公开(公告)号：US09981732B2

公开(公告)日：2018-05-29

申请号：US14900973

申请日：2014-07-11

Applicant: LEARJET INC. ,  C&D ZODIAC INC.

Inventor： William A. Goings ,  Eric Long

IPC: B64C1/14 ,  B64D11/00 ,  B64D11/02 ,  E05F11/54

CPC classification number: B64C1/14 ,  B64D11/0023 ,  B64D11/02 ,  E05F11/54 ,  E05Y2900/502

Abstract: A door for an aircraft includes a first panel divisible into at least two first slats that are releasably connected to one another, a first tensioning cable attached between the at least two first slats, and a first tensioner connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.

公开(公告)号：US09873503B2

公开(公告)日：2018-01-23

申请号：US14906605

申请日：2014-07-21

Applicant: LEARJET INC.

Inventor： Reuben Chandrasekharan ,  Nick Iarocci ,  Shermineh Vafa ,  Iyad Akel

IPC: B64C5/02 ,  B64C9/00

CPC classification number: B64C5/02 ,  B64C9/00

Abstract: Tailplanes and empennages for aircraft are disclosed. An exemplary tailplane disclosed includes a stabilizer having a fixed shape and an elevator movably secured to the stabilizer. The elevator is movable from a neutral position relative to the stabilizer. The stabilizer and the elevator define an airfoil cross-sectional shape having a positive camber when the elevator is in the neutral position. The positive camber of the airfoil cross-sectional shape may facilitate movement of the elevator during some flight conditions. Also disclosed are tailplanes having camber distributions that vary along the spans of the tailplanes.

公开(公告)号：US20160176505A1

公开(公告)日：2016-06-23

申请号：US14906605

申请日：2014-07-21

Applicant: LEARJET INC.

Inventor： Reuben CHANDRASEKHARAN ,  Nick IAROCCI ,  Shermineh VAFA ,  Iyad AKEL

IPC: B64C5/02 ,  B64C9/00

CPC classification number: B64C5/02 ,  B64C9/00

Abstract: Tailplanes and empennages for aircraft are disclosed. An exemplary tailplane disclosed includes a stabilizer having a fixed shape and an elevator movably secured to the stabilizer. The elevator is movable from a neutral position relative to the stabilizer. The stabilizer and the elevator define an airfoil cross-sectional shape having a positive camber when the elevator is in the neutral position. The positive camber of the airfoil cross-sectional shape may facilitate movement of the elevator during some flight conditions. Also disclosed are tailplanes having camber distributions that vary along the spans of the tailplanes.

Abstract translation: 披露飞机的飞机和尾翼。 公开的示例性尾板包括具有固定形状的稳定器和可移动地固定到稳定器的电梯。 电梯可以相对于稳定器从中立位置移动。 当电梯处于中立位置时，稳定器和升降机限定了具有正外倾角的翼型横截面形状。 机翼横截面形状的正弧度可能有助于在某些飞行条件下电梯的移动。 还公开了具有沿着尾板跨度变化的弯度分布的尾翼。

公开(公告)号：US20150259072A1

公开(公告)日：2015-09-17

申请号：US14428243

申请日：2012-10-08

Applicant: Pierre GAGNON ,  Tom DEKA ,  Patrick FAHMY ,  Michele MONARDO ,  LEARJET INC. ,  BOMBARDIER INC.

Inventor： Pierre Gagnon ,  Tom Deka ,  Patrick Fahmy ,  Michele Monardo

IPC: B64D11/06 ,  B64D11/00

CPC classification number: B64D11/0638 ,  B64D11/0007 ,  B64D11/0015 ,  B64D11/0604 ,  B64D11/0624 ,  B64D11/0636

Abstract: An aircraft sideboard includes a first portion with a first top surface and a first panel. The first top surface is disposed substantially horizontally at a first height and the first panel is disposed substantially vertically adjacent to the first top surface. A second portion is disposed adjacent to the first portion at a first end of the first portion. The second portion includes a second top surface and a second panel. The second top surface is disposed substantially horizontally at a second height and the second panel is disposed substantially vertically adjacent to the second top surface. A table is stowed interiorly to the first portion. The table extends from the first portion when deployed. The first top surface is immovable. The table deploys by tilting the first panel along a pivot axis defined adjacent to a bottom end thereof. The first height is greater than the second height.

Abstract translation: 飞机侧板包括具有第一顶表面和第一面板的第一部分。 第一顶表面基本上水平地设置在第一高度处，并且第一面板被设置成基本上垂直于第一顶表面。 第二部分在第一部分的第一端处邻近第一部分设置。 第二部分包括第二顶表面和第二面板。 第二顶表面基本上水平地设置在第二高度处，并且第二面板基本上垂直地布置成与第二顶表面相邻。 一张桌子内部存放在第一部分。 部署时，表从第一部分延伸。 第一个顶面是不可移动的。 桌子通过沿着与其底端相邻限定的枢转轴线倾斜第一面板来展开。 第一个高度大于第二个高度。