Search

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 numberTitle of the applicationFiling DateStatus
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
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