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] => 1336102 [patent_doc_number] => 06578667 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-06-17 [patent_title] => 'Thrust reverser blocker door access platform' [patent_app_type] => B2 [patent_app_number] => 09/791442 [patent_app_country] => US [patent_app_date] => 2001-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 9 [patent_no_of_words] => 1826 [patent_no_of_claims] => 7 [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/06/578/06578667.pdf [firstpage_image] =>[orig_patent_app_number] => 09791442 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/791442
Thrust reverser blocker door access platform Feb 22, 2001 Issued
Array ( [id] => 1019511 [patent_doc_number] => 06886777 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-03 [patent_title] => 'Coaxial helicopter' [patent_app_type] => utility [patent_app_number] => 09/782941 [patent_app_country] => US [patent_app_date] => 2001-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 17 [patent_no_of_words] => 10663 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/886/06886777.pdf [firstpage_image] =>[orig_patent_app_number] => 09782941 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/782941
Coaxial helicopter Feb 13, 2001 Issued
Array ( [id] => 6903287 [patent_doc_number] => 20050098682 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-12 [patent_title] => 'Light weight helicopter' [patent_app_type] => utility [patent_app_number] => 10/380904 [patent_app_country] => US [patent_app_date] => 2001-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3203 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0098/20050098682.pdf [firstpage_image] =>[orig_patent_app_number] => 10380904 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/380904
Light weight helicopter Feb 6, 2001 Abandoned
Array ( [id] => 1217318 [patent_doc_number] => 06702233 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-03-09 [patent_title] => 'Airfoil anti-icing assembly and method' [patent_app_type] => B1 [patent_app_number] => 09/778178 [patent_app_country] => US [patent_app_date] => 2001-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3818 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/702/06702233.pdf [firstpage_image] =>[orig_patent_app_number] => 09778178 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/778178
Airfoil anti-icing assembly and method Feb 6, 2001 Issued
Array ( [id] => 1541511 [patent_doc_number] => 06443392 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-09-03 [patent_title] => 'Monolithic structure with redundant load paths' [patent_app_type] => B2 [patent_app_number] => 09/778359 [patent_app_country] => US [patent_app_date] => 2001-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 3210 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 179 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/443/06443392.pdf [firstpage_image] =>[orig_patent_app_number] => 09778359 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/778359
Monolithic structure with redundant load paths Feb 6, 2001 Issued
Array ( [id] => 1347443 [patent_doc_number] => 06568636 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-05-27 [patent_title] => 'Buffer stop assembly' [patent_app_type] => B2 [patent_app_number] => 09/778640 [patent_app_country] => US [patent_app_date] => 2001-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3318 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/568/06568636.pdf [firstpage_image] =>[orig_patent_app_number] => 09778640 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/778640
Buffer stop assembly Feb 6, 2001 Issued
Array ( [id] => 1555350 [patent_doc_number] => 06435457 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-20 [patent_title] => 'Thruster systems for spacecraft station changing, station keeping and momentum dumping' [patent_app_type] => B1 [patent_app_number] => 09/769936 [patent_app_country] => US [patent_app_date] => 2001-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 4040 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 301 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/435/06435457.pdf [firstpage_image] =>[orig_patent_app_number] => 09769936 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/769936
Thruster systems for spacecraft station changing, station keeping and momentum dumping Jan 24, 2001 Issued
Array ( [id] => 1449523 [patent_doc_number] => 06460809 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-08 [patent_title] => 'Spacecraft methods and systems for autonomous correction of star tracker charge-transfer-efficiency errors' [patent_app_type] => B1 [patent_app_number] => 09/769637 [patent_app_country] => US [patent_app_date] => 2001-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 13 [patent_no_of_words] => 5296 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 282 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/460/06460809.pdf [firstpage_image] =>[orig_patent_app_number] => 09769637 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/769637
Spacecraft methods and systems for autonomous correction of star tracker charge-transfer-efficiency errors Jan 24, 2001 Issued
Array ( [id] => 1525582 [patent_doc_number] => 06478255 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-11-12 [patent_title] => 'Crash energy absorbing glareshield and method of protecting against head injury in aircraft crashes' [patent_app_type] => B1 [patent_app_number] => 09/765849 [patent_app_country] => US [patent_app_date] => 2001-01-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1542 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/478/06478255.pdf [firstpage_image] =>[orig_patent_app_number] => 09765849 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/765849
Crash energy absorbing glareshield and method of protecting against head injury in aircraft crashes Jan 18, 2001 Issued
Array ( [id] => 6300030 [patent_doc_number] => 20020092948 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-18 [patent_title] => 'Apparatus and method for reducing jet engine noise' [patent_app_type] => new [patent_app_number] => 09/761335 [patent_app_country] => US [patent_app_date] => 2001-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2912 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0092/20020092948.pdf [firstpage_image] =>[orig_patent_app_number] => 09761335 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/761335
Apparatus and method for reducing jet engine noise Jan 15, 2001 Abandoned
Array ( [id] => 1331888 [patent_doc_number] => 06589017 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-07-08 [patent_title] => 'Aircraft airfoil assembly and method' [patent_app_type] => B1 [patent_app_number] => 09/752239 [patent_app_country] => US [patent_app_date] => 2001-01-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 2131 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 284 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/589/06589017.pdf [firstpage_image] =>[orig_patent_app_number] => 09752239 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/752239
Aircraft airfoil assembly and method Jan 1, 2001 Issued
09/720876 SPIRAL AND CYLINDRICAL WING TIP Jan 1, 2001 Abandoned
Array ( [id] => 6569027 [patent_doc_number] => 20020084385 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-04 [patent_title] => 'Spacecraft attack and distress ejectable recorder' [patent_app_type] => new [patent_app_number] => 09/752175 [patent_app_country] => US [patent_app_date] => 2000-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2296 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0084/20020084385.pdf [firstpage_image] =>[orig_patent_app_number] => 09752175 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/752175
Spacecraft attack and distress ejectable recorder Dec 28, 2000 Issued
Array ( [id] => 7039975 [patent_doc_number] => 20010005000 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-06-28 [patent_title] => 'Opening reinforcement for aerostat envelope' [patent_app_type] => new-utility [patent_app_number] => 09/742543 [patent_app_country] => US [patent_app_date] => 2000-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2039 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0005/20010005000.pdf [firstpage_image] =>[orig_patent_app_number] => 09742543 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/742543
Opening reinforcement for aerostat envelope Dec 21, 2000 Issued
Array ( [id] => 1371403 [patent_doc_number] => 06543717 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-04-08 [patent_title] => 'Compact optimal and modulatable thrust device for controlling aerospace vehicles' [patent_app_type] => B1 [patent_app_number] => 09/720210 [patent_app_country] => US [patent_app_date] => 2000-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2750 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/543/06543717.pdf [firstpage_image] =>[orig_patent_app_number] => 09720210 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/720210
Compact optimal and modulatable thrust device for controlling aerospace vehicles Dec 21, 2000 Issued
Array ( [id] => 6885821 [patent_doc_number] => 20010019090 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-09-06 [patent_title] => 'High pressure spray system' [patent_app_type] => new [patent_app_number] => 09/741745 [patent_app_country] => US [patent_app_date] => 2000-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1542 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0019/20010019090.pdf [firstpage_image] =>[orig_patent_app_number] => 09741745 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/741745
High pressure spray system Dec 18, 2000 Abandoned
Array ( [id] => 1591015 [patent_doc_number] => 06491255 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-12-10 [patent_title] => 'Crashworthy external auxiliary fuel tank for aircraft' [patent_app_type] => B1 [patent_app_number] => 09/738125 [patent_app_country] => US [patent_app_date] => 2000-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 15 [patent_no_of_words] => 2726 [patent_no_of_claims] => 27 [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/06/491/06491255.pdf [firstpage_image] =>[orig_patent_app_number] => 09738125 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/738125
Crashworthy external auxiliary fuel tank for aircraft Dec 14, 2000 Issued
Array ( [id] => 1443854 [patent_doc_number] => 06367741 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-04-09 [patent_title] => 'Flight control system for a rotary-wing aircraft, particularly for a helicopter' [patent_app_type] => B2 [patent_app_number] => 09/734641 [patent_app_country] => US [patent_app_date] => 2000-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3592 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/367/06367741.pdf [firstpage_image] =>[orig_patent_app_number] => 09734641 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/734641
Flight control system for a rotary-wing aircraft, particularly for a helicopter Dec 12, 2000 Issued
Array ( [id] => 1485590 [patent_doc_number] => 06428381 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-06 [patent_title] => 'Flying device which rotates as it travels through the air' [patent_app_type] => B1 [patent_app_number] => 09/734263 [patent_app_country] => US [patent_app_date] => 2000-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 2357 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/428/06428381.pdf [firstpage_image] =>[orig_patent_app_number] => 09734263 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/734263
Flying device which rotates as it travels through the air Dec 10, 2000 Issued
Array ( [id] => 6300029 [patent_doc_number] => 20020092947 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-18 [patent_title] => 'Aircraft with elliptical Winglets' [patent_app_type] => new [patent_app_number] => 09/734347 [patent_app_country] => US [patent_app_date] => 2000-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3353 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0092/20020092947.pdf [firstpage_image] =>[orig_patent_app_number] => 09734347 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/734347
Aircraft with elliptical winglets Dec 10, 2000 Issued
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