
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 |
|---|---|---|---|
| 08/366821 | FLUIDIC CONTROL THRUST VECTORING NOZZLE | Dec 29, 1994 | Abandoned |
Array
(
[id] => 3704810
[patent_doc_number] => 05615848
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-04-01
[patent_title] => 'Rescue and ambulance helicopter'
[patent_app_type] => 1
[patent_app_number] => 8/363155
[patent_app_country] => US
[patent_app_date] => 1994-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 2142
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/615/05615848.pdf
[firstpage_image] =>[orig_patent_app_number] => 363155
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/363155 | Rescue and ambulance helicopter | Dec 22, 1994 | Issued |
Array
(
[id] => 3575035
[patent_doc_number] => 05549258
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-08-27
[patent_title] => 'Retrofit luggage bin assembly compatible with existing aircraft bin supports'
[patent_app_type] => 1
[patent_app_number] => 8/363765
[patent_app_country] => US
[patent_app_date] => 1994-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3414
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 230
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/549/05549258.pdf
[firstpage_image] =>[orig_patent_app_number] => 363765
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/363765 | Retrofit luggage bin assembly compatible with existing aircraft bin supports | Dec 22, 1994 | Issued |
Array
(
[id] => 3717702
[patent_doc_number] => 05664743
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-09-09
[patent_title] => 'Device for gripping, guiding and transporting wheeled helicopters particularly for ship\'s decks'
[patent_app_type] => 1
[patent_app_number] => 8/362154
[patent_app_country] => US
[patent_app_date] => 1994-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 12
[patent_no_of_words] => 2282
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 280
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/664/05664743.pdf
[firstpage_image] =>[orig_patent_app_number] => 362154
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/362154 | Device for gripping, guiding and transporting wheeled helicopters particularly for ship's decks | Dec 21, 1994 | Issued |
Array
(
[id] => 3611820
[patent_doc_number] => 05607122
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-03-04
[patent_title] => 'Tail rotor authority control for a helicopter'
[patent_app_type] => 1
[patent_app_number] => 8/362245
[patent_app_country] => US
[patent_app_date] => 1994-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 30
[patent_no_of_words] => 14920
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/607/05607122.pdf
[firstpage_image] =>[orig_patent_app_number] => 362245
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/362245 | Tail rotor authority control for a helicopter | Dec 21, 1994 | Issued |
Array
(
[id] => 3611737
[patent_doc_number] => 05641123
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-06-24
[patent_title] => 'Expandable nozzle mechanism for a rocket engine'
[patent_app_type] => 1
[patent_app_number] => 8/360421
[patent_app_country] => US
[patent_app_date] => 1994-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 22
[patent_no_of_words] => 6594
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/641/05641123.pdf
[firstpage_image] =>[orig_patent_app_number] => 360421
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/360421 | Expandable nozzle mechanism for a rocket engine | Dec 20, 1994 | Issued |
Array
(
[id] => 3586750
[patent_doc_number] => 05558301
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-09-24
[patent_title] => 'Aircraft and in particular rotary-wing aircraft seat having an energy absorption device automatically adjustable as a function of the size of the occupant'
[patent_app_type] => 1
[patent_app_number] => 8/360564
[patent_app_country] => US
[patent_app_date] => 1994-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3713
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/558/05558301.pdf
[firstpage_image] =>[orig_patent_app_number] => 360564
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/360564 | Aircraft and in particular rotary-wing aircraft seat having an energy absorption device automatically adjustable as a function of the size of the occupant | Dec 20, 1994 | Issued |
Array
(
[id] => 3569298
[patent_doc_number] => 05580013
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-12-03
[patent_title] => 'Economical construction and assembly method for a modular permanent orbiting space station'
[patent_app_type] => 1
[patent_app_number] => 8/359644
[patent_app_country] => US
[patent_app_date] => 1994-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 28
[patent_no_of_words] => 4742
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 275
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/580/05580013.pdf
[firstpage_image] =>[orig_patent_app_number] => 359644
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/359644 | Economical construction and assembly method for a modular permanent orbiting space station | Dec 19, 1994 | Issued |
Array
(
[id] => 3575879
[patent_doc_number] => 05584447
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-12-17
[patent_title] => 'Noise control using a plate radiator and an acoustic resonator'
[patent_app_type] => 1
[patent_app_number] => 8/359165
[patent_app_country] => US
[patent_app_date] => 1994-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2982
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/584/05584447.pdf
[firstpage_image] =>[orig_patent_app_number] => 359165
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/359165 | Noise control using a plate radiator and an acoustic resonator | Dec 18, 1994 | Issued |
Array
(
[id] => 3654868
[patent_doc_number] => 05598990
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-02-04
[patent_title] => 'Supersonic vortex generator'
[patent_app_type] => 1
[patent_app_number] => 8/356646
[patent_app_country] => US
[patent_app_date] => 1994-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 19
[patent_no_of_words] => 5245
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 279
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/598/05598990.pdf
[firstpage_image] =>[orig_patent_app_number] => 356646
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/356646 | Supersonic vortex generator | Dec 14, 1994 | Issued |
Array
(
[id] => 3540752
[patent_doc_number] => 05573205
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-11-12
[patent_title] => 'Pull cord tension transmitting device using dual rack-pinion'
[patent_app_type] => 1
[patent_app_number] => 8/352234
[patent_app_country] => US
[patent_app_date] => 1994-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1060
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 247
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/573/05573205.pdf
[firstpage_image] =>[orig_patent_app_number] => 352234
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/352234 | Pull cord tension transmitting device using dual rack-pinion | Dec 7, 1994 | Issued |
Array
(
[id] => 3608226
[patent_doc_number] => 05613651
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-03-25
[patent_title] => 'Landing gear axle steering without walking beam'
[patent_app_type] => 1
[patent_app_number] => 8/352326
[patent_app_country] => US
[patent_app_date] => 1994-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 610
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/613/05613651.pdf
[firstpage_image] =>[orig_patent_app_number] => 352326
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/352326 | Landing gear axle steering without walking beam | Dec 7, 1994 | Issued |
Array
(
[id] => 3609181
[patent_doc_number] => 05593112
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-01-14
[patent_title] => 'Nacelle air pump for vector nozzles for aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/349844
[patent_app_country] => US
[patent_app_date] => 1994-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2160
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/593/05593112.pdf
[firstpage_image] =>[orig_patent_app_number] => 349844
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/349844 | Nacelle air pump for vector nozzles for aircraft | Dec 5, 1994 | Issued |
Array
(
[id] => 3586703
[patent_doc_number] => 05558298
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-09-24
[patent_title] => 'Active noise control of aircraft engine discrete tonal noise'
[patent_app_type] => 1
[patent_app_number] => 8/349285
[patent_app_country] => US
[patent_app_date] => 1994-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 3049
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 124
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/558/05558298.pdf
[firstpage_image] =>[orig_patent_app_number] => 349285
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/349285 | Active noise control of aircraft engine discrete tonal noise | Dec 4, 1994 | Issued |
| 08/350046 | METHOD OF CONTROLLING A PLURALITY OF SATELLITES | Nov 28, 1994 | Abandoned |
Array
(
[id] => 3503266
[patent_doc_number] => 05575441
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-11-19
[patent_title] => 'Fuel liquid/vapor vent containment/recovery system'
[patent_app_type] => 1
[patent_app_number] => 8/345182
[patent_app_country] => US
[patent_app_date] => 1994-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 1469
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 35
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/575/05575441.pdf
[firstpage_image] =>[orig_patent_app_number] => 345182
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/345182 | Fuel liquid/vapor vent containment/recovery system | Nov 27, 1994 | Issued |
Array
(
[id] => 3503254
[patent_doc_number] => 05575440
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-11-19
[patent_title] => 'Procedure and devices to determine the severity of icing conditions for an aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/348086
[patent_app_country] => US
[patent_app_date] => 1994-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2370
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/575/05575440.pdf
[firstpage_image] =>[orig_patent_app_number] => 348086
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/348086 | Procedure and devices to determine the severity of icing conditions for an aircraft | Nov 24, 1994 | Issued |
Array
(
[id] => 3503238
[patent_doc_number] => 05575439
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-11-19
[patent_title] => 'Fastening of a thermal insulation structure'
[patent_app_type] => 1
[patent_app_number] => 8/344112
[patent_app_country] => US
[patent_app_date] => 1994-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3051
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 267
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/575/05575439.pdf
[firstpage_image] =>[orig_patent_app_number] => 344112
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/344112 | Fastening of a thermal insulation structure | Nov 22, 1994 | Issued |
Array
(
[id] => 3645741
[patent_doc_number] => 05626310
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-05-06
[patent_title] => 'Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/342596
[patent_app_country] => US
[patent_app_date] => 1994-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 15
[patent_no_of_words] => 5578
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/626/05626310.pdf
[firstpage_image] =>[orig_patent_app_number] => 342596
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/342596 | Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft | Nov 20, 1994 | Issued |
Array
(
[id] => 3538738
[patent_doc_number] => 05547148
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-08-20
[patent_title] => 'Crashworthy landing gear'
[patent_app_type] => 1
[patent_app_number] => 8/341786
[patent_app_country] => US
[patent_app_date] => 1994-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 5103
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 349
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/547/05547148.pdf
[firstpage_image] =>[orig_patent_app_number] => 341786
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/341786 | Crashworthy landing gear | Nov 17, 1994 | Issued |