
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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 |