FIELD: isolating mats.
SUBSTANCE: invention relates to methods and devices for shaping insulating mats and their installation in vehicle compartment. Vehicle isolation unit comprises insulating mat, which includes outer layer, insulating layer arranged in outer layer, and first fastening element located in insulating layer. Outer and insulating layers are configured to form a first channel, and first fastening element is configured to receive, by first channel, first part of vehicle compartment component for connection sealing of insulating layer and outer layer of insulating mat with carcass element of vehicle compartment. Insulating layer and the first fastener located in the insulating layer are placed in the outer layer. First fastening element has a solid structure comprising a first flange, a second flange opposite the first flange and a middle part extending between the first flange and the second flange. First and second flanges are configured to attach part of insulating mat to carcass element of vehicle compartment.
EFFECT: higher strength of structure after assembly.
13 cl, 11 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD, SYSTEM AND LINING OF CARGO COMPARTMENT OF AIRCRAFT | 2016 |
|
RU2719096C2 |
STRUCTURAL BEAM ASSEMBLY (VERSIONS), METHOD OF ASSEMBLING A REINFORCED STRUCTURAL BEAM, AERODYNAMIC SURFACE AND AIRCRAFT | 2017 |
|
RU2742128C2 |
APPARATUS AND METHODS FOR JOINING AIRCRAFT COMPOSITE STRUCTURES | 2014 |
|
RU2666593C2 |
CLAMPING SYSTEM FOR TRANSPORT ELEMENTS, METHOD FOR STABILIZING TRANSPORT ELEMENT AND AIRCRAFT | 2018 |
|
RU2754235C2 |
FAIRING NODE AND METHOD FOR IT | 2018 |
|
RU2759138C2 |
EXHAUST PIPE (VERSIONS), STIFFNESS MECHANISM FOR AN EXHAUST PIPE AND A METHOD FOR INCREASING THE RESONANCE FREQUENCY OF AN EXHAUST SYSTEM COMPRISING AN EXHAUST PIPE | 2017 |
|
RU2737061C2 |
SPACECRAFT DOCKING SYSTEM | 2014 |
|
RU2683706C2 |
THERMOPLASTIC SANDWICH STRUCTURES | 2014 |
|
RU2667543C2 |
SYSTEMS AND METHODS FOR TRANSMITTING ELECTRICAL SIGNALS TO ELECTRICAL DEVICES IN THE VEHICLE INTERIOR | 2017 |
|
RU2752669C2 |
HEAT INSULATION FOR AIRCRAFT COMPONENTS AND METHOD FOR ASSEMBLY AND USE THEREOF | 2018 |
|
RU2753048C2 |
Authors
Dates
2020-11-24—Published
2017-02-06—Filed