
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] => 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 |