
William Alexander Grant
Examiner (ID: 3268)
| Most Active Art Unit | 3104 |
| Art Unit(s) | 3641, 3613, 2121, 2786, 3104 |
| Total Applications | 665 |
| Issued Applications | 580 |
| Pending Applications | 19 |
| Abandoned Applications | 66 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 3987352
[patent_doc_number] => 06003814
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-12-21
[patent_title] => 'Double-walled duct assembly for aircraft anti-icing conduit systems'
[patent_app_type] => 1
[patent_app_number] => 8/668434
[patent_app_country] => US
[patent_app_date] => 1996-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2545
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 41
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/003/06003814.pdf
[firstpage_image] =>[orig_patent_app_number] => 668434
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/668434 | Double-walled duct assembly for aircraft anti-icing conduit systems | Jun 16, 1996 | Issued |
Array
(
[id] => 4030349
[patent_doc_number] => 05873544
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-02-23
[patent_title] => 'Slidable duct assembly for aircraft anti-icing conduit systems'
[patent_app_type] => 1
[patent_app_number] => 8/664704
[patent_app_country] => US
[patent_app_date] => 1996-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 2797
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/873/05873544.pdf
[firstpage_image] =>[orig_patent_app_number] => 664704
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/664704 | Slidable duct assembly for aircraft anti-icing conduit systems | Jun 16, 1996 | Issued |
Array
(
[id] => 4047012
[patent_doc_number] => 05865400
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-02-02
[patent_title] => 'Multipiece, slidable duct assembly for aircraft anit-icing conduit systems'
[patent_app_type] => 1
[patent_app_number] => 8/668433
[patent_app_country] => US
[patent_app_date] => 1996-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2456
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 229
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/865/05865400.pdf
[firstpage_image] =>[orig_patent_app_number] => 668433
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/668433 | Multipiece, slidable duct assembly for aircraft anit-icing conduit systems | Jun 16, 1996 | Issued |
Array
(
[id] => 3772459
[patent_doc_number] => 05839700
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-24
[patent_title] => 'Articulated fin'
[patent_app_type] => 1
[patent_app_number] => 8/668605
[patent_app_country] => US
[patent_app_date] => 1996-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2493
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/839/05839700.pdf
[firstpage_image] =>[orig_patent_app_number] => 668605
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/668605 | Articulated fin | Jun 2, 1996 | Issued |
Array
(
[id] => 3746874
[patent_doc_number] => 05720452
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-02-24
[patent_title] => 'Solar panel parallel mounting configuration'
[patent_app_type] => 1
[patent_app_number] => 8/655110
[patent_app_country] => US
[patent_app_date] => 1996-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 5506
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 331
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/720/05720452.pdf
[firstpage_image] =>[orig_patent_app_number] => 655110
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/655110 | Solar panel parallel mounting configuration | May 28, 1996 | Issued |
Array
(
[id] => 3810601
[patent_doc_number] => 05758844
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-02
[patent_title] => 'Vertical/short take-off and landing (V/STOL) air vehicle capable of providing high speed horizontal flight'
[patent_app_type] => 1
[patent_app_number] => 8/654133
[patent_app_country] => US
[patent_app_date] => 1996-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 1641
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 215
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/758/05758844.pdf
[firstpage_image] =>[orig_patent_app_number] => 654133
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/654133 | Vertical/short take-off and landing (V/STOL) air vehicle capable of providing high speed horizontal flight | May 27, 1996 | Issued |
Array
(
[id] => 3771878
[patent_doc_number] => 05735488
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-07
[patent_title] => 'Method and apparatus for coupling space vehicles'
[patent_app_type] => 1
[patent_app_number] => 8/654460
[patent_app_country] => US
[patent_app_date] => 1996-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 3661
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 176
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/735/05735488.pdf
[firstpage_image] =>[orig_patent_app_number] => 654460
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/654460 | Method and apparatus for coupling space vehicles | May 27, 1996 | Issued |
Array
(
[id] => 3792720
[patent_doc_number] => 05810287
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-22
[patent_title] => 'Aircraft support pylon'
[patent_app_type] => 1
[patent_app_number] => 8/652965
[patent_app_country] => US
[patent_app_date] => 1996-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3535
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/810/05810287.pdf
[firstpage_image] =>[orig_patent_app_number] => 652965
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/652965 | Aircraft support pylon | May 23, 1996 | Issued |
Array
(
[id] => 3755297
[patent_doc_number] => 05755403
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-26
[patent_title] => 'Aircraft motor pod including a pivotable pod cowling'
[patent_app_type] => 1
[patent_app_number] => 8/652002
[patent_app_country] => US
[patent_app_date] => 1996-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 3967
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 199
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/755/05755403.pdf
[firstpage_image] =>[orig_patent_app_number] => 652002
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/652002 | Aircraft motor pod including a pivotable pod cowling | May 22, 1996 | Issued |
Array
(
[id] => 4031268
[patent_doc_number] => 05868351
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-02-09
[patent_title] => 'Rotor blade stowing system'
[patent_app_type] => 1
[patent_app_number] => 8/653731
[patent_app_country] => US
[patent_app_date] => 1996-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 35
[patent_no_of_words] => 8541
[patent_no_of_claims] => 39
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 269
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/868/05868351.pdf
[firstpage_image] =>[orig_patent_app_number] => 653731
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/653731 | Rotor blade stowing system | May 22, 1996 | Issued |
Array
(
[id] => 3857058
[patent_doc_number] => 05823479
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-20
[patent_title] => 'Landing attitude modifier for airplane'
[patent_app_type] => 1
[patent_app_number] => 8/650413
[patent_app_country] => US
[patent_app_date] => 1996-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 6906
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/823/05823479.pdf
[firstpage_image] =>[orig_patent_app_number] => 650413
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/650413 | Landing attitude modifier for airplane | May 19, 1996 | Issued |
Array
(
[id] => 3717508
[patent_doc_number] => 05692703
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-02
[patent_title] => 'Multiple application wheel well design'
[patent_app_type] => 1
[patent_app_number] => 8/644353
[patent_app_country] => US
[patent_app_date] => 1996-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2058
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 265
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/692/05692703.pdf
[firstpage_image] =>[orig_patent_app_number] => 644353
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/644353 | Multiple application wheel well design | May 9, 1996 | Issued |
Array
(
[id] => 3721335
[patent_doc_number] => 05697579
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-16
[patent_title] => 'Aircraft having inflatable tubular support structure'
[patent_app_type] => 1
[patent_app_number] => 8/642984
[patent_app_country] => US
[patent_app_date] => 1996-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 27
[patent_no_of_words] => 2024
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 126
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/697/05697579.pdf
[firstpage_image] =>[orig_patent_app_number] => 642984
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/642984 | Aircraft having inflatable tubular support structure | May 5, 1996 | Issued |
Array
(
[id] => 3775481
[patent_doc_number] => 05779195
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-14
[patent_title] => 'Satellite assembly having modular common bus components'
[patent_app_type] => 1
[patent_app_number] => 8/642713
[patent_app_country] => US
[patent_app_date] => 1996-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 13
[patent_no_of_words] => 3262
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 33
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/779/05779195.pdf
[firstpage_image] =>[orig_patent_app_number] => 642713
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/642713 | Satellite assembly having modular common bus components | May 2, 1996 | Issued |
Array
(
[id] => 3798677
[patent_doc_number] => 05769362
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-23
[patent_title] => 'Aircraft control mechanism for a speed brake'
[patent_app_type] => 1
[patent_app_number] => 8/639521
[patent_app_country] => US
[patent_app_date] => 1996-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2986
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/769/05769362.pdf
[firstpage_image] =>[orig_patent_app_number] => 639521
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/639521 | Aircraft control mechanism for a speed brake | Apr 30, 1996 | Issued |
Array
(
[id] => 3778226
[patent_doc_number] => 05725181
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-10
[patent_title] => 'Aircraft engine thrust mount'
[patent_app_type] => 1
[patent_app_number] => 8/640698
[patent_app_country] => US
[patent_app_date] => 1996-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 4215
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 227
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/725/05725181.pdf
[firstpage_image] =>[orig_patent_app_number] => 640698
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/640698 | Aircraft engine thrust mount | Apr 30, 1996 | Issued |
Array
(
[id] => 3861261
[patent_doc_number] => 05803406
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-08
[patent_title] => 'Integrated thermal insulation system for spacecraft'
[patent_app_type] => 1
[patent_app_number] => 8/656144
[patent_app_country] => US
[patent_app_date] => 1996-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 3728
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/803/05803406.pdf
[firstpage_image] =>[orig_patent_app_number] => 656144
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/656144 | Integrated thermal insulation system for spacecraft | Apr 21, 1996 | Issued |
Array
(
[id] => 3732510
[patent_doc_number] => 05716032
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-02-10
[patent_title] => 'Unmanned aerial vehicle automatic landing system'
[patent_app_type] => 1
[patent_app_number] => 8/641133
[patent_app_country] => US
[patent_app_date] => 1996-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 4457
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 306
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/716/05716032.pdf
[firstpage_image] =>[orig_patent_app_number] => 641133
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/641133 | Unmanned aerial vehicle automatic landing system | Apr 21, 1996 | Issued |
| 08/634931 | MULTI-AXIS UNFOLDING MECHANISM WITH RATE CONTROLLED SYNCHRONIZED MOVEMENT | Apr 18, 1996 | Abandoned |
Array
(
[id] => 3783358
[patent_doc_number] => 05826822
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-27
[patent_title] => 'System and method for providing cyclic and collective pitch control in a rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/634970
[patent_app_country] => US
[patent_app_date] => 1996-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 13
[patent_no_of_words] => 4115
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/826/05826822.pdf
[firstpage_image] =>[orig_patent_app_number] => 634970
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/634970 | System and method for providing cyclic and collective pitch control in a rotary wing aircraft | Apr 18, 1996 | Issued |