Crespo Pena; Soledad

Patent Applications and Registrations

Patent applications and USPTO patent grants for Crespo Pena; Soledad.The latest application filed is for "lifting surface".

Company Profile

1.8.9

Crespo Pena; Soledad - Getafe ES
Crespo Pena; Soledad - Madrid ES
Crespo Pena; Soledad - GETAFE Madrid

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Lifting surface Grant 11,052,996 - Garcia Nieto , et al. July 6, 2	2021-07-06
Aircraft airfoil having a stitched trailing edge and manufacturing method thereof Grant 10,953,624 - Crespo Pena , et al. March 23, 2	2021-03-23
Lifting surface Grant 10,906,631 - Garcia Nieto , et al. February 2, 2	2021-02-02
Thermoplastic moulded injected tip structure for an aircraft Grant 10,745,105 - Crespo Pena , et al. A	2020-08-18
Leading edge with laminar flow control and manufacturing method thereof Grant 10,532,807 - Garcia Nieto , et al. Ja	2020-01-14
Integrated detachable ballistic shield Grant 10,414,497 - Velez De Mendizabal Alonso , et al. Sept	2019-09-17
Method, injection moulding tool for manufacturing a leading edge section with hybrid laminar flow control for an aircraft, and leading edge section with hybrid laminar flow control obtained thereof Grant 10,377,464 - Cebolla Garrofe , et al. A	2019-08-13
Multi-spar torsion box structure Grant 10,239,602 - Garcia Nieto , et al.	2019-03-26
Lifting Surface App 20180201360 - GARC A NIETO; Carlos ; et al.	2018-07-19
Lifting Surface App 20180201361 - GARC A NIETO; Carlos ; et al.	2018-07-19
Integrated Detachable Ballistic Shield App 20180072423 - VELEZ DE MENDIZ BAL ALONSO; Iker ; et al.	2018-03-15
Thermoplastic Moulded Injected Tip Structure For An Aircraft App 20180022438 - Crespo Pena; Soledad ; et al.	2018-01-25
Method, Injection Moulding Tool For Manufacturing A Leading Edge Section With Hybrid Laminar Flow Control For An Aircraft, And Leading Edge Section With Hybrid Laminar Flow Control Obtained Thereof App 20170259903 - CEBOLLA GARROFE; Pablo ; et al.	2017-09-14
Aircraft Aerodynamic Surface With A Detachable Leading Edge App 20170259902 - Cebolla Garrofe; Pablo ; et al.	2017-09-14
Aircraft Airfoil Having A Stitched Trailing Edge And Manufacturing Method Thereof App 20170246833 - Crespo Pena; Soledad ; et al.	2017-08-31
Leading Edge With Laminar Flow Control And Manufacturing Method Thereof App 20170197706 - Garcia Nieto; Carlos ; et al.	2017-07-13
Multi-spar Torsion Box Structure App 20160340022 - Garcia Nieto; Carlos ; et al.	2016-11-24

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