
Alicia L. Otton
Examiner (ID: 2346, Phone: (571)270-7683 , Office: P/1626 )
| Most Active Art Unit | 1626 |
| Art Unit(s) | 1699, 1626, 4121 |
| Total Applications | 1587 |
| Issued Applications | 977 |
| Pending Applications | 102 |
| Abandoned Applications | 543 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2803407
[patent_doc_number] => 05115637
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-26
[patent_title] => 'External cartridge gas combustor ignitor'
[patent_app_type] => 1
[patent_app_number] => 7/455270
[patent_app_country] => US
[patent_app_date] => 1989-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2274
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 159
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/115/05115637.pdf
[firstpage_image] =>[orig_patent_app_number] => 455270
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/455270 | External cartridge gas combustor ignitor | Dec 21, 1989 | Issued |
Array
(
[id] => 2832186
[patent_doc_number] => 05111655
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-12
[patent_title] => 'Single wall combustor assembly'
[patent_app_type] => 1
[patent_app_number] => 7/455245
[patent_app_country] => US
[patent_app_date] => 1989-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2290
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 283
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/111/05111655.pdf
[firstpage_image] =>[orig_patent_app_number] => 455245
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/455245 | Single wall combustor assembly | Dec 21, 1989 | Issued |
Array
(
[id] => 2815001
[patent_doc_number] => 05119636
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-06-09
[patent_title] => 'Fuel injector for a turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/455509
[patent_app_country] => US
[patent_app_date] => 1989-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3983
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 175
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/119/05119636.pdf
[firstpage_image] =>[orig_patent_app_number] => 455509
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/455509 | Fuel injector for a turbine engine | Dec 20, 1989 | Issued |
Array
(
[id] => 2653738
[patent_doc_number] => 05072578
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-17
[patent_title] => 'Acceleration override means for a fuel control'
[patent_app_type] => 1
[patent_app_number] => 7/450797
[patent_app_country] => US
[patent_app_date] => 1989-12-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 4003
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 464
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/072/05072578.pdf
[firstpage_image] =>[orig_patent_app_number] => 450797
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/450797 | Acceleration override means for a fuel control | Dec 13, 1989 | Issued |
Array
(
[id] => 2806554
[patent_doc_number] => 05097659
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-24
[patent_title] => 'Airframe power unit using stored air and jet fuel'
[patent_app_type] => 1
[patent_app_number] => 7/450671
[patent_app_country] => US
[patent_app_date] => 1989-12-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4533
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 213
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/097/05097659.pdf
[firstpage_image] =>[orig_patent_app_number] => 450671
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/450671 | Airframe power unit using stored air and jet fuel | Dec 13, 1989 | Issued |
Array
(
[id] => 2913471
[patent_doc_number] => 05245820
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-09-21
[patent_title] => 'Air turbine starter with passive hydraulic capacitor'
[patent_app_type] => 1
[patent_app_number] => 7/450640
[patent_app_country] => US
[patent_app_date] => 1989-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2140
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 83
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/245/05245820.pdf
[firstpage_image] =>[orig_patent_app_number] => 450640
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/450640 | Air turbine starter with passive hydraulic capacitor | Dec 12, 1989 | Issued |
Array
(
[id] => 2834901
[patent_doc_number] => 05133182
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-28
[patent_title] => 'Control of low compressor vanes and fuel for a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/448391
[patent_app_country] => US
[patent_app_date] => 1989-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3504
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 282
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/133/05133182.pdf
[firstpage_image] =>[orig_patent_app_number] => 448391
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/448391 | Control of low compressor vanes and fuel for a gas turbine engine | Dec 10, 1989 | Issued |
Array
(
[id] => 2821151
[patent_doc_number] => 05136838
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-08-11
[patent_title] => 'Stored energy, wide energy range turbine starting system'
[patent_app_type] => 1
[patent_app_number] => 7/447444
[patent_app_country] => US
[patent_app_date] => 1989-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 3567
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 177
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/136/05136838.pdf
[firstpage_image] =>[orig_patent_app_number] => 447444
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/447444 | Stored energy, wide energy range turbine starting system | Dec 6, 1989 | Issued |
Array
(
[id] => 2726097
[patent_doc_number] => 05029439
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-09
[patent_title] => 'Gas turbine engine including a turbine braking device'
[patent_app_type] => 1
[patent_app_number] => 7/447407
[patent_app_country] => US
[patent_app_date] => 1989-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1309
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/029/05029439.pdf
[firstpage_image] =>[orig_patent_app_number] => 447407
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/447407 | Gas turbine engine including a turbine braking device | Dec 6, 1989 | Issued |
Array
(
[id] => 3078019
[patent_doc_number] => 05313779
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-05-24
[patent_title] => 'Surge protected gas turbine engine for providing variable bleed air flow'
[patent_app_type] => 1
[patent_app_number] => 7/447179
[patent_app_country] => US
[patent_app_date] => 1989-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2168
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 219
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/313/05313779.pdf
[firstpage_image] =>[orig_patent_app_number] => 447179
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/447179 | Surge protected gas turbine engine for providing variable bleed air flow | Dec 6, 1989 | Issued |
Array
(
[id] => 2797336
[patent_doc_number] => 05121596
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-06-16
[patent_title] => 'Method of starting gas turbine'
[patent_app_type] => 1
[patent_app_number] => 7/446317
[patent_app_country] => US
[patent_app_date] => 1989-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 14
[patent_no_of_words] => 4129
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/121/05121596.pdf
[firstpage_image] =>[orig_patent_app_number] => 446317
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/446317 | Method of starting gas turbine | Dec 4, 1989 | Issued |
Array
(
[id] => 2680751
[patent_doc_number] => 04987735
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-01-29
[patent_title] => 'Heat and power supply system'
[patent_app_type] => 1
[patent_app_number] => 7/445520
[patent_app_country] => US
[patent_app_date] => 1989-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2530
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 243
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/987/04987735.pdf
[firstpage_image] =>[orig_patent_app_number] => 445520
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/445520 | Heat and power supply system | Dec 3, 1989 | Issued |
Array
(
[id] => 2711093
[patent_doc_number] => 05031398
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-16
[patent_title] => 'Direct controlled control valve with an offset of a digital to analog converter'
[patent_app_type] => 1
[patent_app_number] => 7/443159
[patent_app_country] => US
[patent_app_date] => 1989-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 3227
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/031/05031398.pdf
[firstpage_image] =>[orig_patent_app_number] => 443159
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/443159 | Direct controlled control valve with an offset of a digital to analog converter | Nov 29, 1989 | Issued |
Array
(
[id] => 2825898
[patent_doc_number] => 05103629
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-14
[patent_title] => 'Gas turbine control system having optimized ignition air flow control'
[patent_app_type] => 1
[patent_app_number] => 7/439112
[patent_app_country] => US
[patent_app_date] => 1989-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 13
[patent_no_of_words] => 8638
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/103/05103629.pdf
[firstpage_image] =>[orig_patent_app_number] => 439112
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/439112 | Gas turbine control system having optimized ignition air flow control | Nov 19, 1989 | Issued |
Array
(
[id] => 2602124
[patent_doc_number] => 04955190
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-09-11
[patent_title] => 'Method for driving a gas turbine utilizing a hexagonal pressurized fluidized bed reactor'
[patent_app_type] => 1
[patent_app_number] => 7/437056
[patent_app_country] => US
[patent_app_date] => 1989-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 4378
[patent_no_of_claims] => 5
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/955/04955190.pdf
[firstpage_image] =>[orig_patent_app_number] => 437056
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/437056 | Method for driving a gas turbine utilizing a hexagonal pressurized fluidized bed reactor | Nov 13, 1989 | Issued |
Array
(
[id] => 2829350
[patent_doc_number] => 05088276
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-02-18
[patent_title] => 'Turbo-compressor engine'
[patent_app_type] => 1
[patent_app_number] => 7/434316
[patent_app_country] => US
[patent_app_date] => 1989-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1493
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 212
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/088/05088276.pdf
[firstpage_image] =>[orig_patent_app_number] => 434316
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/434316 | Turbo-compressor engine | Nov 12, 1989 | Issued |
Array
(
[id] => 2734573
[patent_doc_number] => 05042246
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-08-27
[patent_title] => 'Control system for single shaft combined cycle gas and steam turbine unit'
[patent_app_type] => 1
[patent_app_number] => 7/431892
[patent_app_country] => US
[patent_app_date] => 1989-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 6750
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 210
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/042/05042246.pdf
[firstpage_image] =>[orig_patent_app_number] => 431892
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/431892 | Control system for single shaft combined cycle gas and steam turbine unit | Nov 5, 1989 | Issued |
Array
(
[id] => 2716087
[patent_doc_number] => 04996836
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-03-05
[patent_title] => 'Combined gas and steam turbine process'
[patent_app_type] => 1
[patent_app_number] => 7/423669
[patent_app_country] => US
[patent_app_date] => 1989-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/996/04996836.pdf
[firstpage_image] =>[orig_patent_app_number] => 423669
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/423669 | Combined gas and steam turbine process | Oct 17, 1989 | Issued |
Array
(
[id] => 2648139
[patent_doc_number] => 05046307
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-09-10
[patent_title] => 'Thrust reverser for high bypass turbofan engine'
[patent_app_type] => 1
[patent_app_number] => 7/422717
[patent_app_country] => US
[patent_app_date] => 1989-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/046/05046307.pdf
[firstpage_image] =>[orig_patent_app_number] => 422717
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/422717 | Thrust reverser for high bypass turbofan engine | Oct 16, 1989 | Issued |
Array
(
[id] => 2684579
[patent_doc_number] => 04999991
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-03-19
[patent_title] => 'Synthesized feedback for gas turbine clearance control'
[patent_app_type] => 1
[patent_app_number] => 7/420199
[patent_app_country] => US
[patent_app_date] => 1989-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/999/04999991.pdf
[firstpage_image] =>[orig_patent_app_number] => 420199
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/420199 | Synthesized feedback for gas turbine clearance control | Oct 11, 1989 | Issued |