
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 |
|---|---|---|---|
| 07/938674 | APPARATUS FOR DISCHARGING PARTICULATE MATERIAL | Aug 31, 1992 | Abandoned |
Array
(
[id] => 3080761
[patent_doc_number] => 05297760
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-03-29
[patent_title] => 'Aircraft skin lap splice'
[patent_app_type] => 1
[patent_app_number] => 7/933255
[patent_app_country] => US
[patent_app_date] => 1992-08-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 4061
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/297/05297760.pdf
[firstpage_image] =>[orig_patent_app_number] => 933255
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/933255 | Aircraft skin lap splice | Aug 20, 1992 | Issued |
Array
(
[id] => 2939289
[patent_doc_number] => 05242178
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-09-07
[patent_title] => 'Hitch for attaching a trailer to a bicycle'
[patent_app_type] => 1
[patent_app_number] => 7/931702
[patent_app_country] => US
[patent_app_date] => 1992-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 14
[patent_no_of_words] => 2569
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/242/05242178.pdf
[firstpage_image] =>[orig_patent_app_number] => 931702
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/931702 | Hitch for attaching a trailer to a bicycle | Aug 17, 1992 | Issued |
Array
(
[id] => 2929064
[patent_doc_number] => 05253825
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-19
[patent_title] => 'Aircraft ski'
[patent_app_type] => 1
[patent_app_number] => 7/921945
[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] => 3767
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 323
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/253/05253825.pdf
[firstpage_image] =>[orig_patent_app_number] => 921945
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/921945 | Aircraft ski | Jul 29, 1992 | Issued |
Array
(
[id] => 2993250
[patent_doc_number] => 05354016
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-10-11
[patent_title] => 'Pivoted wheel roll control with automatic offset'
[patent_app_type] => 1
[patent_app_number] => 7/922306
[patent_app_country] => US
[patent_app_date] => 1992-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2218
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/354/05354016.pdf
[firstpage_image] =>[orig_patent_app_number] => 922306
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/922306 | Pivoted wheel roll control with automatic offset | Jul 29, 1992 | Issued |
Array
(
[id] => 2998886
[patent_doc_number] => 05308024
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-05-03
[patent_title] => 'Disturbance torque compensated three axis yaw control system'
[patent_app_type] => 1
[patent_app_number] => 7/916734
[patent_app_country] => US
[patent_app_date] => 1992-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 4580
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 425
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/308/05308024.pdf
[firstpage_image] =>[orig_patent_app_number] => 916734
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/916734 | Disturbance torque compensated three axis yaw control system | Jul 19, 1992 | Issued |
Array
(
[id] => 2929118
[patent_doc_number] => 05253828
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-19
[patent_title] => 'Concealable flap-actuated vortex generator'
[patent_app_type] => 1
[patent_app_number] => 7/916316
[patent_app_country] => US
[patent_app_date] => 1992-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 16
[patent_no_of_words] => 5323
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/253/05253828.pdf
[firstpage_image] =>[orig_patent_app_number] => 916316
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/916316 | Concealable flap-actuated vortex generator | Jul 16, 1992 | Issued |
Array
(
[id] => 2995840
[patent_doc_number] => 05275362
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-04
[patent_title] => 'Multiple port connection pneumatic deicing system'
[patent_app_type] => 1
[patent_app_number] => 7/914956
[patent_app_country] => US
[patent_app_date] => 1992-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2648
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 175
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/275/05275362.pdf
[firstpage_image] =>[orig_patent_app_number] => 914956
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/914956 | Multiple port connection pneumatic deicing system | Jul 15, 1992 | Issued |
Array
(
[id] => 3036631
[patent_doc_number] => 05305971
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-04-26
[patent_title] => 'Spacecraft control by electrochromic devices'
[patent_app_type] => 1
[patent_app_number] => 7/913106
[patent_app_country] => US
[patent_app_date] => 1992-07-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2205
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/305/05305971.pdf
[firstpage_image] =>[orig_patent_app_number] => 913106
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/913106 | Spacecraft control by electrochromic devices | Jul 13, 1992 | Issued |
Array
(
[id] => 2961233
[patent_doc_number] => 05255880
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-26
[patent_title] => 'Fly by wire/fly by light control system with manual override'
[patent_app_type] => 1
[patent_app_number] => 7/912407
[patent_app_country] => US
[patent_app_date] => 1992-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1327
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/255/05255880.pdf
[firstpage_image] =>[orig_patent_app_number] => 912407
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/912407 | Fly by wire/fly by light control system with manual override | Jul 12, 1992 | Issued |
Array
(
[id] => 3055682
[patent_doc_number] => 05294078
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-03-15
[patent_title] => 'Integrated system and method for assembling, and then transporting and supporting a launch vehicle'
[patent_app_type] => 1
[patent_app_number] => 7/909966
[patent_app_country] => US
[patent_app_date] => 1992-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 19
[patent_no_of_words] => 3375
[patent_no_of_claims] => 45
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/294/05294078.pdf
[firstpage_image] =>[orig_patent_app_number] => 909966
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/909966 | Integrated system and method for assembling, and then transporting and supporting a launch vehicle | Jul 6, 1992 | Issued |
Array
(
[id] => 2938474
[patent_doc_number] => 05242135
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-09-07
[patent_title] => 'Space transfer vehicle and integrated guidance launch system'
[patent_app_type] => 1
[patent_app_number] => 7/908345
[patent_app_country] => US
[patent_app_date] => 1992-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2497
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/242/05242135.pdf
[firstpage_image] =>[orig_patent_app_number] => 908345
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/908345 | Space transfer vehicle and integrated guidance launch system | Jul 5, 1992 | Issued |
Array
(
[id] => 3006570
[patent_doc_number] => 05326051
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-07-05
[patent_title] => 'Electro-expulsive deicing system having circuit board expulsive members'
[patent_app_type] => 1
[patent_app_number] => 7/906714
[patent_app_country] => US
[patent_app_date] => 1992-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4122
[patent_no_of_claims] => 29
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/326/05326051.pdf
[firstpage_image] =>[orig_patent_app_number] => 906714
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/906714 | Electro-expulsive deicing system having circuit board expulsive members | Jun 29, 1992 | Issued |
| 07/904570 | ELECTROMAGNETIC DEVICE AND METHOD FOR BOUNDARY LAYER CONTROL | Jun 25, 1992 | Abandoned |
Array
(
[id] => 3082821
[patent_doc_number] => 05318255
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-06-07
[patent_title] => 'Stage separation mechanism for space vehicles'
[patent_app_type] => 1
[patent_app_number] => 7/902270
[patent_app_country] => US
[patent_app_date] => 1992-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3873
[patent_no_of_claims] => 14
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[patent_words_short_claim] => 176
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/318/05318255.pdf
[firstpage_image] =>[orig_patent_app_number] => 902270
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/902270 | Stage separation mechanism for space vehicles | Jun 21, 1992 | Issued |
Array
(
[id] => 3051037
[patent_doc_number] => 05351913
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-10-04
[patent_title] => 'Coaxial transmission/center hub subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors'
[patent_app_type] => 1
[patent_app_number] => 7/903065
[patent_app_country] => US
[patent_app_date] => 1992-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 25
[patent_no_of_words] => 14534
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 292
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/351/05351913.pdf
[firstpage_image] =>[orig_patent_app_number] => 903065
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/903065 | Coaxial transmission/center hub subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors | Jun 21, 1992 | Issued |
Array
(
[id] => 2995822
[patent_doc_number] => 05275361
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-04
[patent_title] => 'Venting a space to relieve pressure generated by an explosion'
[patent_app_type] => 1
[patent_app_number] => 7/897495
[patent_app_country] => US
[patent_app_date] => 1992-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 964
[patent_no_of_claims] => 2
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[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/275/05275361.pdf
[firstpage_image] =>[orig_patent_app_number] => 897495
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/897495 | Venting a space to relieve pressure generated by an explosion | Jun 11, 1992 | Issued |
Array
(
[id] => 2956761
[patent_doc_number] => 05257757
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-02
[patent_title] => 'Advanced hypersonic nosecap'
[patent_app_type] => 1
[patent_app_number] => 7/901617
[patent_app_country] => US
[patent_app_date] => 1992-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2534
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 5
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/257/05257757.pdf
[firstpage_image] =>[orig_patent_app_number] => 901617
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/901617 | Advanced hypersonic nosecap | Jun 10, 1992 | Issued |
Array
(
[id] => 2961163
[patent_doc_number] => 05255876
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-26
[patent_title] => 'Linear lift and counterbalance aircraft passenger door'
[patent_app_type] => 1
[patent_app_number] => 7/896524
[patent_app_country] => US
[patent_app_date] => 1992-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 728
[patent_no_of_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/255/05255876.pdf
[firstpage_image] =>[orig_patent_app_number] => 896524
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/896524 | Linear lift and counterbalance aircraft passenger door | Jun 7, 1992 | Issued |
Array
(
[id] => 2818063
[patent_doc_number] => 05174523
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-29
[patent_title] => 'Compound helicopter with engine shaft power output control'
[patent_app_type] => 1
[patent_app_number] => 7/895166
[patent_app_country] => US
[patent_app_date] => 1992-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2670
[patent_no_of_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/174/05174523.pdf
[firstpage_image] =>[orig_patent_app_number] => 895166
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/895166 | Compound helicopter with engine shaft power output control | Jun 4, 1992 | Issued |