公开(公告)号：US20160101845A1

公开(公告)日：2016-04-14

申请号：US14513172

申请日：2014-10-13

Applicant: Gulfstream Aerospace Corporation

Inventor： Tongan Wang ,  Michael Eugene Lucas ,  Kristopher P. Lynch ,  Tyler Relf ,  John Willett Maxon, JR.

IPC: B64C1/40 ,  B64D37/32 ,  B64C7/00

CPC classification number: B64C1/40 ,  B64C7/00 ,  B64D37/32

Abstract: Aircraft, wing-to-body fairing assemblies, and air exchange systems are provided. An aircraft includes a fuselage, a wing secured to the fuselage, an outer skin panel, and an air exchange system. The outer skin panel is secured to the wing and/or the fuselage and at least partially defines a cavity. The air exchange system is secured to the outer skin panel and exchanges air between the cavity and an external environment. The air exchange system includes an air inlet, a diffuser, and a silencer. The air inlet is disposed in the outer skin panel and accommodates an air flow between the cavity and the external environment. The diffuser is attached to the air inlet and has a varying cross sectional area to change the speed of the air flow. The silencer is attached to the diffuser and communicates the air flow between the diffuser and the cavity and reduces noise.

Abstract translation: 提供飞机，翼对整流罩组件和空气交换系统。 一架飞机包括一个机身，一个固定在机身上的机翼，一个外壳和一个空气交换系统。 外部皮肤面板固定到机翼和/或机身上，并且至少部分地限定空腔。 空气交换系统固定在外皮面板上，并在空腔和外部环境之间交换空气。 空气交换系统包括进气口，扩散器和消音器。 空气入口设置在外表面板中并且容纳在空腔和外部环境之间的空气流。 扩散器连接到空气入口并且具有变化的横截面积以改变空气流的速度。 消声器连接到扩散器，并使扩散器和空腔之间的空气流通过并减少噪音。

公开(公告)号：US09845144B2

公开(公告)日：2017-12-19

申请号：US14513172

申请日：2014-10-13

Applicant: Gulfstream Aerospace Corporation

Inventor： Tongan Wang ,  Michael Eugene Lucas ,  Kristopher P. Lynch ,  Tyler Relf ,  John Willett Maxon, Jr.

IPC: B64C1/40 ,  B64C7/00 ,  B64D37/32

CPC classification number: B64C1/40 ,  B64C7/00 ,  B64D37/32

Abstract: Aircraft, wing-to-body fairing assemblies, and air exchange systems are provided. An aircraft includes a fuselage, a wing secured to the fuselage, an outer skin panel, and an air exchange system. The outer skin panel is secured to the wing and/or the fuselage and at least partially defines a cavity. The air exchange system is secured to the outer skin panel and exchanges air between the cavity and an external environment. The air exchange system includes an air inlet, a diffuser, and a silencer. The air inlet is disposed in the outer skin panel and accommodates an air flow between the cavity and the external environment. The diffuser is attached to the air inlet and has a varying cross sectional area to change the speed of the air flow. The silencer is attached to the diffuser and communicates the air flow between the diffuser and the cavity and reduces noise.

公开(公告)号：US11214374B2

公开(公告)日：2022-01-04

申请号：US15658140

申请日：2017-07-24

Applicant: Gulfstream Aerospace Corporation

Inventor： Michael Lucas ,  Kristopher P. Lynch ,  Benjamin Frank Wilson ,  Jeffrey Jonas

IPC: B64D11/06

Abstract: Aircraft, vibration isolation assemblies, and methods of assembling vibration isolation assemblies are provided. An aircraft includes a vibration isolation assembly. The vibration isolation assembly includes a mounting track, a plate, a clamp block, a vibration isolator, and a support fitting. The mounting track defines a cavity and includes flanges that define an opening to the cavity. The plate is configured to be positioned on the flanges outside of the cavity. The clamp block is configured to be fastened to the plate under the flanges of the mounting track within the cavity. The vibration isolator is configured to be laterally constrained by the clamp block within the cavity. The support fitting is configured to be secured to the vibration isolator outside of the cavity.

公开(公告)号：US20180029714A1

公开(公告)日：2018-02-01

申请号：US15658140

申请日：2017-07-24

Applicant: Gulfstream Aerospace Corporation

Inventor： Michael Lucas ,  Kristopher P. Lynch ,  Benjamin Frank Wilson ,  Jeffrey Jonas

IPC: B64D11/06

CPC classification number: B64D11/0619 ,  B64D11/0696

Abstract: Aircraft, vibration isolation assemblies, and methods of assembling vibration isolation assemblies are provided. An aircraft includes a vibration isolation assembly. The vibration isolation assembly includes a mounting track, a plate, a clamp block, a vibration isolator, and a support fitting. The mounting track defines a cavity and includes flanges that define an opening to the cavity. The plate is configured to be positioned on the flanges outside of the cavity. The clamp block is configured to be fastened to the plate under the flanges of the mounting track within the cavity. The vibration isolator is configured to be laterally constrained by the clamp block within the cavity. The support fitting is configured to be secured to the vibration isolator outside of the cavity.

公开(公告)号：US20160083098A1

公开(公告)日：2016-03-24

申请号：US14495667

申请日：2014-09-24

Applicant: Gulfstream Aerospace Corporation

Inventor： Michael Lucas ,  Kristopher P. Lynch ,  Benjamin Frank Wilson ,  Jeffrey Jonas

IPC: B64D11/06

CPC classification number: B64D11/0696

Abstract: Aircraft, vibration isolation assemblies, and methods of assembling vibration isolation assemblies are provided. An aircraft includes a fuselage, a mounted component disposed within the fuselage, and a vibration isolation assembly disposed within the fuselage and mounting the mounted component to the fuselage. The vibration isolation assembly includes a mounting track, an inner member, a support fitting, and an elastomer. The mounting track defines a cavity and an opening. The inner member has a post and a flange, where the flange is disposed in the cavity. The support fitting is secured to the post and the mounted component. The elastomer is disposed between the flange and the mounting track within the cavity.

Abstract translation: 提供飞机，隔振组件以及组装隔振组件的方法。 飞机包括机身，设置在机身内的安装部件和设置在机身内的防振组件，并将安装的部件安装在机身上。 隔振组件包括安装轨道，内部构件，支撑配件和弹性体。 安装轨道定义了空腔和开口。 内部构件具有柱和凸缘，其中凸缘设置在空腔中。 支撑配件被固定到柱和安装的部件上。 弹性体设置在凸缘和腔内的安装轨道之间。