Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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] => 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] => 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] => 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
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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2296 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 241 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_country] => US [patent_app_date] => 1998-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2526 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/979/05979831.pdf [firstpage_image] =>[orig_patent_app_number] => 104963 [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 [patent_app_country] => US [patent_app_date] => 1998-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 14 [patent_no_of_words] => 2935 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 52 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 18 [patent_no_of_words] => 7293 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 183 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_country] => US [patent_app_date] => 1998-06-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 1931 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/068/06068213.pdf [firstpage_image] =>[orig_patent_app_number] => 096293 [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 [patent_country] => US [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 [patent_app_date] => 1998-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 16824 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 297 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/059/06059228.pdf [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 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-07-31 [patent_title] => 'Airfoil with dynamic stall control by oscillatory forcing' [patent_app_type] => 1 [patent_app_number] => 9/092271 [patent_app_country] => US [patent_app_date] => 1998-06-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 36 [patent_no_of_words] => 8756 [patent_no_of_claims] => 35 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/267/06267331.pdf [firstpage_image] =>[orig_patent_app_number] => 092271 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/092271
Airfoil with dynamic stall control by oscillatory forcing Jun 4, 1998 Issued
Array ( [id] => 4167587 [patent_doc_number] => 06019317 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-02-01 [patent_title] => 'Air-dropped, precision-guided, payload delivery system' [patent_app_type] => 1 [patent_app_number] => 9/088085 [patent_app_country] => US [patent_app_date] => 1998-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 1 [patent_no_of_words] => 1486 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/019/06019317.pdf [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 ( [id] => 4135618 [patent_doc_number] => 06102329 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-08-15 [patent_title] => 'Flow diverter system for multiple streams for gas turbine engine' [patent_app_type] => 1 [patent_app_number] => 9/087891 [patent_app_country] => US [patent_app_date] => 1998-05-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 18 [patent_no_of_words] => 4516 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/102/06102329.pdf [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
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