
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] => 2489947
[patent_doc_number] => 04817379
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1989-04-04
[patent_title] => 'Jet propulsion engine and method'
[patent_app_type] => 1
[patent_app_number] => 7/007363
[patent_app_country] => US
[patent_app_date] => 1987-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 5
[patent_no_of_words] => 3482
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 288
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/817/04817379.pdf
[firstpage_image] =>[orig_patent_app_number] => 007363
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/007363 | Jet propulsion engine and method | Jan 26, 1987 | Issued |
Array
(
[id] => 2450445
[patent_doc_number] => 04759997
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-07-26
[patent_title] => 'Air supply apparatus for fuel cell system'
[patent_app_type] => 1
[patent_app_number] => 7/006426
[patent_app_country] => US
[patent_app_date] => 1987-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2315
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/759/04759997.pdf
[firstpage_image] =>[orig_patent_app_number] => 006426
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/006426 | Air supply apparatus for fuel cell system | Jan 22, 1987 | Issued |
Array
(
[id] => 2530936
[patent_doc_number] => 04813226
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1989-03-21
[patent_title] => 'Demand control of variable geometry gas turbine power plant'
[patent_app_type] => 1
[patent_app_number] => 7/002070
[patent_app_country] => US
[patent_app_date] => 1987-01-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2638
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 98
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/813/04813226.pdf
[firstpage_image] =>[orig_patent_app_number] => 002070
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/002070 | Demand control of variable geometry gas turbine power plant | Jan 11, 1987 | Issued |
Array
(
[id] => 2534078
[patent_doc_number] => 04815277
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1989-03-28
[patent_title] => 'Integrated power unit'
[patent_app_type] => 1
[patent_app_number] => 7/001818
[patent_app_country] => US
[patent_app_date] => 1987-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 3642
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/815/04815277.pdf
[firstpage_image] =>[orig_patent_app_number] => 001818
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/001818 | Integrated power unit | Jan 7, 1987 | Issued |
Array
(
[id] => 2427563
[patent_doc_number] => 04748805
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-06-07
[patent_title] => 'Gas turbine exhaust device including a jet diffuser'
[patent_app_type] => 1
[patent_app_number] => 7/000807
[patent_app_country] => US
[patent_app_date] => 1987-01-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1014
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/748/04748805.pdf
[firstpage_image] =>[orig_patent_app_number] => 000807
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/000807 | Gas turbine exhaust device including a jet diffuser | Jan 5, 1987 | Issued |
Array
(
[id] => 2433867
[patent_doc_number] => 04731990
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-03-22
[patent_title] => 'Internal combustion engine system and method with reduced noxious emissions'
[patent_app_type] => 1
[patent_app_number] => 6/948033
[patent_app_country] => US
[patent_app_date] => 1986-12-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4672
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/731/04731990.pdf
[firstpage_image] =>[orig_patent_app_number] => 948033
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/948033 | Internal combustion engine system and method with reduced noxious emissions | Dec 30, 1986 | Issued |
Array
(
[id] => 2433828
[patent_doc_number] => 04731988
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-03-22
[patent_title] => 'Internal combustion engine system and method with reduced noxious emissions'
[patent_app_type] => 1
[patent_app_number] => 6/948250
[patent_app_country] => US
[patent_app_date] => 1986-12-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4673
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/731/04731988.pdf
[firstpage_image] =>[orig_patent_app_number] => 948250
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/948250 | Internal combustion engine system and method with reduced noxious emissions | Dec 30, 1986 | Issued |
Array
(
[id] => 2437199
[patent_doc_number] => 04783957
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-11-15
[patent_title] => 'Fuel control circuit for a turbine engine'
[patent_app_type] => 1
[patent_app_number] => 6/946455
[patent_app_country] => US
[patent_app_date] => 1986-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 8335
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/783/04783957.pdf
[firstpage_image] =>[orig_patent_app_number] => 946455
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/946455 | Fuel control circuit for a turbine engine | Dec 22, 1986 | Issued |
Array
(
[id] => 2471197
[patent_doc_number] => 04822249
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1989-04-18
[patent_title] => 'Axial flow blade wheel of a gas or steam driven turbine'
[patent_app_type] => 1
[patent_app_number] => 6/946449
[patent_app_country] => US
[patent_app_date] => 1986-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 13
[patent_no_of_words] => 3417
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 292
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/822/04822249.pdf
[firstpage_image] =>[orig_patent_app_number] => 946449
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/946449 | Axial flow blade wheel of a gas or steam driven turbine | Dec 22, 1986 | Issued |
Array
(
[id] => 2401923
[patent_doc_number] => 04747262
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-05-31
[patent_title] => 'Compressor power unit fuel flow control'
[patent_app_type] => 1
[patent_app_number] => 6/945940
[patent_app_country] => US
[patent_app_date] => 1986-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1507
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/747/04747262.pdf
[firstpage_image] =>[orig_patent_app_number] => 945940
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/945940 | Compressor power unit fuel flow control | Dec 21, 1986 | Issued |
Array
(
[id] => 2470719
[patent_doc_number] => 04800717
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1989-01-31
[patent_title] => 'Turbine rotor cooling'
[patent_app_type] => 1
[patent_app_number] => 6/944761
[patent_app_country] => US
[patent_app_date] => 1986-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 1499
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/800/04800717.pdf
[firstpage_image] =>[orig_patent_app_number] => 944761
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/944761 | Turbine rotor cooling | Dec 21, 1986 | Issued |
Array
(
[id] => 2370075
[patent_doc_number] => 04719750
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-01-19
[patent_title] => 'Installation for the control of the fuel supply to the afterburner of a bypass gas turbine jet propulsion unit'
[patent_app_type] => 1
[patent_app_number] => 6/940419
[patent_app_country] => US
[patent_app_date] => 1986-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 5380
[patent_no_of_claims] => 18
[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/04/719/04719750.pdf
[firstpage_image] =>[orig_patent_app_number] => 940419
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/940419 | Installation for the control of the fuel supply to the afterburner of a bypass gas turbine jet propulsion unit | Dec 10, 1986 | Issued |
Array
(
[id] => 2427426
[patent_doc_number] => 04756152
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-07-12
[patent_title] => 'Control for bleed modulation during engine deceleration'
[patent_app_type] => 1
[patent_app_number] => 6/939214
[patent_app_country] => US
[patent_app_date] => 1986-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2020
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/756/04756152.pdf
[firstpage_image] =>[orig_patent_app_number] => 939214
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/939214 | Control for bleed modulation during engine deceleration | Dec 7, 1986 | Issued |
Array
(
[id] => 2434717
[patent_doc_number] => 04765133
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-08-23
[patent_title] => 'Fuel control with smooth mode transition'
[patent_app_type] => 1
[patent_app_number] => 6/939217
[patent_app_country] => US
[patent_app_date] => 1986-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3568
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 283
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/765/04765133.pdf
[firstpage_image] =>[orig_patent_app_number] => 939217
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/939217 | Fuel control with smooth mode transition | Dec 7, 1986 | Issued |
Array
(
[id] => 2403819
[patent_doc_number] => 04773213
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-09-27
[patent_title] => 'Engine control with smooth transition to synthesized parameter'
[patent_app_type] => 1
[patent_app_number] => 6/939215
[patent_app_country] => US
[patent_app_date] => 1986-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3356
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/773/04773213.pdf
[firstpage_image] =>[orig_patent_app_number] => 939215
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/939215 | Engine control with smooth transition to synthesized parameter | Dec 7, 1986 | Issued |
Array
(
[id] => 2427546
[patent_doc_number] => 04748804
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-06-07
[patent_title] => 'Inlet total temperature synthesis for gas turbine engines'
[patent_app_type] => 1
[patent_app_number] => 6/939218
[patent_app_country] => US
[patent_app_date] => 1986-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2172
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/748/04748804.pdf
[firstpage_image] =>[orig_patent_app_number] => 939218
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/939218 | Inlet total temperature synthesis for gas turbine engines | Dec 7, 1986 | Issued |
| 06/937827 | FUEL INJECTION SYSTEM FOR RAMJET ENGINE, RAMJET ENGINE EQUIPPED WITH SUCH AN INJECTION SYSTEM AND MISSILE PROPELLED BY THIS RAMJET ENGINE | Dec 3, 1986 | Abandoned |
Array
(
[id] => 2367931
[patent_doc_number] => 04736582
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-04-12
[patent_title] => 'Gas turbine engine fuel control system'
[patent_app_type] => 1
[patent_app_number] => 6/934994
[patent_app_country] => US
[patent_app_date] => 1986-11-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1499
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/736/04736582.pdf
[firstpage_image] =>[orig_patent_app_number] => 934994
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/934994 | Gas turbine engine fuel control system | Nov 25, 1986 | Issued |
Array
(
[id] => 2303705
[patent_doc_number] => 04685288
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1987-08-11
[patent_title] => 'Apparatus for removing noncondensable gases from cogenerated process steam in dual fluid Cheng cycle engines'
[patent_app_type] => 1
[patent_app_number] => 6/933101
[patent_app_country] => US
[patent_app_date] => 1986-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1404
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 251
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/685/04685288.pdf
[firstpage_image] =>[orig_patent_app_number] => 933101
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/933101 | Apparatus for removing noncondensable gases from cogenerated process steam in dual fluid Cheng cycle engines | Nov 19, 1986 | Issued |
Array
(
[id] => 2436544
[patent_doc_number] => 04722180
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1988-02-02
[patent_title] => 'Method and means for enhancing recovery of a surge condition in a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 6/932960
[patent_app_country] => US
[patent_app_date] => 1986-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2699
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/722/04722180.pdf
[firstpage_image] =>[orig_patent_app_number] => 932960
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/932960 | Method and means for enhancing recovery of a surge condition in a gas turbine engine | Nov 19, 1986 | Issued |