
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] => 3771831
[patent_doc_number] => 05735485
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-07
[patent_title] => 'Variable slot airbrake for aircraft wing'
[patent_app_type] => 1
[patent_app_number] => 8/577834
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4129
[patent_no_of_claims] => 13
[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/05/735/05735485.pdf
[firstpage_image] =>[orig_patent_app_number] => 577834
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577834 | Variable slot airbrake for aircraft wing | Dec 21, 1995 | Issued |
Array
(
[id] => 3860586
[patent_doc_number] => 05746398
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-05
[patent_title] => 'Force-gradient cyclic stick system for a helicopter'
[patent_app_type] => 1
[patent_app_number] => 8/577130
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 5541
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 465
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/746/05746398.pdf
[firstpage_image] =>[orig_patent_app_number] => 577130
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577130 | Force-gradient cyclic stick system for a helicopter | Dec 21, 1995 | Issued |
Array
(
[id] => 3882982
[patent_doc_number] => 05893534
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-04-13
[patent_title] => 'Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads'
[patent_app_type] => 1
[patent_app_number] => 8/577319
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 9
[patent_no_of_words] => 1690
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/893/05893534.pdf
[firstpage_image] =>[orig_patent_app_number] => 577319
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577319 | Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads | Dec 21, 1995 | Issued |
Array
(
[id] => 3684123
[patent_doc_number] => 05676334
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-10-14
[patent_title] => 'Cyclic minimizer through alignment of the center of gravity and direction of flight vectors'
[patent_app_type] => 1
[patent_app_number] => 8/576603
[patent_app_country] => US
[patent_app_date] => 1995-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6941
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/676/05676334.pdf
[firstpage_image] =>[orig_patent_app_number] => 576603
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/576603 | Cyclic minimizer through alignment of the center of gravity and direction of flight vectors | Dec 20, 1995 | Issued |
Array
(
[id] => 3811952
[patent_doc_number] => 05730394
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-24
[patent_title] => 'Vertical performance limit compensator'
[patent_app_type] => 1
[patent_app_number] => 8/575452
[patent_app_country] => US
[patent_app_date] => 1995-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4954
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 156
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/730/05730394.pdf
[firstpage_image] =>[orig_patent_app_number] => 575452
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/575452 | Vertical performance limit compensator | Dec 19, 1995 | Issued |
Array
(
[id] => 3755430
[patent_doc_number] => 05732907
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-31
[patent_title] => 'Ejection seat buckle'
[patent_app_type] => 1
[patent_app_number] => 8/574381
[patent_app_country] => US
[patent_app_date] => 1995-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 1498
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/732/05732907.pdf
[firstpage_image] =>[orig_patent_app_number] => 574381
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/574381 | Ejection seat buckle | Dec 17, 1995 | Issued |
Array
(
[id] => 3775104
[patent_doc_number] => 05779169
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-14
[patent_title] => 'Aircraft engine inlet hot gas and foreign object ingestion reduction and pitch control system'
[patent_app_type] => 1
[patent_app_number] => 8/573047
[patent_app_country] => US
[patent_app_date] => 1995-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 7917
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 311
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/779/05779169.pdf
[firstpage_image] =>[orig_patent_app_number] => 573047
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/573047 | Aircraft engine inlet hot gas and foreign object ingestion reduction and pitch control system | Dec 14, 1995 | Issued |
Array
(
[id] => 3775495
[patent_doc_number] => 05779196
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-14
[patent_title] => 'Ram air drive laminar flow control system'
[patent_app_type] => 1
[patent_app_number] => 8/569907
[patent_app_country] => US
[patent_app_date] => 1995-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4331
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/779/05779196.pdf
[firstpage_image] =>[orig_patent_app_number] => 569907
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/569907 | Ram air drive laminar flow control system | Dec 7, 1995 | Issued |
Array
(
[id] => 4046971
[patent_doc_number] => 05865397
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-02-02
[patent_title] => 'Method and apparatus for creating detail surfaces on composite aircraft structures'
[patent_app_type] => 1
[patent_app_number] => 8/567542
[patent_app_country] => US
[patent_app_date] => 1995-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 4635
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/865/05865397.pdf
[firstpage_image] =>[orig_patent_app_number] => 567542
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/567542 | Method and apparatus for creating detail surfaces on composite aircraft structures | Dec 4, 1995 | Issued |
Array
(
[id] => 3874564
[patent_doc_number] => 05722621
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-03
[patent_title] => 'Bipod load support'
[patent_app_type] => 1
[patent_app_number] => 8/567621
[patent_app_country] => US
[patent_app_date] => 1995-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2417
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 366
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/722/05722621.pdf
[firstpage_image] =>[orig_patent_app_number] => 567621
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/567621 | Bipod load support | Dec 4, 1995 | Issued |
Array
(
[id] => 3861314
[patent_doc_number] => 05803410
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-08
[patent_title] => 'Skin friction reduction by micro-blowing technique'
[patent_app_type] => 1
[patent_app_number] => 8/566211
[patent_app_country] => US
[patent_app_date] => 1995-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 16
[patent_no_of_words] => 3446
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/803/05803410.pdf
[firstpage_image] =>[orig_patent_app_number] => 566211
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/566211 | Skin friction reduction by micro-blowing technique | Nov 30, 1995 | Issued |
Array
(
[id] => 3801722
[patent_doc_number] => 05709356
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-01-20
[patent_title] => 'Anti-spark structure, in particular for aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/549670
[patent_app_country] => US
[patent_app_date] => 1995-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2814
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 242
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/709/05709356.pdf
[firstpage_image] =>[orig_patent_app_number] => 549670
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/549670 | Anti-spark structure, in particular for aircraft | Nov 29, 1995 | Issued |
Array
(
[id] => 3775439
[patent_doc_number] => 05779192
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-14
[patent_title] => 'Thrust reverser with improved forward thrust efficiency'
[patent_app_type] => 1
[patent_app_number] => 8/566433
[patent_app_country] => US
[patent_app_date] => 1995-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 2090
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 169
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/779/05779192.pdf
[firstpage_image] =>[orig_patent_app_number] => 566433
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/566433 | Thrust reverser with improved forward thrust efficiency | Nov 29, 1995 | Issued |
Array
(
[id] => 3874494
[patent_doc_number] => 05722616
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-03
[patent_title] => 'Conical rotary actuator and its application to the control of a rudder'
[patent_app_type] => 1
[patent_app_number] => 8/562761
[patent_app_country] => US
[patent_app_date] => 1995-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4698
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 147
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/722/05722616.pdf
[firstpage_image] =>[orig_patent_app_number] => 562761
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/562761 | Conical rotary actuator and its application to the control of a rudder | Nov 26, 1995 | Issued |
Array
(
[id] => 3775412
[patent_doc_number] => 05779190
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-14
[patent_title] => 'Portable unmanned aerial vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/561929
[patent_app_country] => US
[patent_app_date] => 1995-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 3042
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/779/05779190.pdf
[firstpage_image] =>[orig_patent_app_number] => 561929
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/561929 | Portable unmanned aerial vehicle | Nov 21, 1995 | Issued |
| 08/553124 | SYSTEM FOR PROGRAMMING PROGRAMMABLE HEARING AIDS AND UPDATING DATABASE OF PATIENT INFORMATION | Nov 6, 1995 | Abandoned |
Array
(
[id] => 3847200
[patent_doc_number] => 05794892
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-18
[patent_title] => 'Critical nutation dampling on spinning bodies via momentum wheels or similar devices'
[patent_app_type] => 1
[patent_app_number] => 8/548158
[patent_app_country] => US
[patent_app_date] => 1995-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 12
[patent_no_of_words] => 3852
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/794/05794892.pdf
[firstpage_image] =>[orig_patent_app_number] => 548158
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/548158 | Critical nutation dampling on spinning bodies via momentum wheels or similar devices | Oct 24, 1995 | Issued |
Array
(
[id] => 3860545
[patent_doc_number] => 05746395
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-05
[patent_title] => 'Helicopter seat safety system'
[patent_app_type] => 1
[patent_app_number] => 8/546073
[patent_app_country] => US
[patent_app_date] => 1995-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3970
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 82
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/746/05746395.pdf
[firstpage_image] =>[orig_patent_app_number] => 546073
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/546073 | Helicopter seat safety system | Oct 19, 1995 | Issued |
Array
(
[id] => 3843096
[patent_doc_number] => 05704567
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-01-06
[patent_title] => 'Blade de-icer for rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/543688
[patent_app_country] => US
[patent_app_date] => 1995-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 9
[patent_no_of_words] => 2351
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 155
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/704/05704567.pdf
[firstpage_image] =>[orig_patent_app_number] => 543688
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/543688 | Blade de-icer for rotary wing aircraft | Oct 15, 1995 | Issued |
Array
(
[id] => 3608670
[patent_doc_number] => 05687933
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-11-18
[patent_title] => 'Attitude control for spacecraft with movable appendages such as solar panels'
[patent_app_type] => 1
[patent_app_number] => 8/543733
[patent_app_country] => US
[patent_app_date] => 1995-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2481
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 449
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/687/05687933.pdf
[firstpage_image] =>[orig_patent_app_number] => 543733
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/543733 | Attitude control for spacecraft with movable appendages such as solar panels | Oct 15, 1995 | Issued |