Search

Timothy S. Thorpe

Examiner (ID: 6367)

Most Active Art Unit
3403
Art Unit(s)
3746, 3403
Total Applications
1046
Issued Applications
836
Pending Applications
39
Abandoned Applications
171

Applications

Application numberTitle of the applicationFiling DateStatus
08/204424 INLET CONTROL COMBINATION FOR A COMPRESSOR SYSTEM Mar 15, 1994 Abandoned
Array ( [id] => 2975166 [patent_doc_number] => 05357745 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-10-25 [patent_title] => 'Combustor cap assembly for a combustor casing of a gas turbine' [patent_app_type] => 1 [patent_app_number] => 8/214053 [patent_app_country] => US [patent_app_date] => 1994-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1632 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 133 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/357/05357745.pdf [firstpage_image] =>[orig_patent_app_number] => 214053 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/214053
Combustor cap assembly for a combustor casing of a gas turbine Mar 14, 1994 Issued
Array ( [id] => 3413876 [patent_doc_number] => 05454221 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-10-03 [patent_title] => 'Dilution flow sleeve for reducing emissions in a gas turbine combustor' [patent_app_type] => 1 [patent_app_number] => 8/212407 [patent_app_country] => US [patent_app_date] => 1994-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2265 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/454/05454221.pdf [firstpage_image] =>[orig_patent_app_number] => 212407 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/212407
Dilution flow sleeve for reducing emissions in a gas turbine combustor Mar 13, 1994 Issued
Array ( [id] => 3102617 [patent_doc_number] => 05435126 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-07-25 [patent_title] => 'Fuel nozzle for a turbine having dual capability for diffusion and premix combustion and methods of operation' [patent_app_type] => 1 [patent_app_number] => 8/212401 [patent_app_country] => US [patent_app_date] => 1994-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2599 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/435/05435126.pdf [firstpage_image] =>[orig_patent_app_number] => 212401 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/212401
Fuel nozzle for a turbine having dual capability for diffusion and premix combustion and methods of operation Mar 13, 1994 Issued
Array ( [id] => 3569330 [patent_doc_number] => 05551230 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-09-03 [patent_title] => 'Heat induced high pressure lox pump rocket engine cycle' [patent_app_type] => 1 [patent_app_number] => 8/209282 [patent_app_country] => US [patent_app_date] => 1994-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2149 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/551/05551230.pdf [firstpage_image] =>[orig_patent_app_number] => 209282 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/209282
Heat induced high pressure lox pump rocket engine cycle Mar 13, 1994 Issued
Array ( [id] => 3474219 [patent_doc_number] => 05438821 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-08-08 [patent_title] => 'Method and appliance for influencing the wake of combustion chamber inserts' [patent_app_type] => 1 [patent_app_number] => 8/208830 [patent_app_country] => US [patent_app_date] => 1994-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1066 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/438/05438821.pdf [firstpage_image] =>[orig_patent_app_number] => 208830 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/208830
Method and appliance for influencing the wake of combustion chamber inserts Mar 10, 1994 Issued
Array ( [id] => 3462872 [patent_doc_number] => 05398496 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-03-21 [patent_title] => 'Gas turbine engines' [patent_app_type] => 1 [patent_app_number] => 8/207614 [patent_app_country] => US [patent_app_date] => 1994-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 2923 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/398/05398496.pdf [firstpage_image] =>[orig_patent_app_number] => 207614 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/207614
Gas turbine engines Mar 8, 1994 Issued
Array ( [id] => 3503445 [patent_doc_number] => 05528904 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-06-25 [patent_title] => 'Coated hot gas duct liner' [patent_app_type] => 1 [patent_app_number] => 8/203166 [patent_app_country] => US [patent_app_date] => 1994-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 2232 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/528/05528904.pdf [firstpage_image] =>[orig_patent_app_number] => 203166 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/203166
Coated hot gas duct liner Feb 27, 1994 Issued
Array ( [id] => 3435701 [patent_doc_number] => 05397144 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-03-14 [patent_title] => 'Bicycle operated air pump' [patent_app_type] => 1 [patent_app_number] => 8/169424 [patent_app_country] => US [patent_app_date] => 1994-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 19 [patent_no_of_words] => 14924 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 278 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/397/05397144.pdf [firstpage_image] =>[orig_patent_app_number] => 169424 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/169424
Bicycle operated air pump Feb 27, 1994 Issued
Array ( [id] => 3439973 [patent_doc_number] => 05400587 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-03-28 [patent_title] => 'Gas turbine annular combustion chamber having radially displaced groups of oppositely swirling burners.' [patent_app_type] => 1 [patent_app_number] => 8/202687 [patent_app_country] => US [patent_app_date] => 1994-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 2954 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/400/05400587.pdf [firstpage_image] =>[orig_patent_app_number] => 202687 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/202687
Gas turbine annular combustion chamber having radially displaced groups of oppositely swirling burners. Feb 24, 1994 Issued
Array ( [id] => 3412217 [patent_doc_number] => 05461865 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-10-31 [patent_title] => 'Tangential entry fuel nozzle' [patent_app_type] => 1 [patent_app_number] => 8/201310 [patent_app_country] => US [patent_app_date] => 1994-02-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 1594 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/461/05461865.pdf [firstpage_image] =>[orig_patent_app_number] => 201310 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/201310
Tangential entry fuel nozzle Feb 23, 1994 Issued
Array ( [id] => 3538985 [patent_doc_number] => 05491967 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-02-20 [patent_title] => 'Pressurized fluidized bed reactor and a method of operating the same' [patent_app_type] => 1 [patent_app_number] => 8/200327 [patent_app_country] => US [patent_app_date] => 1994-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 3649 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/491/05491967.pdf [firstpage_image] =>[orig_patent_app_number] => 200327 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/200327
Pressurized fluidized bed reactor and a method of operating the same Feb 22, 1994 Issued
Array ( [id] => 2985043 [patent_doc_number] => 05353587 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-10-11 [patent_title] => 'Film cooling starter geometry for combustor lines' [patent_app_type] => 1 [patent_app_number] => 8/221972 [patent_app_country] => US [patent_app_date] => 1994-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 14 [patent_no_of_words] => 3568 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 281 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/353/05353587.pdf [firstpage_image] =>[orig_patent_app_number] => 221972 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/221972
Film cooling starter geometry for combustor lines Feb 15, 1994 Issued
Array ( [id] => 3093538 [patent_doc_number] => 05408830 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-04-25 [patent_title] => 'Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines' [patent_app_type] => 1 [patent_app_number] => 8/194554 [patent_app_country] => US [patent_app_date] => 1994-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3556 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/408/05408830.pdf [firstpage_image] =>[orig_patent_app_number] => 194554 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/194554
Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines Feb 9, 1994 Issued
08/192528 BLANCHING RESISTANT COATING FOR COPPER ALLOY ROCKET ENGINE MAIN CHAMBER LINING Feb 6, 1994 Abandoned
Array ( [id] => 3412067 [patent_doc_number] => 05461855 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-10-31 [patent_title] => 'Method and device for controlling combustors for gasturbine' [patent_app_type] => 1 [patent_app_number] => 8/193354 [patent_app_country] => US [patent_app_date] => 1994-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 3010 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/461/05461855.pdf [firstpage_image] =>[orig_patent_app_number] => 193354 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/193354
Method and device for controlling combustors for gasturbine Feb 2, 1994 Issued
Array ( [id] => 3523935 [patent_doc_number] => 05479774 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-01-02 [patent_title] => 'Combustion chamber assembly in a gas turbine engine' [patent_app_type] => 1 [patent_app_number] => 8/137129 [patent_app_country] => US [patent_app_date] => 1994-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1393 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 165 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/479/05479774.pdf [firstpage_image] =>[orig_patent_app_number] => 137129 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/137129
Combustion chamber assembly in a gas turbine engine Jan 23, 1994 Issued
Array ( [id] => 3430003 [patent_doc_number] => 05419118 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-05-30 [patent_title] => 'Multi-stage rocket motors' [patent_app_type] => 1 [patent_app_number] => 8/183726 [patent_app_country] => US [patent_app_date] => 1994-01-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 2421 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 205 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/419/05419118.pdf [firstpage_image] =>[orig_patent_app_number] => 183726 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/183726
Multi-stage rocket motors Jan 18, 1994 Issued
08/181702 REFRIGERANT COMPRESSOR AND MOTOR Jan 13, 1994 Abandoned
Array ( [id] => 3404466 [patent_doc_number] => 05452574 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-09-26 [patent_title] => 'Gas turbine engine catalytic and primary combustor arrangement having selective air flow control' [patent_app_type] => 1 [patent_app_number] => 8/181516 [patent_app_country] => US [patent_app_date] => 1994-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3356 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 189 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/452/05452574.pdf [firstpage_image] =>[orig_patent_app_number] => 181516 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/181516
Gas turbine engine catalytic and primary combustor arrangement having selective air flow control Jan 13, 1994 Issued
Menu