijacking system' [patent_app_type] => utility [patent_app_number] => 10/397563 [patent_app_country] => US [patent_app_date] => 2003-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1369 [patent_no_of_claims] => 3 [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/07/014/07014147.pdf [firstpage_image] =>[orig_patent_app_number] => 10397563 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/397563
Anti hijacking system Mar 26, 2003 Issued
Array ( [id] => 7387603 [patent_doc_number] => 20040016845 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-01-29 [patent_title] => 'Integrated and/or modular high-speed aircraft' [patent_app_type] => new [patent_app_number] => 10/394550 [patent_app_country] => US [patent_app_date] => 2003-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 9698 [patent_no_of_claims] => 90 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0016/20040016845.pdf [firstpage_image] =>[orig_patent_app_number] => 10394550 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/394550
Integrated and/or modular high-speed aircraft Mar 20, 2003 Issued
Array ( [id] => 6770903 [patent_doc_number] => 20030216843 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-11-20 [patent_title] => 'AirSafety system' [patent_app_type] => new [patent_app_number] => 10/394081 [patent_app_country] => US [patent_app_date] => 2003-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1087 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 28 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0216/20030216843.pdf [firstpage_image] =>[orig_patent_app_number] => 10394081 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/394081
AirSafety system Mar 20, 2003 Abandoned
Array ( [id] => 721088 [patent_doc_number] => 07044422 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-05-16 [patent_title] => 'Gyrostabilized self propelled aircraft' [patent_app_type] => utility [patent_app_number] => 10/390222 [patent_app_country] => US [patent_app_date] => 2003-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 23 [patent_no_of_words] => 9489 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 228 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/044/07044422.pdf [firstpage_image] =>[orig_patent_app_number] => 10390222 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/390222
Gyrostabilized self propelled aircraft Mar 16, 2003 Issued
Array ( [id] => 1120319 [patent_doc_number] => 06793177 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-09-21 [patent_title] => 'Active drag and thrust modulation system and method' [patent_app_type] => B2 [patent_app_number] => 10/386992 [patent_app_country] => US [patent_app_date] => 2003-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 42 [patent_no_of_words] => 17482 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/793/06793177.pdf [firstpage_image] =>[orig_patent_app_number] => 10386992 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/386992
Active drag and thrust modulation system and method Mar 11, 2003 Issued
Array ( [id] => 653563 [patent_doc_number] => 07108225 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-09-19 [patent_title] => 'More aerodynamic wheel fairings for small airplanes' [patent_app_type] => utility [patent_app_number] => 10/385360 [patent_app_country] => US [patent_app_date] => 2003-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6764 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/108/07108225.pdf [firstpage_image] =>[orig_patent_app_number] => 10385360 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/385360
More aerodynamic wheel fairings for small airplanes Mar 10, 2003 Issued
Array ( [id] => 1061425 [patent_doc_number] => 06848652 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-01 [patent_title] => 'Aircraft heater' [patent_app_type] => utility [patent_app_number] => 10/376004 [patent_app_country] => US [patent_app_date] => 2003-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 3170 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/848/06848652.pdf [firstpage_image] =>[orig_patent_app_number] => 10376004 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/376004
Aircraft heater Feb 27, 2003 Issued
Array ( [id] => 6827470 [patent_doc_number] => 20030178528 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-09-25 [patent_title] => 'Rotary-wing aircraft rotor with constant velocity drive' [patent_app_type] => new [patent_app_number] => 10/378003 [patent_app_country] => US [patent_app_date] => 2003-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 10138 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 430 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0178/20030178528.pdf [firstpage_image] =>[orig_patent_app_number] => 10378003 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/378003
Rotary-wing aircraft rotor with constant velocity drive Feb 27, 2003 Issued
Array ( [id] => 7367742 [patent_doc_number] => 20040026564 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-02-12 [patent_title] => 'METHOD AND APPARATUS FOR FOLDING/UNFOLDING THE BLADES OF A ROTARY-WING AIRCRAFT ROTOR' [patent_app_type] => new [patent_app_number] => 10/375707 [patent_app_country] => US [patent_app_date] => 2003-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 13325 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0026/20040026564.pdf [firstpage_image] =>[orig_patent_app_number] => 10375707 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/375707
Method and apparatus for folding/unfolding the blades of a rotary-wing aircraft rotor Feb 26, 2003 Issued
Array ( [id] => 7304744 [patent_doc_number] => 20040140403 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-22 [patent_title] => 'Asymetric gravitational wave propulsion system' [patent_app_type] => new [patent_app_number] => 10/363287 [patent_app_country] => US [patent_app_date] => 2003-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1811 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0140/20040140403.pdf [firstpage_image] =>[orig_patent_app_number] => 10363287 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/363287
Asymetric gravitational wave propulsion system Feb 26, 2003 Abandoned
Array ( [id] => 1166874 [patent_doc_number] => 06745981 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-06-08 [patent_title] => 'Aircraft sensor pod assembly' [patent_app_type] => B1 [patent_app_number] => 10/373459 [patent_app_country] => US [patent_app_date] => 2003-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1608 [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/06/745/06745981.pdf [firstpage_image] =>[orig_patent_app_number] => 10373459 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/373459
Aircraft sensor pod assembly Feb 24, 2003 Issued
Array ( [id] => 7446669 [patent_doc_number] => 20040164203 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-08-26 [patent_title] => 'Vertical take-off and landing aircraft' [patent_app_type] => new [patent_app_number] => 10/371704 [patent_app_country] => US [patent_app_date] => 2003-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5678 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 48 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0164/20040164203.pdf [firstpage_image] =>[orig_patent_app_number] => 10371704 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/371704
Vertical take-off and landing aircraft Feb 20, 2003 Abandoned
Array ( [id] => 7432627 [patent_doc_number] => 20040065772 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-08 [patent_title] => 'High-lift, low-drag, stall-resistant airfoil' [patent_app_type] => new [patent_app_number] => 10/370740 [patent_app_country] => US [patent_app_date] => 2003-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 5728 [patent_no_of_claims] => 68 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0065/20040065772.pdf [firstpage_image] =>[orig_patent_app_number] => 10370740 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/370740
High-lift, low-drag, stall-resistant airfoil Feb 20, 2003 Issued
Array ( [id] => 7446683 [patent_doc_number] => 20040164205 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-08-26 [patent_title] => 'Deployable spacecraft mount for electric propulsion' [patent_app_type] => new [patent_app_number] => 10/371838 [patent_app_country] => US [patent_app_date] => 2003-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4302 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 59 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0164/20040164205.pdf [firstpage_image] =>[orig_patent_app_number] => 10371838 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/371838
Deployable spacecraft mount for electric propulsion Feb 20, 2003 Issued
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