Search

Lissi Mojica Marquis

Examiner (ID: 12147)

Most Active Art Unit
3104
Art Unit(s)
3614, 3661, 3104, 3105, 3107, 3613
Total Applications
667
Issued Applications
565
Pending Applications
34
Abandoned Applications
68

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 2972154 [patent_doc_number] => 05265826 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-11-30 [patent_title] => 'Helicopter engine control having lateral cyclic pitch anticipation' [patent_app_type] => 1 [patent_app_number] => 7/935764 [patent_app_country] => US [patent_app_date] => 1992-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 6955 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/265/05265826.pdf [firstpage_image] =>[orig_patent_app_number] => 935764 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/935764
Helicopter engine control having lateral cyclic pitch anticipation Aug 25, 1992 Issued
Array ( [id] => 3413470 [patent_doc_number] => 05421540 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-06-06 [patent_title] => 'Method and apparatus for disposal/recovery of orbiting space debris' [patent_app_type] => 1 [patent_app_number] => 7/937057 [patent_app_country] => US [patent_app_date] => 1992-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 80 [patent_no_of_words] => 10903 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/421/05421540.pdf [firstpage_image] =>[orig_patent_app_number] => 937057 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/937057
Method and apparatus for disposal/recovery of orbiting space debris Aug 25, 1992 Issued
Array ( [id] => 2972134 [patent_doc_number] => 05265825 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-11-30 [patent_title] => 'Helicopter engine control having yaw input anticipation' [patent_app_type] => 1 [patent_app_number] => 7/936187 [patent_app_country] => US [patent_app_date] => 1992-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 7761 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/265/05265825.pdf [firstpage_image] =>[orig_patent_app_number] => 936187 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/936187
Helicopter engine control having yaw input anticipation Aug 25, 1992 Issued
Array ( [id] => 3073865 [patent_doc_number] => 05279481 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-01-18 [patent_title] => 'Airborne liquid-spreading system' [patent_app_type] => 1 [patent_app_number] => 7/935156 [patent_app_country] => US [patent_app_date] => 1992-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 4487 [patent_no_of_claims] => 37 [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/05/279/05279481.pdf [firstpage_image] =>[orig_patent_app_number] => 935156 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/935156
Airborne liquid-spreading system Aug 24, 1992 Issued
Array ( [id] => 2904458 [patent_doc_number] => 05205547 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-04-27 [patent_title] => 'Wave spring having uniformly positioned projections and predetermined spring' [patent_app_type] => 1 [patent_app_number] => 7/932273 [patent_app_country] => US [patent_app_date] => 1992-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 3099 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/205/05205547.pdf [firstpage_image] =>[orig_patent_app_number] => 932273 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/932273
Wave spring having uniformly positioned projections and predetermined spring Aug 18, 1992 Issued
Array ( [id] => 3098064 [patent_doc_number] => 05409066 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-04-25 [patent_title] => 'Adjustable sprinkler head positioning assembly' [patent_app_type] => 1 [patent_app_number] => 7/931920 [patent_app_country] => US [patent_app_date] => 1992-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 45 [patent_no_of_words] => 15468 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 416 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/409/05409066.pdf [firstpage_image] =>[orig_patent_app_number] => 931920 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/931920
Adjustable sprinkler head positioning assembly Aug 17, 1992 Issued
Array ( [id] => 3005020 [patent_doc_number] => 05301900 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-04-12 [patent_title] => 'Autogyro aircraft' [patent_app_type] => 1 [patent_app_number] => 7/931018 [patent_app_country] => US [patent_app_date] => 1992-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 32 [patent_figures_cnt] => 36 [patent_no_of_words] => 16660 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 305 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/301/05301900.pdf [firstpage_image] =>[orig_patent_app_number] => 931018 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/931018
Autogyro aircraft Aug 16, 1992 Issued
Array ( [id] => 3013783 [patent_doc_number] => 05316240 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-05-31 [patent_title] => 'Method and device for filtering the vibratory excitations transmitted between two parts especially between the rotor and the fuselage of a helicopter' [patent_app_type] => 1 [patent_app_number] => 7/928306 [patent_app_country] => US [patent_app_date] => 1992-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 4333 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/316/05316240.pdf [firstpage_image] =>[orig_patent_app_number] => 928306 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/928306
Method and device for filtering the vibratory excitations transmitted between two parts especially between the rotor and the fuselage of a helicopter Aug 11, 1992 Issued
Array ( [id] => 2880658 [patent_doc_number] => 05240207 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-08-31 [patent_title] => 'Generic drone control system' [patent_app_type] => 1 [patent_app_number] => 7/923867 [patent_app_country] => US [patent_app_date] => 1992-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3621 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 261 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/240/05240207.pdf [firstpage_image] =>[orig_patent_app_number] => 923867 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/923867
Generic drone control system Aug 2, 1992 Issued
Array ( [id] => 2998904 [patent_doc_number] => 05308025 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-05-03 [patent_title] => 'Spacecraft spin axis capture system and method' [patent_app_type] => 1 [patent_app_number] => 7/921676 [patent_app_country] => US [patent_app_date] => 1992-07-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2192 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/308/05308025.pdf [firstpage_image] =>[orig_patent_app_number] => 921676 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/921676
Spacecraft spin axis capture system and method Jul 29, 1992 Issued
Array ( [id] => 2984016 [patent_doc_number] => 05358224 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-10-25 [patent_title] => 'Isolator mount assembly' [patent_app_type] => 1 [patent_app_number] => 7/917283 [patent_app_country] => US [patent_app_date] => 1992-07-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 39 [patent_no_of_words] => 6594 [patent_no_of_claims] => 47 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/358/05358224.pdf [firstpage_image] =>[orig_patent_app_number] => 917283 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/917283
Isolator mount assembly Jul 22, 1992 Issued
Array ( [id] => 2921236 [patent_doc_number] => 05195811 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-03-23 [patent_title] => 'Circuit configuration for an electronically controlled anti-lock brake system' [patent_app_type] => 1 [patent_app_number] => 7/911245 [patent_app_country] => US [patent_app_date] => 1992-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2003 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 178 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/195/05195811.pdf [firstpage_image] =>[orig_patent_app_number] => 911245 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/911245
Circuit configuration for an electronically controlled anti-lock brake system Jul 5, 1992 Issued
Array ( [id] => 2896697 [patent_doc_number] => 05236153 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-08-17 [patent_title] => 'Longitudinal floating pivot track fitting' [patent_app_type] => 1 [patent_app_number] => 7/904236 [patent_app_country] => US [patent_app_date] => 1992-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 1588 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 216 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/236/05236153.pdf [firstpage_image] =>[orig_patent_app_number] => 904236 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/904236
Longitudinal floating pivot track fitting Jun 24, 1992 Issued
Array ( [id] => 2920165 [patent_doc_number] => 05228640 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-07-20 [patent_title] => 'Device for the elastic coupling between two parts, and aircraft with rotating wings comprising said device' [patent_app_type] => 1 [patent_app_number] => 7/897986 [patent_app_country] => US [patent_app_date] => 1992-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4726 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 316 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/228/05228640.pdf [firstpage_image] =>[orig_patent_app_number] => 897986 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/897986
Device for the elastic coupling between two parts, and aircraft with rotating wings comprising said device Jun 15, 1992 Issued
Array ( [id] => 2871611 [patent_doc_number] => 05213289 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-05-25 [patent_title] => 'Framed airfoil kite' [patent_app_type] => 1 [patent_app_number] => 7/894916 [patent_app_country] => US [patent_app_date] => 1992-06-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 22 [patent_no_of_words] => 6970 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/213/05213289.pdf [firstpage_image] =>[orig_patent_app_number] => 894916 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/894916
Framed airfoil kite Jun 7, 1992 Issued
Array ( [id] => 4034797 [patent_doc_number] => 05931417 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-08-03 [patent_title] => 'Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes above 25.degree. and its extension to global coverage tailored to the distribution of populated land masses on earth' [patent_app_type] => 1 [patent_app_number] => 7/892239 [patent_app_country] => US [patent_app_date] => 1992-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6487 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/931/05931417.pdf [firstpage_image] =>[orig_patent_app_number] => 892239 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/892239
Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes above 25.degree. and its extension to global coverage tailored to the distribution of populated land masses on earth Jun 1, 1992 Issued
Array ( [id] => 3020700 [patent_doc_number] => 05299759 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-04-05 [patent_title] => 'Helicopter turn coordination and heading hold mode control' [patent_app_type] => 1 [patent_app_number] => 7/891624 [patent_app_country] => US [patent_app_date] => 1992-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 4824 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 206 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/299/05299759.pdf [firstpage_image] =>[orig_patent_app_number] => 891624 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/891624
Helicopter turn coordination and heading hold mode control May 31, 1992 Issued
Array ( [id] => 3925397 [patent_doc_number] => 05871181 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-02-16 [patent_title] => 'Artificial satellite communication system' [patent_app_type] => 1 [patent_app_number] => 7/886228 [patent_app_country] => US [patent_app_date] => 1992-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 3261 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/871/05871181.pdf [firstpage_image] =>[orig_patent_app_number] => 886228 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/886228
Artificial satellite communication system May 20, 1992 Issued
07/885037 TORSIONAL TWIST AIRFOIL CONTROL MEANS May 14, 1992 Abandoned
Array ( [id] => 3014651 [patent_doc_number] => 05348256 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-09-20 [patent_title] => 'Supersonic aircraft and method' [patent_app_type] => 1 [patent_app_number] => 7/883590 [patent_app_country] => US [patent_app_date] => 1992-05-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 7573 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/348/05348256.pdf [firstpage_image] =>[orig_patent_app_number] => 883590 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/883590
Supersonic aircraft and method May 12, 1992 Issued
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