
John W. Eldred
Examiner (ID: 10195)
| Most Active Art Unit | 3641 |
| Art Unit(s) | 3644, 3641, 2201, 2899 |
| Total Applications | 3389 |
| Issued Applications | 2819 |
| Pending Applications | 192 |
| Abandoned Applications | 398 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 4092936
[patent_doc_number] => 06056239
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-05-02
[patent_title] => 'Convertible seating and sleeping accommodations for aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/132658
[patent_app_country] => US
[patent_app_date] => 1998-08-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 23
[patent_no_of_words] => 8261
[patent_no_of_claims] => 13
[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/06/056/06056239.pdf
[firstpage_image] =>[orig_patent_app_number] => 132658
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/132658 | Convertible seating and sleeping accommodations for aircraft | Aug 11, 1998 | Issued |
Array
(
[id] => 4196811
[patent_doc_number] => 06086014
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-07-11
[patent_title] => 'Roadable aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/132911
[patent_app_country] => US
[patent_app_date] => 1998-08-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 18
[patent_no_of_words] => 12513
[patent_no_of_claims] => 69
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 101
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/086/06086014.pdf
[firstpage_image] =>[orig_patent_app_number] => 132911
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/132911 | Roadable aircraft | Aug 11, 1998 | Issued |
Array
(
[id] => 4083596
[patent_doc_number] => 06098928
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-08-08
[patent_title] => 'Tube connection, in particular, for connecting two tubular fuselage portions of a missile'
[patent_app_type] => 1
[patent_app_number] => 9/132263
[patent_app_country] => US
[patent_app_date] => 1998-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1094
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 239
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/098/06098928.pdf
[firstpage_image] =>[orig_patent_app_number] => 132263
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/132263 | Tube connection, in particular, for connecting two tubular fuselage portions of a missile | Aug 10, 1998 | Issued |
Array
(
[id] => 3954210
[patent_doc_number] => 05947100
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-09-07
[patent_title] => 'Paint ball gun agitator sound trigger and duration control'
[patent_app_type] => 1
[patent_app_number] => 9/131816
[patent_app_country] => US
[patent_app_date] => 1998-08-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 5978
[patent_no_of_claims] => 16
[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/05/947/05947100.pdf
[firstpage_image] =>[orig_patent_app_number] => 131816
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/131816 | Paint ball gun agitator sound trigger and duration control | Aug 9, 1998 | Issued |
Array
(
[id] => 4068196
[patent_doc_number] => 06131854
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-17
[patent_title] => 'Ground handling apparatus for unmanned tactical aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/131136
[patent_app_country] => US
[patent_app_date] => 1998-08-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1849
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/131/06131854.pdf
[firstpage_image] =>[orig_patent_app_number] => 131136
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/131136 | Ground handling apparatus for unmanned tactical aircraft | Aug 6, 1998 | Issued |
Array
(
[id] => 4098999
[patent_doc_number] => 06045092
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-04
[patent_title] => 'Apparatus and method for deicing aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/129533
[patent_app_country] => US
[patent_app_date] => 1998-08-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3243
[patent_no_of_claims] => 34
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/045/06045092.pdf
[firstpage_image] =>[orig_patent_app_number] => 129533
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/129533 | Apparatus and method for deicing aircraft | Aug 4, 1998 | Issued |
Array
(
[id] => 4073151
[patent_doc_number] => 06017000
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-01-25
[patent_title] => 'Apparatus and methods for in-space satellite operations'
[patent_app_type] => 1
[patent_app_number] => 9/146161
[patent_app_country] => US
[patent_app_date] => 1998-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 5342
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/017/06017000.pdf
[firstpage_image] =>[orig_patent_app_number] => 146161
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/146161 | Apparatus and methods for in-space satellite operations | Aug 1, 1998 | Issued |
Array
(
[id] => 4190446
[patent_doc_number] => 06076775
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-06-20
[patent_title] => 'Airfoil with a landing flap having a flexible trailing edge'
[patent_app_type] => 1
[patent_app_number] => 9/127406
[patent_app_country] => US
[patent_app_date] => 1998-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4872
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/076/06076775.pdf
[firstpage_image] =>[orig_patent_app_number] => 127406
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/127406 | Airfoil with a landing flap having a flexible trailing edge | Jul 30, 1998 | Issued |
Array
(
[id] => 3913293
[patent_doc_number] => 05971327
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-10-26
[patent_title] => 'Mesoflap passive transpiration system and method for shock/boundary layer interaction control'
[patent_app_type] => 1
[patent_app_number] => 9/123962
[patent_app_country] => US
[patent_app_date] => 1998-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2538
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 48
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/971/05971327.pdf
[firstpage_image] =>[orig_patent_app_number] => 123962
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/123962 | Mesoflap passive transpiration system and method for shock/boundary layer interaction control | Jul 28, 1998 | Issued |
Array
(
[id] => 4192783
[patent_doc_number] => 06027073
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-22
[patent_title] => 'Window release system'
[patent_app_type] => 1
[patent_app_number] => 9/116170
[patent_app_country] => US
[patent_app_date] => 1998-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2420
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 169
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/027/06027073.pdf
[firstpage_image] =>[orig_patent_app_number] => 116170
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/116170 | Window release system | Jul 15, 1998 | Issued |
Array
(
[id] => 4073051
[patent_doc_number] => 06016993
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-01-25
[patent_title] => 'Method of monitoring a transmission assembly of a vehicle equipped with acceleration sensors, in particular a helicopter'
[patent_app_type] => 1
[patent_app_number] => 9/110305
[patent_app_country] => US
[patent_app_date] => 1998-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2429
[patent_no_of_claims] => 9
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/016/06016993.pdf
[firstpage_image] =>[orig_patent_app_number] => 110305
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/110305 | Method of monitoring a transmission assembly of a vehicle equipped with acceleration sensors, in particular a helicopter | Jul 5, 1998 | Issued |
Array
(
[id] => 4127518
[patent_doc_number] => 06029930
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-29
[patent_title] => 'Method of monitoring a transmission assembly of a vehicle equipped with acceleration sensors, in particular a helicopter'
[patent_app_type] => 1
[patent_app_number] => 9/110621
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[patent_app_date] => 1998-07-06
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[pdf_file] => patents/06/029/06029930.pdf
[firstpage_image] =>[orig_patent_app_number] => 110621
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/110621 | Method of monitoring a transmission assembly of a vehicle equipped with acceleration sensors, in particular a helicopter | Jul 5, 1998 | Issued |
Array
(
[id] => 4167485
[patent_doc_number] => 06019310
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-01
[patent_title] => 'Method of monitoring on the basis of signal energy a transmission assembly of a vehicle equipped with acceleration sensors in particular a helicopter'
[patent_app_type] => 1
[patent_app_number] => 9/110307
[patent_app_country] => US
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[pdf_file] => patents/06/019/06019310.pdf
[firstpage_image] =>[orig_patent_app_number] => 110307
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/110307 | Method of monitoring on the basis of signal energy a transmission assembly of a vehicle equipped with acceleration sensors in particular a helicopter | Jul 5, 1998 | Issued |
Array
(
[id] => 4070783
[patent_doc_number] => 06024324
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-15
[patent_title] => 'Method of monitoring an epicyclic assembly of a vehicle equipped with acceleration sensors in particular a helicopter'
[patent_app_type] => 1
[patent_app_number] => 9/110306
[patent_app_country] => US
[patent_app_date] => 1998-07-06
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[patent_no_of_words] => 4235
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[pdf_file] => patents/06/024/06024324.pdf
[firstpage_image] =>[orig_patent_app_number] => 110306
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/110306 | Method of monitoring an epicyclic assembly of a vehicle equipped with acceleration sensors in particular a helicopter | Jul 5, 1998 | Issued |
Array
(
[id] => 4073064
[patent_doc_number] => 06016994
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[patent_issue_date] => 2000-01-25
[patent_title] => 'Method of monitoring a transmission assembly of a vehicle equipped with acceleration sensors, in particular a helicopter'
[patent_app_type] => 1
[patent_app_number] => 9/110622
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[firstpage_image] =>[orig_patent_app_number] => 110622
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/110622 | Method of monitoring a transmission assembly of a vehicle equipped with acceleration sensors, in particular a helicopter | Jul 5, 1998 | Issued |
Array
(
[id] => 4073136
[patent_doc_number] => 06016999
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-01-25
[patent_title] => 'Spacecraft platforms'
[patent_app_type] => 1
[patent_app_number] => 9/109385
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[patent_app_date] => 1998-07-02
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/016/06016999.pdf
[firstpage_image] =>[orig_patent_app_number] => 109385
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/109385 | Spacecraft platforms | Jul 1, 1998 | Issued |
Array
(
[id] => 4114187
[patent_doc_number] => 06032899
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-03-07
[patent_title] => 'Blade pitch locking device for a main rotor of a rotary-wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/114233
[patent_app_country] => US
[patent_app_date] => 1998-07-02
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[pdf_file] => patents/06/032/06032899.pdf
[firstpage_image] =>[orig_patent_app_number] => 114233
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/114233 | Blade pitch locking device for a main rotor of a rotary-wing aircraft | Jul 1, 1998 | Issued |
Array
(
[id] => 8350651
[patent_doc_number] => 08245978
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-08-21
[patent_title] => 'Multiple ASM OBIGGS with different permeability and selectivity membranes'
[patent_app_type] => utility
[patent_app_number] => 09/107141
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/107141 | Multiple ASM OBIGGS with different permeability and selectivity membranes | Jun 29, 1998 | Issued |
Array
(
[id] => 4338662
[patent_doc_number] => 06199796
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[patent_issue_date] => 2001-03-13
[patent_title] => 'Adaptive pneumatic wing for fixed wing aircraft'
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[firstpage_image] =>[orig_patent_app_number] => 043527
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/043527 | Adaptive pneumatic wing for fixed wing aircraft | Jun 28, 1998 | Issued |
Array
(
[id] => 1490364
[patent_doc_number] => 06402090
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[patent_issue_date] => 2002-06-11
[patent_title] => 'Balloon trajectory control system'
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[pdf_file] => patents/06/402/06402090.pdf
[firstpage_image] =>[orig_patent_app_number] => 09106563
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/106563 | Balloon trajectory control system | Jun 28, 1998 | Issued |