Stepped instrument panel for aircraft
AssigneeAirbus Helicopters
InventorAndré Barbieri
Life of this patent
Estimating the term…
Abstract
An instrument panel for a rotorcraft having two pilot seats, said instrument panel being arranged under an anti-glare shield (4) and including display means (2), at least some of the display means (2) being suitable for acting as communications means, said display means (2) comprising a first set (5) of display means (2) arranged on the instrument panel, and a second set (6) of display means (2) arranged on the instrument panel, wherein the instrument panel includes, symmetrically relative to a longitudinal axis, a central dashboard (3), and at least two lateral dashboards arranged on either side of the central dashboard (3), the dashboards being mutually parallel and presenting a forward longitudinal offset from one dashboard to the next starting from the central dashboard (3).
Claims18
An instrument panel for a rotorcraft having two pilot seats side by side, one forming a first piloting position and the other forming a second piloting position, said instrument panel including at least three multifunction display screens, including a first multifunction display screen for the first piloting position, a second multifunction display screen for the second piloting position, and a common multifunction display screen between the first and second multifunction display screens, the instrument panel having a bottom portion, a top portion, and a central axis extending from the bottom portion to the top portion, wherein the instrument panel possesses a rigid, one-piece frame, the frame comprising, transversely on either side of the central axis, a central dashboard including the common multifunction display screen, at least two lateral dashboards disposed on either side of the central dashboard, the central and lateral dashboards being substantially symmetrically arranged relative to the central axis of the instrument panel, said central dashboard being in one piece with the at least two lateral dashboards and being separated from the lateral dashboards by longitudinal sidewalls, one longitudinal sidewall extending from the lateral dashboard including the first multifunction display screen and towards the first piloting position;
- another longitudinal sidewall extending from the lateral dashboard including the second multifunction display screen and toward the second piloting position, said central and lateral dashboards being substantially mutually parallel and presenting a longitudinal offset in a forward direction from said central dashboard relative to each lateral dashboard, said offset having a predefined value of at least 30 mm and being identical between adjacent dashboards across the instrument panel.
A rotorcraft instrument panel comprising:
- a first dashboard having a first multifunction display facing in a first direction and extending in a first plane, the first dashboard having a central axis extending from a top portion of the first dashboard to a bottom portion of the first dashboard;
- a second dashboard proximate the first dashboard on a first side of the central axis and a third dashboard proximate the first dashboard on a second side of the central axis, the second dashboard having a second multifunction display facing in the first direction and the third dashboard having a third multifunction display facing in the first direction, the second and third dashboards being coplanar with each other and extending in a second plane spaced a first distance from the first plane in a second direction opposite the first direction;
- a fourth dashboard on the first side of the central axis proximate the second dashboard and a fifth dashboard on the second side of the central axis proximate the third dashboard, the fourth dashboard having a fourth multifunction display facing in the first direction and the fifth dashboard having a fifth multifunction display facing in the first direction, the fourth and fifth dashboards being coplanar with each other and extending in a third plane spaced a second distance from the first plane in the second direction, the second distance being greater than the first distance;
- and
- a common sidewall having a first portion extending along the first side of the central axis and a second portion extending along the second side of the central axis, the first portion extending from a periphery of the first dashboard in the second direction to connect to a periphery of the second dashboard and extending from the periphery of the second dashboard in the second direction to connect to a periphery of the fourth dashboard and the second portion extending from the periphery of the first dashboard in the second direction to connect to a periphery of the third dashboard and extending from the periphery of the third dashboard in the second direction to connect to a periphery of the fifth dashboard, wherein the first, second, third, fourth, and fifth dashboards and the common sidewall are an integral unit and the first, second, third, fourth, and fifth dashboards are symmetrically arranged relative to the central axis.
A rotorcraft comprising:
- first and second pilot seats in a side by side configuration;
- and
- a display panel comprising an integral frame defining first, second, third, fourth, and fifth dashboards, the first dashboard being positioned between the second and third dashboards and having a first display facing a first direction and extending in a first plane, the second dashboard having a second display facing the first pilot seat and extending in a second plane, and the third dashboard having a third display facing the second pilot seat and extending in a third plane, the second and third planes defining a first angle relative to the first plane;
- the first, second, and third dashboards being positioned between the fourth and fifth dashboards, the fourth dashboard having a fourth display facing the first pilot seat and extending in a fourth plane, the fifth dashboard having a fifth display facing the second pilot seat and extending in a fifth plane, the fourth and fifth planes defining a second angle relative to the first plane, the integral frame further including a first common sidewall portion extending at least 30 mm from a periphery of the fourth dashboard in the first direction to connect to a periphery of the second dashboard and extending at least 30 mm from the periphery of the second dashboard in the first direction to connect to a periphery of the first dashboard, and a second common sidewall portion extending at least 30 mm from a periphery of the fifth dashboard in the first direction to connect to a periphery of the third dashboard and extending at least 30 mm from the periphery of the third dashboard in the first direction to connect to the periphery of the first dashboard.
Dependencies are inferred from the claim text.