PL415538A1 - Parachute rescue system - Google Patents

Parachute rescue system

Info

Publication number
PL415538A1
PL415538A1 PL415538A PL41553815A PL415538A1 PL 415538 A1 PL415538 A1 PL 415538A1 PL 415538 A PL415538 A PL 415538A PL 41553815 A PL41553815 A PL 41553815A PL 415538 A1 PL415538 A1 PL 415538A1
Authority
PL
Poland
Prior art keywords
parachute
aircraft
fuselage
cover
rescue system
Prior art date
Application number
PL415538A
Other languages
Polish (pl)
Other versions
PL229993B1 (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 PL415538A priority Critical patent/PL229993B1/en
Publication of PL415538A1 publication Critical patent/PL415538A1/en
Publication of PL229993B1 publication Critical patent/PL229993B1/en

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  • Emergency Lowering Means (AREA)
  • Toys (AREA)

Abstract

Zgłoszenie dotyczy spadochronowy system ratunkowy lekkiego samolotu z silnikiem odrzutowym zamontowanym na kadłubie. Spadochronowy system ratunkowy lekkiego samolotu z silnikiem odrzutowym (8), zamontowanym na kadłubie, zawierający spadochron w kadłubie samolotu (1), umieszczony w zasobniku (2) z pokrywą (9) oraz rakietę wyciągową (4) spadochronu, połączoną ze spadochronem, której zapalnik uruchamiany jest poprzez cięgno rakiety (5), połączone z uchwytem (6), zamocowanym w oprawie (7) wewnątrz samolotu charakteryzuje się tym, że zasobnik (2) ze spadochronem jest umieszczony w kadłubie samolotu (1) przed wlotem powietrza do silnika odrzutowego (8) i wyposażony jest od góry w otwieraną pokrywę (9), stanowiącą część poszycia kadłuba samolotu (1), osadzoną obrotowo na jej tylnej krawędzi (10) i mechanizm otwierania pokrywy (9), uruchamiany z wnętrza samolotu, przy czym na pokrywie (9) od wewnętrznej strony przymocowana jest rakieta wyciągowa (4) spadochronu.The application concerns a parachute rescue system of a light aircraft with a jet engine mounted on the fuselage. Parachute rescue system of a light aircraft with a jet engine (8), mounted on the fuselage, containing a parachute in the aircraft fuselage (1), placed in the container (2) with a cover (9) and an exhaust rocket (4) of the parachute, combined with a parachute it is activated by a rocket cable (5), connected to the handle (6), mounted in the housing (7) inside the aircraft, characterized by the fact that the container (2) with the parachute is placed in the fuselage (1) in front of the air inlet to the jet engine ( 8) and is equipped from the top with an opening cover (9), which is part of the aircraft fuselage (1), rotatably mounted on its rear edge (10) and a cover opening mechanism (9), activated from the inside of the aircraft, with the cover ( 9) from the inside a parachute hoist (4) is attached.

PL415538A 2015-12-23 2015-12-23 Parachute rescue system PL229993B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL415538A PL229993B1 (en) 2015-12-23 2015-12-23 Parachute rescue system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL415538A PL229993B1 (en) 2015-12-23 2015-12-23 Parachute rescue system

Publications (2)

Publication Number Publication Date
PL415538A1 true PL415538A1 (en) 2017-07-03
PL229993B1 PL229993B1 (en) 2018-09-28

Family

ID=59201326

Family Applications (1)

Application Number Title Priority Date Filing Date
PL415538A PL229993B1 (en) 2015-12-23 2015-12-23 Parachute rescue system

Country Status (1)

Country Link
PL (1) PL229993B1 (en)

Also Published As

Publication number Publication date
PL229993B1 (en) 2018-09-28

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