
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
| 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
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[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
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[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
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[patent_no_of_words] => 2000
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[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
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[patent_no_of_words] => 6341
[patent_no_of_claims] => 21
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[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
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[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
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[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
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[patent_no_of_words] => 3091
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[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
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[patent_no_of_words] => 2189
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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 |