Search

Mohammad I. Yusuf

Examiner (ID: 10292, Phone: (571)270-7487 , Office: P/3725 )

Most Active Art Unit
3725
Art Unit(s)
4177, 3725
Total Applications
383
Issued Applications
264
Pending Applications
0
Abandoned Applications
121

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 16436717 [patent_doc_number] => 20200354043 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-12 [patent_title] => FOLDING MAIN LANDING GEAR FOR CARGO AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/405789 [patent_app_country] => US [patent_app_date] => 2019-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4338 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16405789 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/405789
Folding main landing gear for cargo aircraft May 6, 2019 Issued
Array ( [id] => 16436715 [patent_doc_number] => 20200354041 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-12 [patent_title] => BIPEDAL NOSE LANDING GEAR FOR CARGO AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/405781 [patent_app_country] => US [patent_app_date] => 2019-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3693 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16405781 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/405781
Bipedal nose landing gear for cargo aircraft May 6, 2019 Issued
Array ( [id] => 15022711 [patent_doc_number] => 20190322360 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-10-24 [patent_title] => AIRCRAFT UNDERCARRIAGE HAVING A STEERABLE BOTTOM PORTION, AND A SIMPLIFIED STEERING DEVICE [patent_app_type] => utility [patent_app_number] => 16/387188 [patent_app_country] => US [patent_app_date] => 2019-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2060 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16387188 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/387188
AIRCRAFT UNDERCARRIAGE HAVING A STEERABLE BOTTOM PORTION, AND A SIMPLIFIED STEERING DEVICE Apr 16, 2019 Pending
Array ( [id] => 14993007 [patent_doc_number] => 20190315461 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-10-17 [patent_title] => ROTARY-WINGED VEHICLE SYSTEMS AND DEVICES [patent_app_type] => utility [patent_app_number] => 16/383513 [patent_app_country] => US [patent_app_date] => 2019-04-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8906 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 56 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16383513 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/383513
ROTARY-WINGED VEHICLE SYSTEMS AND DEVICES Apr 11, 2019 Abandoned
Array ( [id] => 16237931 [patent_doc_number] => 20200255165 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-08-13 [patent_title] => SPACECRAFT CONTROL USING RESIDUAL DIPOLE [patent_app_type] => utility [patent_app_number] => 16/273837 [patent_app_country] => US [patent_app_date] => 2019-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7965 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 70 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16273837 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/273837
Spacecraft control using residual dipole Feb 11, 2019 Issued
Array ( [id] => 16222416 [patent_doc_number] => 20200247532 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-08-06 [patent_title] => DOOR ALIGNMENT FOR AIRCRAFT LANDING GEAR [patent_app_type] => utility [patent_app_number] => 16/264439 [patent_app_country] => US [patent_app_date] => 2019-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5424 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 141 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16264439 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/264439
Door alignment for aircraft landing gear Jan 30, 2019 Issued
Array ( [id] => 14807803 [patent_doc_number] => 20190270511 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-09-05 [patent_title] => EMA THERMAL MANAGEMENT OPTIMIZATION [patent_app_type] => utility [patent_app_number] => 16/221900 [patent_app_country] => US [patent_app_date] => 2018-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3458 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16221900 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/221900
EMA thermal management optimization Dec 16, 2018 Issued
Array ( [id] => 16719746 [patent_doc_number] => 20210086893 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-03-25 [patent_title] => CONVERTIPLANE [patent_app_type] => utility [patent_app_number] => 16/971750 [patent_app_country] => US [patent_app_date] => 2018-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1670 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16971750 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/971750
CONVERTIPLANE Dec 16, 2018 Abandoned
Array ( [id] => 17250890 [patent_doc_number] => 11186362 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-11-30 [patent_title] => Brake systems for aircraft and related methods [patent_app_type] => utility [patent_app_number] => 16/222633 [patent_app_country] => US [patent_app_date] => 2018-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 35 [patent_no_of_words] => 19927 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16222633 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/222633
Brake systems for aircraft and related methods Dec 16, 2018 Issued
Array ( [id] => 16687960 [patent_doc_number] => 20210070436 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-03-11 [patent_title] => MODULAR AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/772213 [patent_app_country] => US [patent_app_date] => 2018-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 12953 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16772213 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/772213
Modular aircraft Dec 12, 2018 Issued
Array ( [id] => 16436724 [patent_doc_number] => 20200354050 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-12 [patent_title] => CONVERTIPLANE [patent_app_type] => utility [patent_app_number] => 16/765950 [patent_app_country] => US [patent_app_date] => 2018-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1516 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16765950 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/765950
CONVERTIPLANE Nov 20, 2018 Abandoned
Array ( [id] => 17769103 [patent_doc_number] => 11401027 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-08-02 [patent_title] => Morphing wing [patent_app_type] => utility [patent_app_number] => 16/605621 [patent_app_country] => US [patent_app_date] => 2018-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 6805 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16605621 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/605621
Morphing wing Sep 16, 2018 Issued
Array ( [id] => 16176556 [patent_doc_number] => 20200223524 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-07-16 [patent_title] => AIRCRAFT COMPRISING AN IMPROVED FUSELAGE [patent_app_type] => utility [patent_app_number] => 16/647206 [patent_app_country] => US [patent_app_date] => 2018-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2798 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16647206 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/647206
AIRCRAFT COMPRISING AN IMPROVED FUSELAGE Sep 13, 2018 Abandoned
Array ( [id] => 15680575 [patent_doc_number] => 20200094951 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-03-26 [patent_title] => ROTOR WING AIRCRAFT WITH PROPULSION APPARATUS ON ROTATING POLE [patent_app_type] => utility [patent_app_number] => 16/483928 [patent_app_country] => US [patent_app_date] => 2018-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3290 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16483928 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/483928
Rotor wing aircraft with propulsion apparatus on rotating pole Aug 2, 2018 Issued
Array ( [id] => 18102157 [patent_doc_number] => 11542031 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-01-03 [patent_title] => Fuel tank communication systems [patent_app_type] => utility [patent_app_number] => 16/629702 [patent_app_country] => US [patent_app_date] => 2018-07-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 2308 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16629702 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/629702
Fuel tank communication systems Jul 10, 2018 Issued
Array ( [id] => 17184911 [patent_doc_number] => 20210331796 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-10-28 [patent_title] => AMPHIBIOUS, PRESSURIZABLE AND LOW NOISE TWIN-ENGINE AIRCRAFT CONFIGURATION [patent_app_type] => utility [patent_app_number] => 16/613896 [patent_app_country] => US [patent_app_date] => 2018-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4226 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16613896 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/613896
AMPHIBIOUS, PRESSURIZABLE AND LOW NOISE TWIN-ENGINE AIRCRAFT CONFIGURATION Apr 23, 2018 Abandoned
Array ( [id] => 15556019 [patent_doc_number] => 20200062421 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-02-27 [patent_title] => METHOD FOR LANDING A TETHERED AIRCRAFT AND LAUNCH AND LAND SYSTEM [patent_app_type] => utility [patent_app_number] => 16/500206 [patent_app_country] => US [patent_app_date] => 2018-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3870 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16500206 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/500206
METHOD FOR LANDING A TETHERED AIRCRAFT AND LAUNCH AND LAND SYSTEM Apr 10, 2018 Abandoned
Array ( [id] => 15253523 [patent_doc_number] => 20190375495 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-12-12 [patent_title] => ELECTRICAL VERTICAL TAKE-OFF AND LANDING AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/463702 [patent_app_country] => US [patent_app_date] => 2017-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4466 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16463702 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/463702
ELECTRICAL VERTICAL TAKE-OFF AND LANDING AIRCRAFT Nov 26, 2017 Abandoned
Array ( [id] => 18216171 [patent_doc_number] => 11591090 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-02-28 [patent_title] => Mini suite emergency egress solutions [patent_app_type] => utility [patent_app_number] => 16/349636 [patent_app_country] => US [patent_app_date] => 2017-11-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 50 [patent_no_of_words] => 8626 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 313 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16349636 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/349636
Mini suite emergency egress solutions Nov 14, 2017 Issued
Array ( [id] => 18620109 [patent_doc_number] => 11753135 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-09-12 [patent_title] => Method for transporting a payload to a target location, and related hybrid airship [patent_app_type] => utility [patent_app_number] => 16/763602 [patent_app_country] => US [patent_app_date] => 2017-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 12 [patent_no_of_words] => 5553 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 287 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16763602 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/763602
Method for transporting a payload to a target location, and related hybrid airship Nov 12, 2017 Issued
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