Search

Syed Y. Hasan

Examiner (ID: 10276)

Most Active Art Unit
2484
Art Unit(s)
2621, 2484
Total Applications
654
Issued Applications
405
Pending Applications
4
Abandoned Applications
247

Applications

Application numberTitle of the applicationFiling DateStatus
08/020216 METHOD OF, AND APPARATUS FOR, DE-ICING AN AIR-CRAFT BY INFRARED RADIATION Feb 18, 1993 Abandoned
Array ( [id] => 3065019 [patent_doc_number] => 05322247 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-06-21 [patent_title] => 'Quad-line kite' [patent_app_type] => 1 [patent_app_number] => 8/018195 [patent_app_country] => US [patent_app_date] => 1993-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3825 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/322/05322247.pdf [firstpage_image] =>[orig_patent_app_number] => 018195 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/018195
Quad-line kite Feb 15, 1993 Issued
Array ( [id] => 3006553 [patent_doc_number] => 05326050 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-07-05 [patent_title] => 'Aerodynamic surface distension system for high angle of attack forebody vortex control' [patent_app_type] => 1 [patent_app_number] => 8/014584 [patent_app_country] => US [patent_app_date] => 1993-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 15 [patent_no_of_words] => 2923 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/326/05326050.pdf [firstpage_image] =>[orig_patent_app_number] => 014584 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/014584
Aerodynamic surface distension system for high angle of attack forebody vortex control Feb 7, 1993 Issued
Array ( [id] => 3445811 [patent_doc_number] => 05400986 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-03-28 [patent_title] => 'Optical solar reflector and mounting method' [patent_app_type] => 1 [patent_app_number] => 8/014645 [patent_app_country] => US [patent_app_date] => 1993-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 16 [patent_no_of_words] => 3772 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 257 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/400/05400986.pdf [firstpage_image] =>[orig_patent_app_number] => 014645 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/014645
Optical solar reflector and mounting method Feb 7, 1993 Issued
Array ( [id] => 3405304 [patent_doc_number] => 05393017 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-02-28 [patent_title] => 'Technique for dispensing earth satellites into multi-planar orbits' [patent_app_type] => 1 [patent_app_number] => 8/008036 [patent_app_country] => US [patent_app_date] => 1993-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 2000 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/393/05393017.pdf [firstpage_image] =>[orig_patent_app_number] => 008036 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/008036
Technique for dispensing earth satellites into multi-planar orbits Jan 24, 1993 Issued
Array ( [id] => 3098693 [patent_doc_number] => 05395073 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-03-07 [patent_title] => 'STOL/VTOL free wing aircraft with articulated tail boom' [patent_app_type] => 1 [patent_app_number] => 8/007130 [patent_app_country] => US [patent_app_date] => 1993-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 18 [patent_no_of_words] => 6341 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/395/05395073.pdf [firstpage_image] =>[orig_patent_app_number] => 007130 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/007130
STOL/VTOL free wing aircraft with articulated tail boom Jan 21, 1993 Issued
Array ( [id] => 3051075 [patent_doc_number] => 05351915 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-10-04 [patent_title] => 'Helicopter deck' [patent_app_type] => 1 [patent_app_number] => 8/005245 [patent_app_country] => US [patent_app_date] => 1993-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1872 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/351/05351915.pdf [firstpage_image] =>[orig_patent_app_number] => 005245 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/005245
Helicopter deck Jan 14, 1993 Issued
Array ( [id] => 3096772 [patent_doc_number] => 05413293 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-05-09 [patent_title] => 'Magnetic torque attitude control systems' [patent_app_type] => 1 [patent_app_number] => 7/995114 [patent_app_country] => US [patent_app_date] => 1992-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4079 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/413/05413293.pdf [firstpage_image] =>[orig_patent_app_number] => 995114 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/995114
Magnetic torque attitude control systems Dec 21, 1992 Issued
Array ( [id] => 3077666 [patent_doc_number] => 05289995 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-03-01 [patent_title] => 'Supersonic aircraft' [patent_app_type] => 1 [patent_app_number] => 7/990034 [patent_app_country] => US [patent_app_date] => 1992-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 6 [patent_no_of_words] => 1450 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/289/05289995.pdf [firstpage_image] =>[orig_patent_app_number] => 990034 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/990034
Supersonic aircraft Dec 13, 1992 Issued
Array ( [id] => 3038315 [patent_doc_number] => 05282587 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-02-01 [patent_title] => 'Aircraft wing cover and method of attachment' [patent_app_type] => 1 [patent_app_number] => 7/984995 [patent_app_country] => US [patent_app_date] => 1992-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 25 [patent_no_of_words] => 3091 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 257 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/282/05282587.pdf [firstpage_image] =>[orig_patent_app_number] => 984995 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/984995
Aircraft wing cover and method of attachment Dec 1, 1992 Issued
Array ( [id] => 3450742 [patent_doc_number] => 05390879 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-02-21 [patent_title] => 'Jet pipe for supporting a thrust reverser for aircraft jet engines' [patent_app_type] => 1 [patent_app_number] => 7/980170 [patent_app_country] => US [patent_app_date] => 1992-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2189 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/390/05390879.pdf [firstpage_image] =>[orig_patent_app_number] => 980170 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/980170
Jet pipe for supporting a thrust reverser for aircraft jet engines Nov 22, 1992 Issued
Array ( [id] => 2963704 [patent_doc_number] => 05251851 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-10-12 [patent_title] => 'Door operating mechanism for opening and closing an aircraft door in response to a stored program' [patent_app_type] => 1 [patent_app_number] => 7/975785 [patent_app_country] => US [patent_app_date] => 1992-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 6022 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 291 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/251/05251851.pdf [firstpage_image] =>[orig_patent_app_number] => 975785 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/975785
Door operating mechanism for opening and closing an aircraft door in response to a stored program Nov 12, 1992 Issued
Array ( [id] => 2981618 [patent_doc_number] => 05362016 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-11-08 [patent_title] => 'Parachute deployment system as a function of ejected pilot seat speed' [patent_app_type] => 1 [patent_app_number] => 7/973714 [patent_app_country] => US [patent_app_date] => 1992-11-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1100 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/362/05362016.pdf [firstpage_image] =>[orig_patent_app_number] => 973714 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/973714
Parachute deployment system as a function of ejected pilot seat speed Nov 8, 1992 Issued
Array ( [id] => 3051040 [patent_doc_number] => 05310142 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-05-10 [patent_title] => 'Dimple pattern pneumatic deicer assembly' [patent_app_type] => 1 [patent_app_number] => 7/968774 [patent_app_country] => US [patent_app_date] => 1992-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 11 [patent_no_of_words] => 3621 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/310/05310142.pdf [firstpage_image] =>[orig_patent_app_number] => 968774 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/968774
Dimple pattern pneumatic deicer assembly Oct 29, 1992 Issued
Array ( [id] => 2963624 [patent_doc_number] => 05251847 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-10-12 [patent_title] => 'Tail rotor anti-torque system for a helicopter' [patent_app_type] => 1 [patent_app_number] => 7/969714 [patent_app_country] => US [patent_app_date] => 1992-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 1938 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/251/05251847.pdf [firstpage_image] =>[orig_patent_app_number] => 969714 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/969714
Tail rotor anti-torque system for a helicopter Oct 27, 1992 Issued
Array ( [id] => 3033736 [patent_doc_number] => 05303880 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-04-19 [patent_title] => 'Aircraft engine pin mount' [patent_app_type] => 1 [patent_app_number] => 7/967355 [patent_app_country] => US [patent_app_date] => 1992-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 6334 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/303/05303880.pdf [firstpage_image] =>[orig_patent_app_number] => 967355 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/967355
Aircraft engine pin mount Oct 27, 1992 Issued
07/966390 MULTIPLE ELECTROMAGNETIC TILES FOR BOUNDARY LAYER CONTROL Oct 25, 1992 Abandoned
Array ( [id] => 3072377 [patent_doc_number] => 05277382 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-01-11 [patent_title] => 'Aircraft engine forward mount' [patent_app_type] => 1 [patent_app_number] => 7/959885 [patent_app_country] => US [patent_app_date] => 1992-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3133 [patent_no_of_claims] => 8 [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/05/277/05277382.pdf [firstpage_image] =>[orig_patent_app_number] => 959885 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/959885
Aircraft engine forward mount Oct 12, 1992 Issued
Array ( [id] => 3029998 [patent_doc_number] => 05333816 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-08-02 [patent_title] => 'Aircraft landing gear swivel locking pin having automatic release and reengage' [patent_app_type] => 1 [patent_app_number] => 7/954135 [patent_app_country] => US [patent_app_date] => 1992-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 4416 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 28 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/333/05333816.pdf [firstpage_image] =>[orig_patent_app_number] => 954135 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/954135
Aircraft landing gear swivel locking pin having automatic release and reengage Sep 29, 1992 Issued
Array ( [id] => 2998251 [patent_doc_number] => 05280957 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-01-25 [patent_title] => 'Subframe for a motor vehicle' [patent_app_type] => 1 [patent_app_number] => 7/941812 [patent_app_country] => US [patent_app_date] => 1992-09-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 14 [patent_no_of_words] => 3772 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/280/05280957.pdf [firstpage_image] =>[orig_patent_app_number] => 941812 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/941812
Subframe for a motor vehicle Sep 7, 1992 Issued
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