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
Array ( [id] => 2964214 [patent_doc_number] => 05265409 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-11-30 [patent_title] => 'Uniform cooling film replenishment thermal liner assembly' [patent_app_type] => 1 [patent_app_number] => 7/995406 [patent_app_country] => US [patent_app_date] => 1992-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2685 [patent_no_of_claims] => 11 [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] => patents/05/265/05265409.pdf [firstpage_image] =>[orig_patent_app_number] => 995406 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/995406
Uniform cooling film replenishment thermal liner assembly Dec 17, 1992 Issued
Array ( [id] => 3067173 [patent_doc_number] => 05279126 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-01-18 [patent_title] => 'Diffuser-combustor' [patent_app_type] => 1 [patent_app_number] => 7/995405 [patent_app_country] => US [patent_app_date] => 1992-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1016 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/279/05279126.pdf [firstpage_image] =>[orig_patent_app_number] => 995405 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/995405
Diffuser-combustor Dec 17, 1992 Issued
Array ( [id] => 3581633 [patent_doc_number] => 05487275 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-01-30 [patent_title] => 'Tertiary fuel injection system for use in a dry low NOx combustion system' [patent_app_type] => 1 [patent_app_number] => 7/987957 [patent_app_country] => US [patent_app_date] => 1992-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2778 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/487/05487275.pdf [firstpage_image] =>[orig_patent_app_number] => 987957 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/987957
Tertiary fuel injection system for use in a dry low NOx combustion system Dec 10, 1992 Issued
Array ( [id] => 2993067 [patent_doc_number] => 05339625 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-08-23 [patent_title] => 'Hybrid rocket motor solid fuel grain' [patent_app_type] => 1 [patent_app_number] => 7/986087 [patent_app_country] => US [patent_app_date] => 1992-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2977 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/339/05339625.pdf [firstpage_image] =>[orig_patent_app_number] => 986087 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/986087
Hybrid rocket motor solid fuel grain Dec 3, 1992 Issued
Array ( [id] => 3027556 [patent_doc_number] => 05303554 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-04-19 [patent_title] => 'Low NOx injector with central air swirling and angled fuel inlets' [patent_app_type] => 1 [patent_app_number] => 7/983062 [patent_app_country] => US [patent_app_date] => 1992-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2644 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 176 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/303/05303554.pdf [firstpage_image] =>[orig_patent_app_number] => 983062 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/983062
Low NOx injector with central air swirling and angled fuel inlets Nov 26, 1992 Issued
Array ( [id] => 3071698 [patent_doc_number] => 05311742 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-05-17 [patent_title] => 'Gas turbine combustor with nozzle pressure ratio control' [patent_app_type] => 1 [patent_app_number] => 7/982583 [patent_app_country] => US [patent_app_date] => 1992-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4411 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 302 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/311/05311742.pdf [firstpage_image] =>[orig_patent_app_number] => 982583 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/982583
Gas turbine combustor with nozzle pressure ratio control Nov 26, 1992 Issued
Array ( [id] => 3049099 [patent_doc_number] => 05335502 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-08-09 [patent_title] => 'Arched combustor' [patent_app_type] => 1 [patent_app_number] => 7/982359 [patent_app_country] => US [patent_app_date] => 1992-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4500 [patent_no_of_claims] => 10 [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/05/335/05335502.pdf [firstpage_image] =>[orig_patent_app_number] => 982359 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/982359
Arched combustor Nov 26, 1992 Issued
Array ( [id] => 3042763 [patent_doc_number] => 05309710 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-05-10 [patent_title] => 'Gas turbine combustor having poppet valves for air distribution control' [patent_app_type] => 1 [patent_app_number] => 7/979657 [patent_app_country] => US [patent_app_date] => 1992-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3182 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 222 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/309/05309710.pdf [firstpage_image] =>[orig_patent_app_number] => 979657 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/979657
Gas turbine combustor having poppet valves for air distribution control Nov 19, 1992 Issued
Array ( [id] => 2867001 [patent_doc_number] => 05267442 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-12-07 [patent_title] => 'Fuel nozzle with eccentric primary circuit orifice' [patent_app_type] => 1 [patent_app_number] => 7/977476 [patent_app_country] => US [patent_app_date] => 1992-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 1768 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/267/05267442.pdf [firstpage_image] =>[orig_patent_app_number] => 977476 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/977476
Fuel nozzle with eccentric primary circuit orifice Nov 16, 1992 Issued
Array ( [id] => 3028850 [patent_doc_number] => 05323604 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-06-28 [patent_title] => 'Triple annular combustor for gas turbine engine' [patent_app_type] => 1 [patent_app_number] => 7/976752 [patent_app_country] => US [patent_app_date] => 1992-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 3831 [patent_no_of_claims] => 21 [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] => patents/05/323/05323604.pdf [firstpage_image] =>[orig_patent_app_number] => 976752 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/976752
Triple annular combustor for gas turbine engine Nov 15, 1992 Issued
07/974523 METHOD OF OPERATING AN ANNULAR COMBUSTION CHAMBER Nov 11, 1992 Abandoned
Array ( [id] => 3071903 [patent_doc_number] => 05289686 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-03-01 [patent_title] => 'Low nox gas turbine combustor liner with elliptical apertures for air swirling' [patent_app_type] => 1 [patent_app_number] => 7/974759 [patent_app_country] => US [patent_app_date] => 1992-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 2745 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 270 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/289/05289686.pdf [firstpage_image] =>[orig_patent_app_number] => 974759 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/974759
Low nox gas turbine combustor liner with elliptical apertures for air swirling Nov 11, 1992 Issued
Array ( [id] => 3059476 [patent_doc_number] => 05321947 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-06-21 [patent_title] => 'Lean premix combustion system having reduced combustion pressure oscillation' [patent_app_type] => 1 [patent_app_number] => 7/973895 [patent_app_country] => US [patent_app_date] => 1992-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4801 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 287 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/321/05321947.pdf [firstpage_image] =>[orig_patent_app_number] => 973895 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/973895
Lean premix combustion system having reduced combustion pressure oscillation Nov 9, 1992 Issued
Array ( [id] => 3018768 [patent_doc_number] => 05372008 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-12-13 [patent_title] => 'Lean premix combustor system' [patent_app_type] => 1 [patent_app_number] => 7/973874 [patent_app_country] => US [patent_app_date] => 1992-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4403 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/372/05372008.pdf [firstpage_image] =>[orig_patent_app_number] => 973874 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/973874
Lean premix combustor system Nov 9, 1992 Issued
Array ( [id] => 3073715 [patent_doc_number] => 05297390 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-03-29 [patent_title] => 'Fuel injection nozzle having tip cooling' [patent_app_type] => 1 [patent_app_number] => 7/973892 [patent_app_country] => US [patent_app_date] => 1992-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4410 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 224 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/297/05297390.pdf [firstpage_image] =>[orig_patent_app_number] => 973892 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/973892
Fuel injection nozzle having tip cooling Nov 9, 1992 Issued
Array ( [id] => 2927145 [patent_doc_number] => 05261224 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1993-11-16 [patent_title] => 'High altitude starting two-stage fuel injection apparatus' [patent_app_type] => 1 [patent_app_number] => 7/970101 [patent_app_country] => US [patent_app_date] => 1992-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 3157 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 30 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/261/05261224.pdf [firstpage_image] =>[orig_patent_app_number] => 970101 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/970101
High altitude starting two-stage fuel injection apparatus Nov 1, 1992 Issued
Array ( [id] => 3065709 [patent_doc_number] => 05277022 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-01-11 [patent_title] => 'Air blast fuel injecton system' [patent_app_type] => 1 [patent_app_number] => 7/966903 [patent_app_country] => US [patent_app_date] => 1992-10-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 11 [patent_no_of_words] => 5999 [patent_no_of_claims] => 43 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/277/05277022.pdf [firstpage_image] =>[orig_patent_app_number] => 966903 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/966903
Air blast fuel injecton system Oct 22, 1992 Issued
Array ( [id] => 3029459 [patent_doc_number] => 05305596 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-04-26 [patent_title] => 'Method for preventing lean flaeout at ignition of a stored energy system for driving a turbine wheel' [patent_app_type] => 1 [patent_app_number] => 7/964360 [patent_app_country] => US [patent_app_date] => 1992-10-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 2687 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/305/05305596.pdf [firstpage_image] =>[orig_patent_app_number] => 964360 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/964360
Method for preventing lean flaeout at ignition of a stored energy system for driving a turbine wheel Oct 20, 1992 Issued
Array ( [id] => 3069889 [patent_doc_number] => 05284014 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-02-08 [patent_title] => 'Turbojet-ramjet hypersonic aircraft engine' [patent_app_type] => 1 [patent_app_number] => 7/961319 [patent_app_country] => US [patent_app_date] => 1992-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1743 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/284/05284014.pdf [firstpage_image] =>[orig_patent_app_number] => 961319 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/961319
Turbojet-ramjet hypersonic aircraft engine Oct 14, 1992 Issued
Array ( [id] => 2995905 [patent_doc_number] => 05331816 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1994-07-26 [patent_title] => 'Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles' [patent_app_type] => 1 [patent_app_number] => 7/960158 [patent_app_country] => US [patent_app_date] => 1992-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 3726 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/331/05331816.pdf [firstpage_image] =>[orig_patent_app_number] => 960158 [rel_patent_id] =>[rel_patent_doc_number] =>)
07/960158
Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles Oct 12, 1992 Issued
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