
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 |
|---|---|---|---|
| 07/384901 | FUEL CONTROL SYSTEM FOR GAS TURBINE AEROENGINE OVERSPEED PROTECTION | Jul 24, 1989 | Abandoned |
Array
(
[id] => 2572947
[patent_doc_number] => 04969324
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-11-13
[patent_title] => 'Control method for use with steam injected gas turbine'
[patent_app_type] => 1
[patent_app_number] => 7/383703
[patent_app_country] => US
[patent_app_date] => 1989-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2351
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/969/04969324.pdf
[firstpage_image] =>[orig_patent_app_number] => 383703
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/383703 | Control method for use with steam injected gas turbine | Jul 23, 1989 | Issued |
Array
(
[id] => 2663592
[patent_doc_number] => 05048284
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-09-17
[patent_title] => 'Method of operating gas turbines with reformed fuel'
[patent_app_type] => 1
[patent_app_number] => 7/378070
[patent_app_country] => US
[patent_app_date] => 1989-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 6390
[patent_no_of_claims] => 11
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/048/05048284.pdf
[firstpage_image] =>[orig_patent_app_number] => 378070
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/378070 | Method of operating gas turbines with reformed fuel | Jul 10, 1989 | Issued |
Array
(
[id] => 2663879
[patent_doc_number] => 05048298
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-09-17
[patent_title] => 'Low cost fuel system for a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/377564
[patent_app_country] => US
[patent_app_date] => 1989-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 1659
[patent_no_of_claims] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/048/05048298.pdf
[firstpage_image] =>[orig_patent_app_number] => 377564
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/377564 | Low cost fuel system for a gas turbine engine | Jul 9, 1989 | Issued |
Array
(
[id] => 2723793
[patent_doc_number] => 05027596
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-02
[patent_title] => 'High performance propulsion thruster, especially for attitude and orbit control of a space flight body'
[patent_app_type] => 1
[patent_app_number] => 7/376765
[patent_app_country] => US
[patent_app_date] => 1989-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3720
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[pdf_file] => patents/05/027/05027596.pdf
[firstpage_image] =>[orig_patent_app_number] => 376765
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/376765 | High performance propulsion thruster, especially for attitude and orbit control of a space flight body | Jul 6, 1989 | Issued |
Array
(
[id] => 2642191
[patent_doc_number] => 04961310
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-10-09
[patent_title] => 'Single shaft combined cycle turbine'
[patent_app_type] => 1
[patent_app_number] => 7/374812
[patent_app_country] => US
[patent_app_date] => 1989-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 4783
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/961/04961310.pdf
[firstpage_image] =>[orig_patent_app_number] => 374812
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/374812 | Single shaft combined cycle turbine | Jul 2, 1989 | Issued |
Array
(
[id] => 2685829
[patent_doc_number] => 04991393
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-02-12
[patent_title] => 'Spacecraft guidance and control system'
[patent_app_type] => 1
[patent_app_number] => 7/372239
[patent_app_country] => US
[patent_app_date] => 1989-06-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2926
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/991/04991393.pdf
[firstpage_image] =>[orig_patent_app_number] => 372239
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/372239 | Spacecraft guidance and control system | Jun 25, 1989 | Issued |
Array
(
[id] => 2850200
[patent_doc_number] => 05090193
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-02-25
[patent_title] => 'Active clearance control with cruise mode'
[patent_app_type] => 1
[patent_app_number] => 7/370434
[patent_app_country] => US
[patent_app_date] => 1989-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1990
[patent_no_of_claims] => 2
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[pdf_file] => patents/05/090/05090193.pdf
[firstpage_image] =>[orig_patent_app_number] => 370434
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/370434 | Active clearance control with cruise mode | Jun 22, 1989 | Issued |
Array
(
[id] => 2743983
[patent_doc_number] => 05005352
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-04-09
[patent_title] => 'Clearance control method for gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/372398
[patent_app_country] => US
[patent_app_date] => 1989-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2819
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/005/05005352.pdf
[firstpage_image] =>[orig_patent_app_number] => 372398
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/372398 | Clearance control method for gas turbine engine | Jun 22, 1989 | Issued |
Array
(
[id] => 2662444
[patent_doc_number] => 05003769
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-04-02
[patent_title] => 'Self-checking speed governor arrangement'
[patent_app_type] => 1
[patent_app_number] => 7/370797
[patent_app_country] => US
[patent_app_date] => 1989-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 4928
[patent_no_of_claims] => 14
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/003/05003769.pdf
[firstpage_image] =>[orig_patent_app_number] => 370797
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/370797 | Self-checking speed governor arrangement | Jun 22, 1989 | Issued |
Array
(
[id] => 2727860
[patent_doc_number] => 05020314
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-04
[patent_title] => 'Multiple fluid speed systems'
[patent_app_type] => 1
[patent_app_number] => 7/367613
[patent_app_country] => US
[patent_app_date] => 1989-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 979
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/020/05020314.pdf
[firstpage_image] =>[orig_patent_app_number] => 367613
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/367613 | Multiple fluid speed systems | Jun 18, 1989 | Issued |
Array
(
[id] => 2580434
[patent_doc_number] => 04910956
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-03-27
[patent_title] => 'Gas turbine overtemperature protection'
[patent_app_type] => 1
[patent_app_number] => 7/368135
[patent_app_country] => US
[patent_app_date] => 1989-06-16
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/04/910/04910956.pdf
[firstpage_image] =>[orig_patent_app_number] => 368135
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/368135 | Gas turbine overtemperature protection | Jun 15, 1989 | Issued |
Array
(
[id] => 2751901
[patent_doc_number] => 04984423
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-01-15
[patent_title] => 'Aerodynamic loading in gas turbine engines'
[patent_app_type] => 1
[patent_app_number] => 7/362865
[patent_app_country] => US
[patent_app_date] => 1989-06-07
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[patent_drawing_sheets_cnt] => 2
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[pdf_file] => patents/04/984/04984423.pdf
[firstpage_image] =>[orig_patent_app_number] => 362865
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/362865 | Aerodynamic loading in gas turbine engines | Jun 6, 1989 | Issued |
Array
(
[id] => 2640745
[patent_doc_number] => 04977740
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-12-18
[patent_title] => 'Dual fuel injector'
[patent_app_type] => 1
[patent_app_number] => 7/362534
[patent_app_country] => US
[patent_app_date] => 1989-06-07
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[pdf_file] => patents/04/977/04977740.pdf
[firstpage_image] =>[orig_patent_app_number] => 362534
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/362534 | Dual fuel injector | Jun 6, 1989 | Issued |
Array
(
[id] => 2711272
[patent_doc_number] => 05031407
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-16
[patent_title] => 'Apparatus for use in a fuel delivery system for a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/362182
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[patent_app_date] => 1989-06-06
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[pdf_file] => patents/05/031/05031407.pdf
[firstpage_image] =>[orig_patent_app_number] => 362182
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/362182 | Apparatus for use in a fuel delivery system for a gas turbine engine | Jun 5, 1989 | Issued |
Array
(
[id] => 2613510
[patent_doc_number] => 04976100
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-12-11
[patent_title] => 'System and method for heat recovery in a combined cycle power plant'
[patent_app_type] => 1
[patent_app_number] => 7/359531
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[patent_app_date] => 1989-06-01
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[pdf_file] => patents/04/976/04976100.pdf
[firstpage_image] =>[orig_patent_app_number] => 359531
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/359531 | System and method for heat recovery in a combined cycle power plant | May 31, 1989 | Issued |
Array
(
[id] => 2723271
[patent_doc_number] => 05010727
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-04-30
[patent_title] => 'Method for evaluating the working line characteristics of a compressor of a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/359144
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[patent_app_date] => 1989-05-31
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[pdf_file] => patents/05/010/05010727.pdf
[firstpage_image] =>[orig_patent_app_number] => 359144
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/359144 | Method for evaluating the working line characteristics of a compressor of a gas turbine engine | May 30, 1989 | Issued |
Array
(
[id] => 2724099
[patent_doc_number] => 05022224
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-11
[patent_title] => 'Acceleration control with duct pressure loss compensation'
[patent_app_type] => 1
[patent_app_number] => 7/359451
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[pdf_file] => patents/05/022/05022224.pdf
[firstpage_image] =>[orig_patent_app_number] => 359451
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/359451 | Acceleration control with duct pressure loss compensation | May 29, 1989 | Issued |
Array
(
[id] => 2751936
[patent_doc_number] => 04984425
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[patent_kind] => NA
[patent_issue_date] => 1991-01-15
[patent_title] => 'Acceleration control for a gas turbine engine'
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[pdf_file] => patents/04/984/04984425.pdf
[firstpage_image] =>[orig_patent_app_number] => 359186
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/359186 | Acceleration control for a gas turbine engine | May 29, 1989 | Issued |
Array
(
[id] => 2727901
[patent_doc_number] => 05020316
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-04
[patent_title] => 'Helicopter control with multiple schedule rotor speed decay anticipator'
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[pdf_file] => patents/05/020/05020316.pdf
[firstpage_image] =>[orig_patent_app_number] => 354534
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/354534 | Helicopter control with multiple schedule rotor speed decay anticipator | May 18, 1989 | Issued |