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] => 3569044 [patent_doc_number] => 05490376 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-02-13 [patent_title] => 'Gas turbine system' [patent_app_type] => 1 [patent_app_number] => 8/263913 [patent_app_country] => US [patent_app_date] => 1994-06-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 1686 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/490/05490376.pdf [firstpage_image] =>[orig_patent_app_number] => 263913 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/263913
Gas turbine system Jun 21, 1994 Issued
Array ( [id] => 3397029 [patent_doc_number] => 05437159 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-08-01 [patent_title] => 'Fuel injection system for a gas turbine combustor including radial fuel spray arms and V-gutter flameholders' [patent_app_type] => 1 [patent_app_number] => 8/260727 [patent_app_country] => US [patent_app_date] => 1994-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 2563 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 277 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/437/05437159.pdf [firstpage_image] =>[orig_patent_app_number] => 260727 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/260727
Fuel injection system for a gas turbine combustor including radial fuel spray arms and V-gutter flameholders Jun 14, 1994 Issued
Array ( [id] => 3409872 [patent_doc_number] => 05415000 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-05-16 [patent_title] => 'Low NOx combustor retro-fit system for gas turbines' [patent_app_type] => 1 [patent_app_number] => 8/259106 [patent_app_country] => US [patent_app_date] => 1994-06-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2410 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/415/05415000.pdf [firstpage_image] =>[orig_patent_app_number] => 259106 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/259106
Low NOx combustor retro-fit system for gas turbines Jun 12, 1994 Issued
Array ( [id] => 3539025 [patent_doc_number] => 05491970 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-02-20 [patent_title] => 'Method for staging fuel in a turbine between diffusion and premixed operations' [patent_app_type] => 1 [patent_app_number] => 8/258112 [patent_app_country] => US [patent_app_date] => 1994-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4258 [patent_no_of_claims] => 16 [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] => patents/05/491/05491970.pdf [firstpage_image] =>[orig_patent_app_number] => 258112 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/258112
Method for staging fuel in a turbine between diffusion and premixed operations Jun 9, 1994 Issued
08/258041 METHOD FOR STAGING FUEL IN A TURBINE IN THE PREMIXED OPERATING MODE Jun 9, 1994 Abandoned
Array ( [id] => 3085432 [patent_doc_number] => 05417069 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-05-23 [patent_title] => 'Separator for an annular gas turbine combustion chamber' [patent_app_type] => 1 [patent_app_number] => 8/253912 [patent_app_country] => US [patent_app_date] => 1994-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 2929 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 223 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/417/05417069.pdf [firstpage_image] =>[orig_patent_app_number] => 253912 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/253912
Separator for an annular gas turbine combustion chamber Jun 2, 1994 Issued
Array ( [id] => 3712890 [patent_doc_number] => 05664415 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-09-09 [patent_title] => 'After-burning turbo-fan engine with a fixed geometry exhaust nozzle having a variable flow coefficient' [patent_app_type] => 1 [patent_app_number] => 8/252191 [patent_app_country] => US [patent_app_date] => 1994-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 4996 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/664/05664415.pdf [firstpage_image] =>[orig_patent_app_number] => 252191 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/252191
After-burning turbo-fan engine with a fixed geometry exhaust nozzle having a variable flow coefficient May 31, 1994 Issued
Array ( [id] => 3430029 [patent_doc_number] => 05419120 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-05-30 [patent_title] => 'Device for purging combustion residues' [patent_app_type] => 1 [patent_app_number] => 8/251980 [patent_app_country] => US [patent_app_date] => 1994-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2440 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/419/05419120.pdf [firstpage_image] =>[orig_patent_app_number] => 251980 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/251980
Device for purging combustion residues May 31, 1994 Issued
Array ( [id] => 3395356 [patent_doc_number] => 05460002 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-10-24 [patent_title] => 'Catalytically-and aerodynamically-assisted liner for gas turbine combustors' [patent_app_type] => 1 [patent_app_number] => 8/250633 [patent_app_country] => US [patent_app_date] => 1994-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1666 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/460/05460002.pdf [firstpage_image] =>[orig_patent_app_number] => 250633 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/250633
Catalytically-and aerodynamically-assisted liner for gas turbine combustors May 26, 1994 Issued
Array ( [id] => 3573581 [patent_doc_number] => 05566544 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-10-22 [patent_title] => 'Rocket preburner injector with tailored gas temperature profile' [patent_app_type] => 1 [patent_app_number] => 8/250243 [patent_app_country] => US [patent_app_date] => 1994-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2304 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 284 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/566/05566544.pdf [firstpage_image] =>[orig_patent_app_number] => 250243 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/250243
Rocket preburner injector with tailored gas temperature profile May 26, 1994 Issued
Array ( [id] => 3432142 [patent_doc_number] => 05423174 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-06-13 [patent_title] => 'Anti-icing system for a gas turbine engine' [patent_app_type] => 1 [patent_app_number] => 8/249728 [patent_app_country] => US [patent_app_date] => 1994-05-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 1919 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 296 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/423/05423174.pdf [firstpage_image] =>[orig_patent_app_number] => 249728 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/249728
Anti-icing system for a gas turbine engine May 25, 1994 Issued
Array ( [id] => 3471314 [patent_doc_number] => 05473882 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-12-12 [patent_title] => 'Combustion apparatus for a gas turbine having separate combustion and vaporization zones' [patent_app_type] => 1 [patent_app_number] => 8/249284 [patent_app_country] => US [patent_app_date] => 1994-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2383 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/473/05473882.pdf [firstpage_image] =>[orig_patent_app_number] => 249284 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/249284
Combustion apparatus for a gas turbine having separate combustion and vaporization zones May 24, 1994 Issued
Array ( [id] => 3511565 [patent_doc_number] => 05488829 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-02-06 [patent_title] => 'Method and apparatus for reducing noise generated by combustion' [patent_app_type] => 1 [patent_app_number] => 8/248706 [patent_app_country] => US [patent_app_date] => 1994-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3148 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/488/05488829.pdf [firstpage_image] =>[orig_patent_app_number] => 248706 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/248706
Method and apparatus for reducing noise generated by combustion May 24, 1994 Issued
Array ( [id] => 3643516 [patent_doc_number] => 05622041 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-04-22 [patent_title] => 'Catalytic combustion system including a separator body' [patent_app_type] => 1 [patent_app_number] => 8/249913 [patent_app_country] => US [patent_app_date] => 1994-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 28 [patent_no_of_words] => 7676 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/622/05622041.pdf [firstpage_image] =>[orig_patent_app_number] => 249913 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/249913
Catalytic combustion system including a separator body May 24, 1994 Issued
Array ( [id] => 3631012 [patent_doc_number] => 05636510 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-06-10 [patent_title] => 'Gas turbine topping combustor' [patent_app_type] => 1 [patent_app_number] => 8/248742 [patent_app_country] => US [patent_app_date] => 1994-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 14 [patent_no_of_words] => 5354 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 206 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/636/05636510.pdf [firstpage_image] =>[orig_patent_app_number] => 248742 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/248742
Gas turbine topping combustor May 24, 1994 Issued
Array ( [id] => 3440999 [patent_doc_number] => 05450720 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-09-19 [patent_title] => 'Rocket engine nozzle having a notched diverging portion' [patent_app_type] => 1 [patent_app_number] => 8/249140 [patent_app_country] => US [patent_app_date] => 1994-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 3685 [patent_no_of_claims] => 12 [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/05/450/05450720.pdf [firstpage_image] =>[orig_patent_app_number] => 249140 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/249140
Rocket engine nozzle having a notched diverging portion May 24, 1994 Issued
Array ( [id] => 3507630 [patent_doc_number] => 05526640 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-06-18 [patent_title] => 'Gas turbine engine including a bearing support tube cantilevered from a turbine nozzle wall' [patent_app_type] => 1 [patent_app_number] => 8/243183 [patent_app_country] => US [patent_app_date] => 1994-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 14 [patent_no_of_words] => 4669 [patent_no_of_claims] => 59 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/526/05526640.pdf [firstpage_image] =>[orig_patent_app_number] => 243183 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/243183
Gas turbine engine including a bearing support tube cantilevered from a turbine nozzle wall May 15, 1994 Issued
Array ( [id] => 3397014 [patent_doc_number] => 05437158 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-08-01 [patent_title] => 'Low-emission combustor having perforated plate for lean direct injection' [patent_app_type] => 1 [patent_app_number] => 8/243609 [patent_app_country] => US [patent_app_date] => 1994-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2120 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/437/05437158.pdf [firstpage_image] =>[orig_patent_app_number] => 243609 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/243609
Low-emission combustor having perforated plate for lean direct injection May 15, 1994 Issued
08/242762 DISPOSABLE FLUID INFUSION PUMPING CHAMBER CASSETTE HAVING A PUSH BUTTON FLOW STOP THEREON May 12, 1994 Abandoned
Array ( [id] => 3462901 [patent_doc_number] => 05398498 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1995-03-21 [patent_title] => 'Joint construction between components of military projectile and releasable by melting of fusible eutectic helical member' [patent_app_type] => 1 [patent_app_number] => 8/239037 [patent_app_country] => US [patent_app_date] => 1994-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 10 [patent_no_of_words] => 3058 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/398/05398498.pdf [firstpage_image] =>[orig_patent_app_number] => 239037 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/239037
Joint construction between components of military projectile and releasable by melting of fusible eutectic helical member May 5, 1994 Issued
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