
Howard Richman
Examiner (ID: 9704)
| Most Active Art Unit | 3403 |
| Art Unit(s) | 2899, 3403 |
| Total Applications | 311 |
| Issued Applications | 278 |
| Pending Applications | 5 |
| Abandoned Applications | 28 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2900073
[patent_doc_number] => 05199255
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-04-06
[patent_title] => 'Selective gas-phase nox reduction in gas turbines'
[patent_app_type] => 1
[patent_app_number] => 7/679803
[patent_app_country] => US
[patent_app_date] => 1991-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 4193
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/199/05199255.pdf
[firstpage_image] =>[orig_patent_app_number] => 679803
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/679803 | Selective gas-phase nox reduction in gas turbines | Apr 2, 1991 | Issued |
Array
(
[id] => 2917268
[patent_doc_number] => 05189874
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-02
[patent_title] => 'Axial-flow gas turbine cooling arrangement'
[patent_app_type] => 1
[patent_app_number] => 7/679274
[patent_app_country] => US
[patent_app_date] => 1991-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2480
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 218
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/189/05189874.pdf
[firstpage_image] =>[orig_patent_app_number] => 679274
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/679274 | Axial-flow gas turbine cooling arrangement | Apr 1, 1991 | Issued |
Array
(
[id] => 2775338
[patent_doc_number] => 05129790
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-14
[patent_title] => 'Plunger pump'
[patent_app_type] => 1
[patent_app_number] => 7/672318
[patent_app_country] => US
[patent_app_date] => 1991-03-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 4782
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 203
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/129/05129790.pdf
[firstpage_image] =>[orig_patent_app_number] => 672318
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/672318 | Plunger pump | Mar 19, 1991 | Issued |
Array
(
[id] => 2900432
[patent_doc_number] => 05236354
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-17
[patent_title] => 'Power plant with efficient emission control for obtaining high turbine inlet temperature'
[patent_app_type] => 1
[patent_app_number] => 7/672067
[patent_app_country] => US
[patent_app_date] => 1991-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4049
[patent_no_of_claims] => 17
[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/05/236/05236354.pdf
[firstpage_image] =>[orig_patent_app_number] => 672067
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/672067 | Power plant with efficient emission control for obtaining high turbine inlet temperature | Mar 17, 1991 | Issued |
Array
(
[id] => 2834920
[patent_doc_number] => 05133183
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-28
[patent_title] => 'Gel/solid bipropellant propulsion system with energy management capability'
[patent_app_type] => 1
[patent_app_number] => 7/662851
[patent_app_country] => US
[patent_app_date] => 1991-03-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1974
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 1021
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/133/05133183.pdf
[firstpage_image] =>[orig_patent_app_number] => 662851
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/662851 | Gel/solid bipropellant propulsion system with energy management capability | Feb 28, 1991 | Issued |
Array
(
[id] => 2895274
[patent_doc_number] => 05177957
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-01-12
[patent_title] => 'Propfan turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/662442
[patent_app_country] => US
[patent_app_date] => 1991-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 8
[patent_no_of_words] => 2853
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/177/05177957.pdf
[firstpage_image] =>[orig_patent_app_number] => 662442
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/662442 | Propfan turbine engine | Feb 27, 1991 | Issued |
Array
(
[id] => 2873484
[patent_doc_number] => 05239823
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-31
[patent_title] => 'Multiple layer cooled nozzle liner'
[patent_app_type] => 1
[patent_app_number] => 7/661354
[patent_app_country] => US
[patent_app_date] => 1991-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2131
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/239/05239823.pdf
[firstpage_image] =>[orig_patent_app_number] => 661354
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/661354 | Multiple layer cooled nozzle liner | Feb 25, 1991 | Issued |
| 07/659867 | METHOD AND APPARATUS FOR PROPULSION SYSTEMS OF SPACE FLIGHT THRUSTERS | Feb 21, 1991 | Abandoned |
Array
(
[id] => 2838504
[patent_doc_number] => 05165241
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-11-24
[patent_title] => 'Air fuel mixer for gas turbine combustor'
[patent_app_type] => 1
[patent_app_number] => 7/660315
[patent_app_country] => US
[patent_app_date] => 1991-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2759
[patent_no_of_claims] => 15
[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/05/165/05165241.pdf
[firstpage_image] =>[orig_patent_app_number] => 660315
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/660315 | Air fuel mixer for gas turbine combustor | Feb 21, 1991 | Issued |
Array
(
[id] => 2774253
[patent_doc_number] => 05142859
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-01
[patent_title] => 'Turbine cooling system'
[patent_app_type] => 1
[patent_app_number] => 7/658830
[patent_app_country] => US
[patent_app_date] => 1991-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4883
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 49
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/142/05142859.pdf
[firstpage_image] =>[orig_patent_app_number] => 658830
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/658830 | Turbine cooling system | Feb 21, 1991 | Issued |
Array
(
[id] => 2797389
[patent_doc_number] => 05121599
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-06-16
[patent_title] => 'Oil filtration system and method'
[patent_app_type] => 1
[patent_app_number] => 7/658947
[patent_app_country] => US
[patent_app_date] => 1991-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2299
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/121/05121599.pdf
[firstpage_image] =>[orig_patent_app_number] => 658947
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/658947 | Oil filtration system and method | Feb 20, 1991 | Issued |
Array
(
[id] => 2898910
[patent_doc_number] => 05233822
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-10
[patent_title] => 'Method and system for the disassembly of an annular combustor'
[patent_app_type] => 1
[patent_app_number] => 7/648769
[patent_app_country] => US
[patent_app_date] => 1991-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 2803
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/233/05233822.pdf
[firstpage_image] =>[orig_patent_app_number] => 648769
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/648769 | Method and system for the disassembly of an annular combustor | Jan 30, 1991 | Issued |
Array
(
[id] => 2905465
[patent_doc_number] => 05185997
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-02-16
[patent_title] => 'Gas turbine system'
[patent_app_type] => 1
[patent_app_number] => 7/646433
[patent_app_country] => US
[patent_app_date] => 1991-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3237
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 253
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/185/05185997.pdf
[firstpage_image] =>[orig_patent_app_number] => 646433
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/646433 | Gas turbine system | Jan 27, 1991 | Issued |
Array
(
[id] => 2849425
[patent_doc_number] => 05161369
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-11-10
[patent_title] => 'Aft fan gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/646253
[patent_app_country] => US
[patent_app_date] => 1991-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 1646
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 193
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/161/05161369.pdf
[firstpage_image] =>[orig_patent_app_number] => 646253
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/646253 | Aft fan gas turbine engine | Jan 27, 1991 | Issued |
| 07/642780 | GAS TURBINE ENGINE FUEL MANIFOLD | Jan 17, 1991 | Abandoned |
Array
(
[id] => 2805657
[patent_doc_number] => 05172543
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-22
[patent_title] => 'Starting system for a gas turbine and method of starting a gas turbine'
[patent_app_type] => 1
[patent_app_number] => 7/633794
[patent_app_country] => US
[patent_app_date] => 1990-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2567
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/172/05172543.pdf
[firstpage_image] =>[orig_patent_app_number] => 633794
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/633794 | Starting system for a gas turbine and method of starting a gas turbine | Dec 25, 1990 | Issued |
Array
(
[id] => 2905437
[patent_doc_number] => 05185996
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-02-16
[patent_title] => 'Gas turbine engine sensor probe'
[patent_app_type] => 1
[patent_app_number] => 7/633548
[patent_app_country] => US
[patent_app_date] => 1990-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2659
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/185/05185996.pdf
[firstpage_image] =>[orig_patent_app_number] => 633548
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/633548 | Gas turbine engine sensor probe | Dec 20, 1990 | Issued |
Array
(
[id] => 2760557
[patent_doc_number] => 05150571
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-29
[patent_title] => 'Device for exposing or shutting off a turbo-engine on the intake air side of the engine'
[patent_app_type] => 1
[patent_app_number] => 7/631886
[patent_app_country] => US
[patent_app_date] => 1990-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3965
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 43
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/150/05150571.pdf
[firstpage_image] =>[orig_patent_app_number] => 631886
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/631886 | Device for exposing or shutting off a turbo-engine on the intake air side of the engine | Dec 20, 1990 | Issued |
| 07/631661 | GAS GENERATING APPARATUS | Dec 19, 1990 | Abandoned |
Array
(
[id] => 2822972
[patent_doc_number] => 05159809
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-11-03
[patent_title] => 'Highly adaptable combined propulsion engine for an aircraft or a space-going airplane'
[patent_app_type] => 1
[patent_app_number] => 7/630088
[patent_app_country] => US
[patent_app_date] => 1990-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 20
[patent_no_of_words] => 7215
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 284
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/159/05159809.pdf
[firstpage_image] =>[orig_patent_app_number] => 630088
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/630088 | Highly adaptable combined propulsion engine for an aircraft or a space-going airplane | Dec 18, 1990 | Issued |