PL415537A1 - Release lever, preferably of the parachute rescue system - Google Patents

Release lever, preferably of the parachute rescue system

Info

Publication number
PL415537A1
PL415537A1 PL415537A PL41553715A PL415537A1 PL 415537 A1 PL415537 A1 PL 415537A1 PL 415537 A PL415537 A PL 415537A PL 41553715 A PL41553715 A PL 41553715A PL 415537 A1 PL415537 A1 PL 415537A1
Authority
PL
Poland
Prior art keywords
handle
console
rotary lever
rescue system
lever
Prior art date
Application number
PL415537A
Other languages
Polish (pl)
Other versions
PL229266B1 (en
Inventor
Rafał Ładziński
Original Assignee
Flaris Spółka Z Ograniczoną Odpowiedzialnością
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 Flaris Spółka Z Ograniczoną Odpowiedzialnością filed Critical Flaris Spółka Z Ograniczoną Odpowiedzialnością
Priority to PL415537A priority Critical patent/PL229266B1/en
Publication of PL415537A1 publication Critical patent/PL415537A1/en
Publication of PL229266B1 publication Critical patent/PL229266B1/en

Links

Landscapes

  • Emergency Lowering Means (AREA)

Abstract

Zgłoszenie dotyczy dźwigni wyzwalania, zwłaszcza spadochronowego systemu ratunkowego lekkiego samolotu, z silnikiem odrzutowym zamontowanym na kadłubie samolotu. Dźwignia wyzwalania zawierająca uchwyt (7), umieszczony w korpusie, mocowanym do struktury kadłuba w kabinie samolotu charakteryzuje się tym, że korpus składa się z konsoli (4) oraz z dźwigni obrotowej (5), odchylanej od pozycji spoczynku do pozycji pracy, zamocowanej w konsoli (4) obrotowo, przy czym konsola (4) mocowana jest do struktury kadłuba samolotu a wewnątrz dźwigni obrotowej (5) osadzony jest uchwyt (7), wystający poza dźwignię obrotową (5), przy czym uchwyt (7) jest zaopatrzony w mechanizm blokujący (3), uniemożliwiający wyciągnięcie uchwytu (7) z dźwigni obrotowej (5) przed jej odchyleniem z pozycji spoczynku do pozycji pracy.The notification relates to the trigger lever, in particular the lightweight parachute rescue system, with a jet engine mounted on the fuselage. The trigger lever containing the handle (7), located in the body, attached to the fuselage structure in the cabin of the aircraft is characterized by the fact that the body consists of a console (4) and a rotary lever (5), tiltable from rest position to work position, fixed in console (4) rotatably, the console (4) is attached to the fuselage structure and inside the rotary lever (5) there is a handle (7) protruding beyond the rotary lever (5), the handle (7) is equipped with a mechanism locking (3), preventing the handle (7) from being pulled out of the rotary lever (5) before it is moved from the rest position to the working position.

PL415537A 2015-12-23 2015-12-23 Release lever, preferably of the parachute rescue system PL229266B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL415537A PL229266B1 (en) 2015-12-23 2015-12-23 Release lever, preferably of the parachute rescue system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL415537A PL229266B1 (en) 2015-12-23 2015-12-23 Release lever, preferably of the parachute rescue system

Publications (2)

Publication Number Publication Date
PL415537A1 true PL415537A1 (en) 2017-07-03
PL229266B1 PL229266B1 (en) 2018-06-29

Family

ID=59201309

Family Applications (1)

Application Number Title Priority Date Filing Date
PL415537A PL229266B1 (en) 2015-12-23 2015-12-23 Release lever, preferably of the parachute rescue system

Country Status (1)

Country Link
PL (1) PL229266B1 (en)

Also Published As

Publication number Publication date
PL229266B1 (en) 2018-06-29

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