ES41379U - Improved aircraft model (Machine-translation by Google Translate, not legally binding) - Google Patents

Improved aircraft model (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES41379U
ES41379U ES0041379U ES41379U ES41379U ES 41379 U ES41379 U ES 41379U ES 0041379 U ES0041379 U ES 0041379U ES 41379 U ES41379 U ES 41379U ES 41379 U ES41379 U ES 41379U
Authority
ES
Spain
Prior art keywords
translation
machine
legally binding
google translate
aircraft model
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.)
Granted
Application number
ES0041379U
Other languages
Spanish (es)
Other versions
ES41379Y (en
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to ES0041379U priority Critical patent/ES41379Y/en
Publication of ES41379U publication Critical patent/ES41379U/en
Application granted granted Critical
Publication of ES41379Y publication Critical patent/ES41379Y/en
Expired legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

An improved model aircraft, characterized in that it has a force transmission from an electric motor, constituted by a wire, that is inserted in a bushing at one of its ends, serving at the same time as a helical spring. welded by one of its ends to said bushing, being arranged on the other end of the wire mentioned another bushing similar to the previous one, to which the other end of the said spring is welded, both bushings being able to rotate on said wire. (Machine-translation by Google Translate, not legally binding)
ES0041379U 1954-04-06 1954-04-06 Perfected model aircraft Expired ES41379Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES0041379U ES41379Y (en) 1954-04-06 1954-04-06 Perfected model aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES0041379U ES41379Y (en) 1954-04-06 1954-04-06 Perfected model aircraft

Publications (2)

Publication Number Publication Date
ES41379U true ES41379U (en) 1954-06-01
ES41379Y ES41379Y (en) 1956-08-01

Family

ID=51104700

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0041379U Expired ES41379Y (en) 1954-04-06 1954-04-06 Perfected model aircraft

Country Status (1)

Country Link
ES (1) ES41379Y (en)

Also Published As

Publication number Publication date
ES41379Y (en) 1956-08-01

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