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] => 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
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