
Raymond Alejandro
Examiner (ID: 18678, Phone: (571)272-1282 , Office: P/1727 )
| Most Active Art Unit | 1727 |
| Art Unit(s) | 1795, 1727, 1752, 1745 |
| Total Applications | 2441 |
| Issued Applications | 1740 |
| Pending Applications | 256 |
| Abandoned Applications | 490 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10459126
[patent_doc_number] => 20150344141
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-03
[patent_title] => 'FILTERS FOR AIRCRAFT ENGINE INLETS'
[patent_app_type] => utility
[patent_app_number] => 14/292248
[patent_app_country] => US
[patent_app_date] => 2014-05-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3423
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14292248
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/292248 | Filters for aircraft engine inlets | May 29, 2014 | Issued |
Array
(
[id] => 10389271
[patent_doc_number] => 20150274278
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'OVER-FRAME BLANKET ASSEMBLIES AND METHODS OF INSTALLATION IN FUSELAGE ASSEMBLIES'
[patent_app_type] => utility
[patent_app_number] => 14/290018
[patent_app_country] => US
[patent_app_date] => 2014-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4178
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14290018
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/290018 | Over-frame blanket assemblies and methods of installation in fuselage assemblies | May 28, 2014 | Issued |
Array
(
[id] => 11428768
[patent_doc_number] => 09567076
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-02-14
[patent_title] => 'Unmanned aerial vehicle and fuselage thereof and method for manufacturing the fuselage'
[patent_app_type] => utility
[patent_app_number] => 14/418481
[patent_app_country] => US
[patent_app_date] => 2014-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 20
[patent_no_of_words] => 5530
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14418481
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/418481 | Unmanned aerial vehicle and fuselage thereof and method for manufacturing the fuselage | May 21, 2014 | Issued |
Array
(
[id] => 11858704
[patent_doc_number] => 09738376
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-08-22
[patent_title] => 'Landing gear drive systems'
[patent_app_type] => utility
[patent_app_number] => 14/274083
[patent_app_country] => US
[patent_app_date] => 2014-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 25
[patent_no_of_words] => 5779
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14274083
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/274083 | Landing gear drive systems | May 8, 2014 | Issued |
Array
(
[id] => 10436743
[patent_doc_number] => 20150321754
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-12
[patent_title] => 'Coaxial Counter-Rotating Unmanned Helicopter'
[patent_app_type] => utility
[patent_app_number] => 14/272839
[patent_app_country] => US
[patent_app_date] => 2014-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6490
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14272839
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/272839 | Coaxial counter-rotating unmanned helicopter | May 7, 2014 | Issued |
Array
(
[id] => 9728134
[patent_doc_number] => 20140263840
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'Methods and Systems for Mass Distribution of Supply Packs'
[patent_app_type] => utility
[patent_app_number] => 14/267766
[patent_app_country] => US
[patent_app_date] => 2014-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 31
[patent_figures_cnt] => 31
[patent_no_of_words] => 14795
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14267766
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/267766 | Methods and systems for mass distribution of supply packs | Apr 30, 2014 | Issued |
Array
(
[id] => 10813326
[patent_doc_number] => 20160159486
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-09
[patent_title] => 'A STRUCTURE FOR SUSPENDING A TURBOPROP HAVING TWO UNDUCTED PROPELLERS ON A STRUCTURAL ELEMENT OF AN AIRPLANE'
[patent_app_type] => utility
[patent_app_number] => 14/786500
[patent_app_country] => US
[patent_app_date] => 2014-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2173
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14786500
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/786500 | Structure for suspending a turboprop having two unducted propellers on a structural element of an airplane | Apr 23, 2014 | Issued |
Array
(
[id] => 11773183
[patent_doc_number] => 09382009
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-05
[patent_title] => 'Relief valve for being arranged on an opening of a fuselage shell of an aircraft, fuselage part with such a relief valve and aircraft fuselage'
[patent_app_type] => utility
[patent_app_number] => 14/259753
[patent_app_country] => US
[patent_app_date] => 2014-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 15
[patent_no_of_words] => 6599
[patent_no_of_claims] => 7
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14259753
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/259753 | Relief valve for being arranged on an opening of a fuselage shell of an aircraft, fuselage part with such a relief valve and aircraft fuselage | Apr 22, 2014 | Issued |
Array
(
[id] => 9698464
[patent_doc_number] => 20140248149
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'ROTOR/WING AIRCRAFT INCLUDING VECTORABLE NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 14/258003
[patent_app_country] => US
[patent_app_date] => 2014-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 5170
[patent_no_of_claims] => 16
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14258003
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/258003 | Rotor/wing aircraft including vectorable nozzle | Apr 20, 2014 | Issued |
Array
(
[id] => 10909159
[patent_doc_number] => 20140312174
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'WING TIP SHAPE FOR A WING, IN PARTICULAR OF AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/252173
[patent_app_country] => US
[patent_app_date] => 2014-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3510
[patent_no_of_claims] => 18
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14252173
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/252173 | Wing tip shape for a wing, in particular of aircraft | Apr 13, 2014 | Issued |
Array
(
[id] => 9632128
[patent_doc_number] => 20140210235
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-31
[patent_title] => 'SEATING SYSTEM AND A PASSENGER ACCOMMODATION UNIT FOR A VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 14/250894
[patent_app_country] => US
[patent_app_date] => 2014-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 40
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[patent_no_of_words] => 31732
[patent_no_of_claims] => 19
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14250894
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/250894 | SEATING SYSTEM AND A PASSENGER ACCOMMODATION UNIT FOR A VEHICLE | Apr 10, 2014 | Abandoned |
Array
(
[id] => 10399073
[patent_doc_number] => 20150284081
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-08
[patent_title] => 'Helicopter Equipment Mounting Post'
[patent_app_type] => utility
[patent_app_number] => 14/248070
[patent_app_country] => US
[patent_app_date] => 2014-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3465
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14248070
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/248070 | Helicopter equipment mounting post | Apr 7, 2014 | Issued |
Array
(
[id] => 10389315
[patent_doc_number] => 20150274322
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'EMERGENCY LANDING APPARATUS FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/228880
[patent_app_country] => US
[patent_app_date] => 2014-03-28
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14228880
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/228880 | EMERGENCY LANDING APPARATUS FOR AIRCRAFT | Mar 27, 2014 | |
Array
(
[id] => 10381564
[patent_doc_number] => 20150266571
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-24
[patent_title] => 'AERODYNAMICALLY EFFICIENT LIGHTWEIGHT VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH PIVOTING ROTORS AND STOWING ROTOR BLADES'
[patent_app_type] => utility
[patent_app_number] => 14/218845
[patent_app_country] => US
[patent_app_date] => 2014-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 31
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[patent_no_of_words] => 5903
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14218845
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/218845 | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | Mar 17, 2014 | Issued |
Array
(
[id] => 11528270
[patent_doc_number] => 20170088247
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-30
[patent_title] => 'ARMORED WINDOW'
[patent_app_type] => utility
[patent_app_number] => 15/126923
[patent_app_country] => US
[patent_app_date] => 2014-03-18
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15126923
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/126923 | ARMORED WINDOW | Mar 17, 2014 | Abandoned |
Array
(
[id] => 10979573
[patent_doc_number] => 20160176517
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-23
[patent_title] => 'COCKPIT CONTROL SYSTEM FOR CONTROLLING GROUND TRAVEL IN AIRCRAFT EQUIPPED WITH ENGINE-FREE ELECTRIC TAXI SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/775342
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[patent_app_date] => 2014-03-14
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14775342
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/775342 | Cockpit control system for controlling ground travel in aircraft equipped with engine-free electric taxi system | Mar 13, 2014 | Issued |
Array
(
[id] => 10693376
[patent_doc_number] => 20160039522
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-11
[patent_title] => 'Aircraft Lavatory Unit'
[patent_app_type] => utility
[patent_app_number] => 14/776573
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/776573 | Aircraft Lavatory Unit | Mar 11, 2014 | Abandoned |
Array
(
[id] => 9564477
[patent_doc_number] => 20140182190
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[patent_kind] => A1
[patent_issue_date] => 2014-07-03
[patent_title] => 'Lure fishing assembly with weighted wireform'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/999509 | Lure fishing assembly with weighted wireform | Mar 4, 2014 | Issued |
Array
(
[id] => 10614625
[patent_doc_number] => 09334055
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[patent_kind] => B2
[patent_issue_date] => 2016-05-10
[patent_title] => 'Method and apparatus for attaching a trim to a cover of a bin assembly'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/186048 | Method and apparatus for attaching a trim to a cover of a bin assembly | Feb 20, 2014 | Issued |
Array
(
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[patent_title] => 'LINE TRANSFER SYSTEM FOR AIRPLANE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/179291 | Line transfer system for airplane | Feb 11, 2014 | Issued |