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PL442960A1 - Safety system for aircraft with mechanical control system - Google Patents

Safety system for aircraft with mechanical control system Download PDF

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Publication number
PL442960A1
PL442960A1 PL442960A PL44296022A PL442960A1 PL 442960 A1 PL442960 A1 PL 442960A1 PL 442960 A PL442960 A PL 442960A PL 44296022 A PL44296022 A PL 44296022A PL 442960 A1 PL442960 A1 PL 442960A1
Authority
PL
Poland
Prior art keywords
aircraft
output
input
mechanical control
actuator
Prior art date
Application number
PL442960A
Other languages
Polish (pl)
Other versions
PL246555B1 (en
Inventor
Tomasz Rogalski
Andrzej Włoch
Andrzej Wal
Jacek Prusik
Original Assignee
Politechnika Rzeszowska im. Ignacego Łukasiewicza
Podkarpackie Centrum Innowacji 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 Politechnika Rzeszowska im. Ignacego Łukasiewicza, Podkarpackie Centrum Innowacji Spółka Z Ograniczoną Odpowiedzialnością filed Critical Politechnika Rzeszowska im. Ignacego Łukasiewicza
Priority to PL442960A priority Critical patent/PL246555B1/en
Publication of PL442960A1 publication Critical patent/PL442960A1/en
Publication of PL246555B1 publication Critical patent/PL246555B1/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/08—Trimming zero positions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/343—Transmitting means without power amplification or where power amplification is irrelevant mechanical overriding of personal controls; with automatic return to inoperative position

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Regulating Braking Force (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

Układ zabezpieczający dla samolotów z mechanicznym układem sterowania zawiera co najmniej dwa siłowniki (1) oraz układ analizujący (2). Co najmniej jeden siłownik (1) jest w kanale steru wysokości (3), a jego wyjście połączone jest z wejściem wolantu (5) samolotu, a co najmniej drugi siłownik (1) jest w kanale steru kierunku (4), a jego wyście połączone jest z wejściem orczyka (6). Wejście układu analizującego (2) połączone jest z wyjściem co najmniej jednego czujnika pokładowego albo wyjściem instalacji ciśnieniowego pomiaru prędkości (7) albo układ analizujący (2) ma układ pomiarowy, którego wejście połączone jest z instalacją ciśnienia całkowitego i statycznego samolotu. Wyjścia układu analizującego (2) połączone są z wejściami siłowników (1).The safety system for aircraft with a mechanical control system includes at least two actuators (1) and an analyzing system (2). At least one actuator (1) is in the elevator channel (3), and its output is connected to the input of the yoke (5) of the aircraft, and at least the second actuator (1) is in the rudder channel (4), and its output is connected is with the T-bar input (6). The input of the analyzing system (2) is connected to the output of at least one on-board sensor or the output of the pressure speed measurement installation (7), or the analyzing system (2) has a measurement system whose input is connected to the aircraft's total and static pressure installation. The outputs of the analyzing system (2) are connected to the actuator inputs (1).

PL442960A 2022-11-26 2022-11-26 Safety system for aircraft with mechanical control system PL246555B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL442960A PL246555B1 (en) 2022-11-26 2022-11-26 Safety system for aircraft with mechanical control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL442960A PL246555B1 (en) 2022-11-26 2022-11-26 Safety system for aircraft with mechanical control system

Publications (2)

Publication Number Publication Date
PL442960A1 true PL442960A1 (en) 2024-05-27
PL246555B1 PL246555B1 (en) 2025-02-10

Family

ID=91227515

Family Applications (1)

Application Number Title Priority Date Filing Date
PL442960A PL246555B1 (en) 2022-11-26 2022-11-26 Safety system for aircraft with mechanical control system

Country Status (1)

Country Link
PL (1) PL246555B1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170060141A1 (en) * 2015-08-31 2017-03-02 The Boeing Company Aircraft stall protection system
GB2586900A (en) * 2019-09-09 2021-03-10 Paul Robinson Nicholas Flight control system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170060141A1 (en) * 2015-08-31 2017-03-02 The Boeing Company Aircraft stall protection system
GB2586900A (en) * 2019-09-09 2021-03-10 Paul Robinson Nicholas Flight control system

Also Published As

Publication number Publication date
PL246555B1 (en) 2025-02-10

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