ES223446A1 - A control device for the vertical landing of aircraft or aerodines (Machine-translation by Google Translate, not legally binding)
- Google Patents
A control device for the vertical landing of aircraft or aerodines (Machine-translation by Google Translate, not legally binding)
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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Publication date
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SASfiledCriticalSociete Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of ES223446A1publicationCriticalpatent/ES223446A1/en
Aircraft and aerodyne vertical landing control device, equipped with an altitude detector, a detector of the variation of the altitude as a function of time, that is to say of the descent speed, as well as a comparator of the values of the altitude and speed, allowing to verify this comparator if the values of altitude and speed vary, following the law that has been set to obtain at the landing a zero or limited speed. (Machine-translation by Google Translate, not legally binding)
ES0223446A1954-08-111955-08-10A control device for the vertical landing of aircraft or aerodines (Machine-translation by Google Translate, not legally binding)
ExpiredES223446A1
(en)