Search

Adam M. Weidner

Examiner (ID: 9647, Phone: (571)272-3045 , Office: P/1649 )

Most Active Art Unit
1649
Art Unit(s)
1649, 1651, 1675
Total Applications
751
Issued Applications
449
Pending Applications
66
Abandoned Applications
245

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 11829374 [patent_doc_number] => 09726111 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-08 [patent_title] => 'Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method' [patent_app_type] => utility [patent_app_number] => 13/950608 [patent_app_country] => US [patent_app_date] => 2013-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3048 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13950608 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/950608
Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method Jul 24, 2013 Issued
Array ( [id] => 11829374 [patent_doc_number] => 09726111 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-08 [patent_title] => 'Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method' [patent_app_type] => utility [patent_app_number] => 13/950608 [patent_app_country] => US [patent_app_date] => 2013-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3048 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13950608 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/950608
Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method Jul 24, 2013 Issued
Array ( [id] => 11829374 [patent_doc_number] => 09726111 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-08 [patent_title] => 'Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method' [patent_app_type] => utility [patent_app_number] => 13/950608 [patent_app_country] => US [patent_app_date] => 2013-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3048 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13950608 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/950608
Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method Jul 24, 2013 Issued
Array ( [id] => 11829374 [patent_doc_number] => 09726111 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-08 [patent_title] => 'Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method' [patent_app_type] => utility [patent_app_number] => 13/950608 [patent_app_country] => US [patent_app_date] => 2013-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3048 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13950608 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/950608
Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method Jul 24, 2013 Issued
Array ( [id] => 9808585 [patent_doc_number] => 20150020530 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-01-22 [patent_title] => 'GAS TURBINE EMISSIONS CONTROL SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 13/945793 [patent_app_country] => US [patent_app_date] => 2013-07-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6619 [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] => 13945793 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/945793
GAS TURBINE EMISSIONS CONTROL SYSTEM AND METHOD Jul 17, 2013 Abandoned
Array ( [id] => 9808584 [patent_doc_number] => 20150020529 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-01-22 [patent_title] => 'GAS TURBINE EMISSIONS CONTROL SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 13/945786 [patent_app_country] => US [patent_app_date] => 2013-07-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6824 [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] => 13945786 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/945786
GAS TURBINE EMISSIONS CONTROL SYSTEM AND METHOD Jul 17, 2013 Abandoned
Array ( [id] => 10400490 [patent_doc_number] => 20150285499 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-08 [patent_title] => 'LOCAL IMPROVEMENT OF THE MIXTURE OF AIR AND FUEL IN BURNERS COMPRISING SWIRL GENERATORS HAVING BLADE ENDS THAT ARE CROSSED IN THE OUTER REGION' [patent_app_type] => utility [patent_app_number] => 14/420204 [patent_app_country] => US [patent_app_date] => 2013-06-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1635 [patent_no_of_claims] => 6 [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] => 14420204 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/420204
Local improvement of the mixture of air and fuel in burners comprising swirl generators having blade ends that are crossed in the outer region Jun 12, 2013 Issued
Array ( [id] => 9302685 [patent_doc_number] => 20140041359 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-02-13 [patent_title] => 'RAPID STARTUP HEAT RECOVERY STEAM GENERATOR' [patent_app_type] => utility [patent_app_number] => 13/914695 [patent_app_country] => US [patent_app_date] => 2013-06-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 5644 [patent_no_of_claims] => 28 [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] => 13914695 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/914695
RAPID STARTUP HEAT RECOVERY STEAM GENERATOR Jun 10, 2013 Abandoned
Array ( [id] => 10957133 [patent_doc_number] => 20140360155 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-12-11 [patent_title] => 'MICROCHANNEL SYSTEMS AND METHODS FOR COOLING TURBINE COMPONENTS OF A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 13/912582 [patent_app_country] => US [patent_app_date] => 2013-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5371 [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] => 13912582 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/912582
MICROCHANNEL SYSTEMS AND METHODS FOR COOLING TURBINE COMPONENTS OF A GAS TURBINE ENGINE Jun 6, 2013 Abandoned
Array ( [id] => 13141039 [patent_doc_number] => 10087842 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-10-02 [patent_title] => Turbojet engine nacelle reinforcing structure [patent_app_type] => utility [patent_app_number] => 13/894647 [patent_app_country] => US [patent_app_date] => 2013-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 9 [patent_no_of_words] => 5096 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 200 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13894647 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/894647
Turbojet engine nacelle reinforcing structure May 14, 2013 Issued
Array ( [id] => 13857437 [patent_doc_number] => 10190430 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-01-29 [patent_title] => Turbine engine, such as a turbojet or a turboprop engine [patent_app_type] => utility [patent_app_number] => 14/385867 [patent_app_country] => US [patent_app_date] => 2013-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 3269 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 292 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14385867 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/385867
Turbine engine, such as a turbojet or a turboprop engine Apr 8, 2013 Issued
Array ( [id] => 9770896 [patent_doc_number] => 20140294559 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-10-02 [patent_title] => 'MULTIPLE MODE GAS TURBINE ENGINE GAS FUEL SYSTEM WITH INTEGRATED CONTROL' [patent_app_type] => utility [patent_app_number] => 13/852292 [patent_app_country] => US [patent_app_date] => 2013-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4319 [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] => 13852292 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/852292
MULTIPLE MODE GAS TURBINE ENGINE GAS FUEL SYSTEM WITH INTEGRATED CONTROL Mar 27, 2013 Abandoned
Array ( [id] => 10250728 [patent_doc_number] => 20150135725 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-05-21 [patent_title] => 'GAS-TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 13/261958 [patent_app_country] => US [patent_app_date] => 2013-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2414 [patent_no_of_claims] => 5 [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] => 13261958 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/261958
GAS-TURBINE ENGINE Mar 25, 2013 Abandoned
Array ( [id] => 11358141 [patent_doc_number] => 09534787 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-01-03 [patent_title] => 'Micromixing cap assembly' [patent_app_type] => utility [patent_app_number] => 13/797925 [patent_app_country] => US [patent_app_date] => 2013-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6737 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13797925 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/797925
Micromixing cap assembly Mar 11, 2013 Issued
Array ( [id] => 9715785 [patent_doc_number] => 20140251483 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-09-11 [patent_title] => 'TUBE ASSEMBLY FOR USE IN FUEL INJECTION ASSEMBLIES AND METHODS OF ASSEMBLING SAME' [patent_app_type] => utility [patent_app_number] => 13/788812 [patent_app_country] => US [patent_app_date] => 2013-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3753 [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] => 13788812 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/788812
TUBE ASSEMBLY FOR USE IN FUEL INJECTION ASSEMBLIES AND METHODS OF ASSEMBLING SAME Mar 6, 2013 Abandoned
Array ( [id] => 9696060 [patent_doc_number] => 20140245746 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-09-04 [patent_title] => 'COMBUSTION ARRANGEMENT AND METHOD OF REDUCING PRESSURE FLUCTUATIONS OF A COMBUSTION ARRANGEMENT' [patent_app_type] => utility [patent_app_number] => 13/784052 [patent_app_country] => US [patent_app_date] => 2013-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1853 [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] => 13784052 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/784052
COMBUSTION ARRANGEMENT AND METHOD OF REDUCING PRESSURE FLUCTUATIONS OF A COMBUSTION ARRANGEMENT Mar 3, 2013 Abandoned
Array ( [id] => 10367726 [patent_doc_number] => 20150252731 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-09-10 [patent_title] => 'GAS TURBINE ENGINE INCLUDING BLEED SYSTEM COUPLED TO UPSTREAM AND DOWNSTREAM LOCATIONS OF COMPRESSOR' [patent_app_type] => utility [patent_app_number] => 14/431316 [patent_app_country] => US [patent_app_date] => 2013-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2791 [patent_no_of_claims] => 17 [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] => 14431316 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/431316
GAS TURBINE ENGINE INCLUDING BLEED SYSTEM COUPLED TO UPSTREAM AND DOWNSTREAM LOCATIONS OF COMPRESSOR Feb 21, 2013 Abandoned
Array ( [id] => 9612303 [patent_doc_number] => 20140202160 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-24 [patent_title] => 'GAS TURBINE SYSTEM WITH MANIFOLD' [patent_app_type] => utility [patent_app_number] => 13/749661 [patent_app_country] => US [patent_app_date] => 2013-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4175 [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] => 13749661 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/749661
GAS TURBINE SYSTEM WITH MANIFOLD Jan 23, 2013 Abandoned
Array ( [id] => 10469803 [patent_doc_number] => 20150354819 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-10 [patent_title] => 'Combustor Cooled Quench Zone Array' [patent_app_type] => utility [patent_app_number] => 14/759811 [patent_app_country] => US [patent_app_date] => 2013-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3312 [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] => 14759811 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/759811
Combustor Cooled Quench Zone Array Jan 15, 2013 Abandoned
Array ( [id] => 10476882 [patent_doc_number] => 20150361899 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-17 [patent_title] => 'Fire Shield for a Gas Turbine Engine' [patent_app_type] => utility [patent_app_number] => 14/760612 [patent_app_country] => US [patent_app_date] => 2013-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 1603 [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] => 14760612 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/760612
Fire Shield for a Gas Turbine Engine Jan 14, 2013 Abandoned
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