Search

Michael B. Kreiner

Examiner (ID: 2194, Phone: (571)270-5379 , Office: P/3644 )

Most Active Art Unit
3644
Art Unit(s)
3642, 3644, 4174
Total Applications
917
Issued Applications
771
Pending Applications
58
Abandoned Applications
124

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 11929505 [patent_doc_number] => 09796488 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-10-24 [patent_title] => 'Dual port payload attach ring compatible satellite' [patent_app_type] => utility [patent_app_number] => 14/873990 [patent_app_country] => US [patent_app_date] => 2015-10-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 3922 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14873990 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/873990
Dual port payload attach ring compatible satellite Oct 1, 2015 Issued
Array ( [id] => 16908748 [patent_doc_number] => 11040770 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-06-22 [patent_title] => Single collective stick for a rotary wing aircraft [patent_app_type] => utility [patent_app_number] => 15/504227 [patent_app_country] => US [patent_app_date] => 2015-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 18 [patent_no_of_words] => 9350 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15504227 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/504227
Single collective stick for a rotary wing aircraft Sep 29, 2015 Issued
Array ( [id] => 11528280 [patent_doc_number] => 20170088257 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-30 [patent_title] => 'UNIFIED CONTROL OF MULTIPLE ACTIVE SYSTEMS FOR HELICOPTER VIBRATION SUPPRESSION' [patent_app_type] => utility [patent_app_number] => 14/871615 [patent_app_country] => US [patent_app_date] => 2015-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3917 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14871615 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/871615
UNIFIED CONTROL OF MULTIPLE ACTIVE SYSTEMS FOR HELICOPTER VIBRATION SUPPRESSION Sep 29, 2015 Abandoned
Array ( [id] => 12016626 [patent_doc_number] => 09809316 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-11-07 [patent_title] => 'Aircraft sill height compensating evacuation system' [patent_app_type] => utility [patent_app_number] => 14/866328 [patent_app_country] => US [patent_app_date] => 2015-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3446 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14866328 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/866328
Aircraft sill height compensating evacuation system Sep 24, 2015 Issued
Array ( [id] => 13660783 [patent_doc_number] => 10160541 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2018-12-25 [patent_title] => Circumferentially-driven propulsion mechanism [patent_app_type] => utility [patent_app_number] => 14/866557 [patent_app_country] => US [patent_app_date] => 2015-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 10373 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14866557 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/866557
Circumferentially-driven propulsion mechanism Sep 24, 2015 Issued
Array ( [id] => 10750466 [patent_doc_number] => 20160096618 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-04-07 [patent_title] => 'AIRCRAFT TAXIING SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/865924 [patent_app_country] => US [patent_app_date] => 2015-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3962 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14865924 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/865924
Aircraft taxiing system Sep 24, 2015 Issued
Array ( [id] => 10744037 [patent_doc_number] => 20160090188 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-03-31 [patent_title] => 'QUICK RELEASE SYSTEM FOR A COUPLING AND DROGUE ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 14/865068 [patent_app_country] => US [patent_app_date] => 2015-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4231 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14865068 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/865068
Quick release system for a coupling and drogue assembly Sep 24, 2015 Issued
Array ( [id] => 11533502 [patent_doc_number] => 20170093483 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-30 [patent_title] => 'HYBRID COMMUNICATIONS ASSEMBLY FOR SPACECRAFT' [patent_app_type] => utility [patent_app_number] => 14/864698 [patent_app_country] => US [patent_app_date] => 2015-09-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5294 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14864698 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/864698
Hybrid communications assembly for spacecraft Sep 23, 2015 Issued
Array ( [id] => 11851081 [patent_doc_number] => 20170225573 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-08-10 [patent_title] => 'HYBRID ELECTRIC POWER DRIVE SYSTEM FOR A ROTORCRAFT' [patent_app_type] => utility [patent_app_number] => 15/501337 [patent_app_country] => US [patent_app_date] => 2015-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6113 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15501337 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/501337
Hybrid electric power drive system for a rotorcraft Sep 21, 2015 Issued
Array ( [id] => 11844266 [patent_doc_number] => 09731810 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-08-15 [patent_title] => 'System and method for improving fuel storage within a wing of an aircraft' [patent_app_type] => utility [patent_app_number] => 14/860943 [patent_app_country] => US [patent_app_date] => 2015-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 25 [patent_no_of_words] => 12628 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14860943 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/860943
System and method for improving fuel storage within a wing of an aircraft Sep 21, 2015 Issued
Array ( [id] => 11513962 [patent_doc_number] => 20170081035 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-23 [patent_title] => 'AFT ENGINE FOR AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/859514 [patent_app_country] => US [patent_app_date] => 2015-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5530 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14859514 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/859514
Aft engine for an aircraft Sep 20, 2015 Issued
Array ( [id] => 12037335 [patent_doc_number] => 09815552 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-11-14 [patent_title] => 'Unmanned aerial vehicle with center mounted fuselage and closed wing' [patent_app_type] => utility [patent_app_number] => 14/860377 [patent_app_country] => US [patent_app_date] => 2015-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 7724 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 187 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14860377 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/860377
Unmanned aerial vehicle with center mounted fuselage and closed wing Sep 20, 2015 Issued
Array ( [id] => 11677987 [patent_doc_number] => 09676501 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-06-13 [patent_title] => 'Space solar array architecture for ultra-high power applications' [patent_app_type] => utility [patent_app_number] => 14/841631 [patent_app_country] => US [patent_app_date] => 2015-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 11163 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 232 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14841631 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/841631
Space solar array architecture for ultra-high power applications Aug 30, 2015 Issued
Array ( [id] => 10505891 [patent_doc_number] => 09233754 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2016-01-12 [patent_title] => 'Unmanned aerial vehicle and operations thereof' [patent_app_type] => utility [patent_app_number] => 14/836344 [patent_app_country] => US [patent_app_date] => 2015-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 12121 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 241 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14836344 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/836344
Unmanned aerial vehicle and operations thereof Aug 25, 2015 Issued
Array ( [id] => 11865774 [patent_doc_number] => 20170233059 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-08-17 [patent_title] => 'AIRFOILS FOR STUNT FLIGHTS' [patent_app_type] => utility [patent_app_number] => 15/504625 [patent_app_country] => US [patent_app_date] => 2015-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 1535 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15504625 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/504625
Airfoils for stunt flights Aug 17, 2015 Issued
Array ( [id] => 11220229 [patent_doc_number] => 09448562 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2016-09-20 [patent_title] => 'Utilizing acceleration information for precision landing of unmanned aerial vehicles' [patent_app_type] => utility [patent_app_number] => 14/829226 [patent_app_country] => US [patent_app_date] => 2015-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 16034 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14829226 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/829226
Utilizing acceleration information for precision landing of unmanned aerial vehicles Aug 17, 2015 Issued
Array ( [id] => 10468286 [patent_doc_number] => 20150353300 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-10 [patent_title] => 'RAPID STORE LOAD SYSTEM FOR AIRCRAFT AND METHOD OF OPERATION THEREOF' [patent_app_type] => utility [patent_app_number] => 14/828343 [patent_app_country] => US [patent_app_date] => 2015-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 22037 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14828343 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/828343
Rapid store load system for aircraft and method of operation thereof Aug 16, 2015 Issued
Array ( [id] => 10162250 [patent_doc_number] => 09193464 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-11-24 [patent_title] => 'Aircraft having a recessed cavity in an aft pressure bulkhead wall surface and a galley moved rearwardly into the recessed cavity increasing floor space in front of the galley' [patent_app_type] => utility [patent_app_number] => 14/799884 [patent_app_country] => US [patent_app_date] => 2015-07-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1663 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14799884 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/799884
Aircraft having a recessed cavity in an aft pressure bulkhead wall surface and a galley moved rearwardly into the recessed cavity increasing floor space in front of the galley Jul 14, 2015 Issued
Array ( [id] => 10490845 [patent_doc_number] => 20150375866 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-31 [patent_title] => 'Aeroplane Equipped With An Internal Escape Hatch Incorporating A Pressure Regulating System' [patent_app_type] => utility [patent_app_number] => 14/750114 [patent_app_country] => US [patent_app_date] => 2015-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7414 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14750114 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/750114
Aeroplane equipped with an internal escape hatch incorporating a pressure regulating system Jun 24, 2015 Issued
Array ( [id] => 11408581 [patent_doc_number] => 09555872 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-01-31 [patent_title] => 'Aeroplane equipped with an internal escape hatch having a double opening controller' [patent_app_type] => utility [patent_app_number] => 14/749854 [patent_app_country] => US [patent_app_date] => 2015-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 26 [patent_no_of_words] => 7355 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14749854 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/749854
Aeroplane equipped with an internal escape hatch having a double opening controller Jun 24, 2015 Issued
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