
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 |
|---|---|---|---|
| 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 |