
John W. Eldred
Examiner (ID: 597, Phone: (571)272-6901 , Office: P/3641 )
| Most Active Art Unit | 3641 |
| Art Unit(s) | 2899, 3644, 2201, 3641 |
| Total Applications | 3399 |
| Issued Applications | 2824 |
| Pending Applications | 195 |
| Abandoned Applications | 399 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 4073064
[patent_doc_number] => 06016994
[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] => 9/110622
[patent_app_country] => US
[patent_app_date] => 1998-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 2950
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/016/06016994.pdf
[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] => 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
[patent_effective_date] => 0000-00-00
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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] => 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
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[patent_no_of_words] => 2429
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[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] => 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
[patent_app_date] => 1998-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2774
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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
[patent_app_country] => US
[patent_app_date] => 1998-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2347
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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] => 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
[patent_app_country] => US
[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
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2455
[patent_no_of_claims] => 7
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[patent_current_assignee] =>[type] => patent
[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
[patent_app_country] => US
[patent_app_date] => 1998-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 3337
[patent_no_of_claims] => 28
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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
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-03-13
[patent_title] => 'Adaptive pneumatic wing for fixed wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/043527
[patent_app_country] => US
[patent_app_date] => 1998-06-29
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[pdf_file] => patents/06/199/06199796.pdf
[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
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-06-11
[patent_title] => 'Balloon trajectory control system'
[patent_app_type] => B1
[patent_app_number] => 09/106563
[patent_app_country] => US
[patent_app_date] => 1998-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 5546
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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 |
| 09/105051 | DUAL-PRESSURE ELECTRONIC PAINTBALL GUN | Jun 25, 1998 | Issued |
Array
(
[id] => 3905517
[patent_doc_number] => 05950964
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-09-14
[patent_title] => 'Cargo guide'
[patent_app_type] => 1
[patent_app_number] => 9/104514
[patent_app_country] => US
[patent_app_date] => 1998-06-25
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[pdf_file] => patents/05/950/05950964.pdf
[firstpage_image] =>[orig_patent_app_number] => 104514
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/104514 | Cargo guide | Jun 24, 1998 | Issued |
Array
(
[id] => 3914908
[patent_doc_number] => 05979831
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-09
[patent_title] => 'System and method for attaching a structural component to an aerospace vehicle'
[patent_app_type] => 1
[patent_app_number] => 9/104963
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/104963 | System and method for attaching a structural component to an aerospace vehicle | Jun 24, 1998 | Issued |
Array
(
[id] => 4284674
[patent_doc_number] => 06250586
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-06-26
[patent_title] => 'Apparatus and method for controlling the motion of a solid body or fluid stream'
[patent_app_type] => 1
[patent_app_number] => 9/091753
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[patent_app_date] => 1998-06-24
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[pdf_file] => patents/06/250/06250586.pdf
[firstpage_image] =>[orig_patent_app_number] => 091753
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/091753 | Apparatus and method for controlling the motion of a solid body or fluid stream | Jun 23, 1998 | Issued |
Array
(
[id] => 4228969
[patent_doc_number] => 06220549
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[patent_kind] => NA
[patent_issue_date] => 2001-04-24
[patent_title] => 'Method and apparatus for fabricating panels used for the active control of surface drag'
[patent_app_type] => 1
[patent_app_number] => 9/100307
[patent_app_country] => US
[patent_app_date] => 1998-06-19
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[pdf_file] => patents/06/220/06220549.pdf
[firstpage_image] =>[orig_patent_app_number] => 100307
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/100307 | Method and apparatus for fabricating panels used for the active control of surface drag | Jun 18, 1998 | Issued |
Array
(
[id] => 4058316
[patent_doc_number] => 06068213
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-05-30
[patent_title] => 'Aircraft engine ducted fan cowling with thrust reverser section and fairings for fan shroud brace members in fan exhaust duct'
[patent_app_type] => 1
[patent_app_number] => 9/096293
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/096293 | Aircraft engine ducted fan cowling with thrust reverser section and fairings for fan shroud brace members in fan exhaust duct | Jun 11, 1998 | Issued |
Array
(
[id] => 4122360
[patent_doc_number] => 06059228
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[patent_kind] => NA
[patent_issue_date] => 2000-05-09
[patent_title] => 'Hydraulic system'
[patent_app_type] => 1
[patent_app_number] => 9/094485
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 094485
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/094485 | Hydraulic system | Jun 9, 1998 | Issued |
Array
(
[id] => 4272505
[patent_doc_number] => 06267331
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[patent_issue_date] => 2001-07-31
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Array
(
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[firstpage_image] =>[orig_patent_app_number] => 088085
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/088085 | Air-dropped, precision-guided, payload delivery system | May 31, 1998 | Issued |
Array
(
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[firstpage_image] =>[orig_patent_app_number] => 087891
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/087891 | Flow diverter system for multiple streams for gas turbine engine | May 29, 1998 | Issued |