Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_maintenance] => 1 [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 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 141 [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 [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] => 2347 [patent_no_of_claims] => 11 [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/06/029/06029930.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 [patent_app_date] => 1998-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2774 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4235 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 133 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [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] => 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 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 4063 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 2455 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 09107141 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 14 [patent_no_of_words] => 4329 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_figures_cnt] => 12 [patent_no_of_words] => 5546 [patent_no_of_claims] => 62 [patent_no_of_ind_claims] => 13 [patent_words_short_claim] => 52 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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
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