ES245113A1 - Improvements introduced in the commissioning of the landing of the aircraft (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements introduced in the commissioning of the landing of the aircraft (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES245113A1
ES245113A1 ES0245113A ES245113A ES245113A1 ES 245113 A1 ES245113 A1 ES 245113A1 ES 0245113 A ES0245113 A ES 0245113A ES 245113 A ES245113 A ES 245113A ES 245113 A1 ES245113 A1 ES 245113A1
Authority
ES
Spain
Prior art keywords
aircraft
landing
translation
machine
legally binding
Prior art date
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.)
Expired
Application number
ES0245113A
Other languages
Spanish (es)
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.)
GUERRA MARTA T
Original Assignee
GUERRA MARTA T
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by GUERRA MARTA T filed Critical GUERRA MARTA T
Priority to ES0245113A priority Critical patent/ES245113A1/en
Publication of ES245113A1 publication Critical patent/ES245113A1/en
Expired legal-status Critical Current

Links

Landscapes

  • Insulated Conductors (AREA)

Abstract

Improvements introduced in the start-up of the landing wheels of the aircraft, characterized in that it consists of electric motors, driven in a reverse way to that of ordinary electric motors; of which the portion to be rotated is the outside or surrounding, which will be housed inside the hub of the wheels of the landing gear and subject to the same hub; and the fixed portion is the internal or central part of the engines, it is also housed inside the hub and attached to the axis of the wheels of the landing gear of the aircraft. (Machine-translation by Google Translate, not legally binding)
ES0245113A 1958-11-06 1958-11-06 Improvements introduced in the commissioning of the landing of the aircraft (Machine-translation by Google Translate, not legally binding) Expired ES245113A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES0245113A ES245113A1 (en) 1958-11-06 1958-11-06 Improvements introduced in the commissioning of the landing of the aircraft (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES0245113A ES245113A1 (en) 1958-11-06 1958-11-06 Improvements introduced in the commissioning of the landing of the aircraft (Machine-translation by Google Translate, not legally binding)

Publications (1)

Publication Number Publication Date
ES245113A1 true ES245113A1 (en) 1959-02-16

Family

ID=34448472

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0245113A Expired ES245113A1 (en) 1958-11-06 1958-11-06 Improvements introduced in the commissioning of the landing of the aircraft (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES245113A1 (en)

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