
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[patent_no_of_words] => 5833
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[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
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[patent_no_of_words] => 5577
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[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
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[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
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[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
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[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
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[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 |