Search

Amanda Lee Bailey

Examiner (ID: 4785)

Most Active Art Unit
3673
Art Unit(s)
3673
Total Applications
468
Issued Applications
245
Pending Applications
48
Abandoned Applications
191

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 4391584 [patent_doc_number] => 06227496 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-05-08 [patent_title] => 'Attitude determination system for artificial satellite' [patent_app_type] => 1 [patent_app_number] => 9/610603 [patent_app_country] => US [patent_app_date] => 2000-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 15 [patent_no_of_words] => 14669 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/227/06227496.pdf [firstpage_image] =>[orig_patent_app_number] => 610603 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/610603
Attitude determination system for artificial satellite Jul 4, 2000 Issued
Array ( [id] => 1544981 [patent_doc_number] => 06398167 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-06-04 [patent_title] => 'Aircraft braking system' [patent_app_type] => B1 [patent_app_number] => 09/609684 [patent_app_country] => US [patent_app_date] => 2000-07-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1477 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/398/06398167.pdf [firstpage_image] =>[orig_patent_app_number] => 09609684 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/609684
Aircraft braking system Jul 2, 2000 Issued
Array ( [id] => 1433860 [patent_doc_number] => 06341150 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-01-22 [patent_title] => 'Fissile material detector' [patent_app_type] => B1 [patent_app_number] => 09/608778 [patent_app_country] => US [patent_app_date] => 2000-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3859 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 58 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/341/06341150.pdf [firstpage_image] =>[orig_patent_app_number] => 09608778 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/608778
Fissile material detector Jun 29, 2000 Issued
Array ( [id] => 1499467 [patent_doc_number] => 06464174 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-15 [patent_title] => 'Round-trip orbital operation of a spacecraft' [patent_app_type] => B1 [patent_app_number] => 09/598128 [patent_app_country] => US [patent_app_date] => 2000-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 5612 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/464/06464174.pdf [firstpage_image] =>[orig_patent_app_number] => 09598128 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/598128
Round-trip orbital operation of a spacecraft Jun 20, 2000 Issued
09/581823 UNMANNED ROTOR CARRIED AERIAL VEHICLE Jun 18, 2000 Abandoned
Array ( [id] => 4309893 [patent_doc_number] => 06328259 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-12-11 [patent_title] => 'Variable-load shear collar for helicopter landing gear shock struts' [patent_app_type] => 1 [patent_app_number] => 9/587954 [patent_app_country] => US [patent_app_date] => 2000-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 8 [patent_no_of_words] => 2814 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 58 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/328/06328259.pdf [firstpage_image] =>[orig_patent_app_number] => 587954 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/587954
Variable-load shear collar for helicopter landing gear shock struts Jun 5, 2000 Issued
09/588154 Hybrid Air Vehicle Having Air Cushion Landing Gear Jun 4, 2000 Abandoned
Array ( [id] => 1522301 [patent_doc_number] => 06352220 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-03-05 [patent_title] => 'Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof' [patent_app_type] => B1 [patent_app_number] => 09/586603 [patent_app_country] => US [patent_app_date] => 2000-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 18 [patent_no_of_words] => 6257 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/352/06352220.pdf [firstpage_image] =>[orig_patent_app_number] => 09586603 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/586603
Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof Jun 1, 2000 Issued
Array ( [id] => 1588756 [patent_doc_number] => 06382558 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-07 [patent_title] => 'Safety system for a helicopter' [patent_app_type] => B1 [patent_app_number] => 09/585482 [patent_app_country] => US [patent_app_date] => 2000-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2476 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/382/06382558.pdf [firstpage_image] =>[orig_patent_app_number] => 09585482 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/585482
Safety system for a helicopter Jun 1, 2000 Issued
Array ( [id] => 1235654 [patent_doc_number] => 06685142 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-02-03 [patent_title] => 'Three-axis position control for low-orbiting satellites' [patent_app_type] => B1 [patent_app_number] => 09/583340 [patent_app_country] => US [patent_app_date] => 2000-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2494 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 72 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/685/06685142.pdf [firstpage_image] =>[orig_patent_app_number] => 09583340 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/583340
Three-axis position control for low-orbiting satellites May 30, 2000 Issued
Array ( [id] => 1584313 [patent_doc_number] => 06481669 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-11-19 [patent_title] => 'Pneumatic actuator for a stores carriage and ejection system' [patent_app_type] => B1 [patent_app_number] => 09/576254 [patent_app_country] => US [patent_app_date] => 2000-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 14 [patent_no_of_words] => 9283 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 219 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/481/06481669.pdf [firstpage_image] =>[orig_patent_app_number] => 09576254 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/576254
Pneumatic actuator for a stores carriage and ejection system May 23, 2000 Issued
Array ( [id] => 1475737 [patent_doc_number] => 06343768 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-02-05 [patent_title] => 'Vertical/short take-off and landing aircraft' [patent_app_type] => B1 [patent_app_number] => 09/571815 [patent_app_country] => US [patent_app_date] => 2000-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4335 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/343/06343768.pdf [firstpage_image] =>[orig_patent_app_number] => 09571815 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/571815
Vertical/short take-off and landing aircraft May 15, 2000 Issued
Array ( [id] => 1446600 [patent_doc_number] => 06454214 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-24 [patent_title] => 'Device and method for connecting two parts of a craft' [patent_app_type] => B1 [patent_app_number] => 09/568144 [patent_app_country] => US [patent_app_date] => 2000-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2669 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 36 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/454/06454214.pdf [firstpage_image] =>[orig_patent_app_number] => 09568144 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/568144
Device and method for connecting two parts of a craft May 9, 2000 Issued
Array ( [id] => 1503081 [patent_doc_number] => 06439507 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-27 [patent_title] => 'Closed-loop spacecraft orbit control' [patent_app_type] => B1 [patent_app_number] => 09/565836 [patent_app_country] => US [patent_app_date] => 2000-05-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 3146 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/439/06439507.pdf [firstpage_image] =>[orig_patent_app_number] => 09565836 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/565836
Closed-loop spacecraft orbit control May 4, 2000 Issued
Array ( [id] => 1550721 [patent_doc_number] => 06347767 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-02-19 [patent_title] => 'Method of and apparatus for detection of ice accretion' [patent_app_type] => B1 [patent_app_number] => 09/530647 [patent_app_country] => US [patent_app_date] => 2000-05-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 5833 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/347/06347767.pdf [firstpage_image] =>[orig_patent_app_number] => 09530647 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/530647
Method of and apparatus for detection of ice accretion May 2, 2000 Issued
Array ( [id] => 998340 [patent_doc_number] => 06910662 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-06-28 [patent_title] => 'Aircraft wing and wing parts movable adjacent to the aircraft wing' [patent_app_type] => utility [patent_app_number] => 09/959707 [patent_app_country] => US [patent_app_date] => 2000-05-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 25 [patent_no_of_words] => 5577 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/910/06910662.pdf [firstpage_image] =>[orig_patent_app_number] => 09959707 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/959707
Aircraft wing and wing parts movable adjacent to the aircraft wing May 1, 2000 Issued
Array ( [id] => 4394341 [patent_doc_number] => 06308919 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-10-30 [patent_title] => 'Spacecraft having a dual reflector holddown for deploying multiple reflectors in a single release event' [patent_app_type] => 1 [patent_app_number] => 9/558444 [patent_app_country] => US [patent_app_date] => 2000-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 2471 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/308/06308919.pdf [firstpage_image] =>[orig_patent_app_number] => 558444 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/558444
Spacecraft having a dual reflector holddown for deploying multiple reflectors in a single release event Apr 24, 2000 Issued
Array ( [id] => 4312921 [patent_doc_number] => 06311926 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-11-06 [patent_title] => 'Space tram' [patent_app_type] => 1 [patent_app_number] => 9/558423 [patent_app_country] => US [patent_app_date] => 2000-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 23 [patent_no_of_words] => 11444 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/311/06311926.pdf [firstpage_image] =>[orig_patent_app_number] => 558423 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/558423
Space tram Apr 24, 2000 Issued
Array ( [id] => 1491905 [patent_doc_number] => 06341746 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-01-29 [patent_title] => 'Device for attaching an aircraft engine' [patent_app_type] => B1 [patent_app_number] => 09/556443 [patent_app_country] => US [patent_app_date] => 2000-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 3599 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/341/06341746.pdf [firstpage_image] =>[orig_patent_app_number] => 09556443 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/556443
Device for attaching an aircraft engine Apr 23, 2000 Issued
Array ( [id] => 4366945 [patent_doc_number] => 06293500 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-09-25 [patent_title] => 'Integrated translation tube assembly for a space module' [patent_app_type] => 1 [patent_app_number] => 9/549624 [patent_app_country] => US [patent_app_date] => 2000-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4831 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 170 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/293/06293500.pdf [firstpage_image] =>[orig_patent_app_number] => 549624 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/549624
Integrated translation tube assembly for a space module Apr 13, 2000 Issued
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