ES283128U - Safety system for aircraft and helicopters in flight (Machine-translation by Google Translate, not legally binding) - Google Patents

Safety system for aircraft and helicopters in flight (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES283128U
ES283128U ES1984283128U ES283128U ES283128U ES 283128 U ES283128 U ES 283128U ES 1984283128 U ES1984283128 U ES 1984283128U ES 283128 U ES283128 U ES 283128U ES 283128 U ES283128 U ES 283128U
Authority
ES
Spain
Prior art keywords
helicopters
flight
aircraft
translation
machine
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
ES1984283128U
Other languages
Spanish (es)
Other versions
ES283128Y (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.)
MAGAZ MARCOS BERNARDO
Original Assignee
MAGAZ MARCOS BERNARDO
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 MAGAZ MARCOS BERNARDO filed Critical MAGAZ MARCOS BERNARDO
Priority to ES1984283128U priority Critical patent/ES283128Y/en
Publication of ES283128U publication Critical patent/ES283128U/en
Application granted granted Critical
Publication of ES283128Y publication Critical patent/ES283128Y/en
Expired legal-status Critical Current

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Abstract

Installation of security for airplanes and helicopters in flight, which aiming to control the fall of the aircraft in an emergency situation, is essentially characterized by the provision of parachute-type aerodynamic brakes, conveniently housed in receptacles established within the fuselage of the apparatus or externally attached thereto, said aerodynamic brakes being operable manually with the collaboration of a microprocessor that causes activation in the presence of a series of conditions duly established for that purpose. (Machine-translation by Google Translate, not legally binding)
ES1984283128U 1984-12-03 1984-12-03 SAFETY SYSTEM FOR AIRCRAFT AND HELICOPTERS IN FLIGHT Expired ES283128Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES1984283128U ES283128Y (en) 1984-12-03 1984-12-03 SAFETY SYSTEM FOR AIRCRAFT AND HELICOPTERS IN FLIGHT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES1984283128U ES283128Y (en) 1984-12-03 1984-12-03 SAFETY SYSTEM FOR AIRCRAFT AND HELICOPTERS IN FLIGHT

Publications (2)

Publication Number Publication Date
ES283128U true ES283128U (en) 1985-11-01
ES283128Y ES283128Y (en) 1986-05-16

Family

ID=8433247

Family Applications (1)

Application Number Title Priority Date Filing Date
ES1984283128U Expired ES283128Y (en) 1984-12-03 1984-12-03 SAFETY SYSTEM FOR AIRCRAFT AND HELICOPTERS IN FLIGHT

Country Status (1)

Country Link
ES (1) ES283128Y (en)

Also Published As

Publication number Publication date
ES283128Y (en) 1986-05-16

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Legal Events

Date Code Title Description
FD1K Utility model lapsed

Effective date: 19970612