Our mounts set the standard for compact, high-load, high-capacity vibration isolation and are specifically designed to support and protect avionics equipment in all types of aircraft and defense systems. They are manufactured with specially compounded silicone elastomers that exhibit excellent resonant control, evidenced by the low transmissibility at resonance. The design of these elastomeric isolators also provides linear deflection characteristics.
All our aerospace equipment vibration isolators are tested and approved to the environmental tests appearing in MIL-STD-810 or MIL-E-5400. They may be used in a temperature range of -65°F to +300°F (-54°C to +149°C) for BTR® Silicone and -40°F to +300°F (-40°C to +149°C) for BTR® II Silicone.
Inertial guidance and navigation systems and radar components are examples of applications where these vibration mounts are used. Equipment isolators also are used to isolate engine/aircraft accessories such as fuel controls, pressure sensors and oil coolers.
Ideal for a variety of shock protection applications. Capable of deflecting in both the axial and radial directions under a shock load, these mounts also provide isolation when high amplitude vibration excitation is expected.
Compression Load Range:
0.91 - 23 kg (2 - 50 lbs)
Lightweight and compact, these mounts provide economical protection from lower frequency disturbances regardless of directions of the forces.
Compression Load Range:
0.10 - 3.6 kg (0.25 - 8 lbs)
Unique, high-performance vibration isolators that are small enough and soft enough to isolate individual sensitive electronic components and circuit boards.
Compression Load Range:
46 g (0.1 lb)
These mounts are for fragile, valuable products needing predictable, low to medium level protection. Offering controlled stiffness in all directions, a rugged one-piece bonded assembly, and long service life, they are reusable for years, even under severe shipping conditions.
Shear Load Range:
25 - 595 kg (55 - 1310 lbs)
These isolators feature compact geometry, lightweight materials, failsafe designs and quick installation snap-in and thread locking. These mounts isolate discrete attach points in sidewall panels, floor panels, close-out panels, bulkheads, luggage bins, windows and more. Select isolators meet flame, smoke and toxicity requirements.
These mounts provide excellent all-attitude control of vibration and resistance to environmental extremes. A mechanically safetied assembly incorporates a reliable elastomer-to-metal bond.
Compression Load Range:
0.45 - 68 kg (1 - 150 lbs)
These mounts set the standard for compact, high-load, high capacity isolators. These mounts are tested and approved to the environmental tests appearing in MIL-STD-810 or MIL-E-5400.
Compression Load Range:
1.4 - 11.4 kg (3 - 25 lbs)
These mounts are suitable for use with circuit boards, sensors, displays, instruments, control and other electronic modules. Their compactness eliminates the need for sway space and provides an overall savings in weight.
Compression Load Range:
0.23 - 4.55 kg (0.5 - 10 lbs)
Mounts to isolate steady-state vibration and control occasional shock. These mounts are easy to install and available in two configurations to suit a variety of design requirements. A contoured flexing element, high strength bond, and specially compounded elastomers provide maximum service life.
Compression Load Range:
0.10 - 5.4 kg (0.25 - 12 lbs)
There are a number of critical pieces of information necessary to define the desired functionality of the isolator and determine which isolator to select. Some items are more critical than others, but all should be considered in order to select or design the appropriate product.
Some of the factors which must be considered are:
Weight, Size, Center-of-Gravity of the Equipment to be Isolated — The weight of the unit will have a direct bearing on the type and size of the isolator. The size or shape of the equipment can also affect the isolator design since this may dictate the type of attachment and the available space for the isolator. The center-of-gravity location is also important as isolators of different load capacities may be necessary at different points on the equipment due to weight distribution. The locations of the isolators relative to the center-of-gravity — at the base of the equipment versus in the plane of the C.G., for example — could also affect the design of the isolator.
Types of Dynamic Disturbances to be Isolated — This is basic to the definition of the problem to be addressed by the isolator selection process. In order to make an educated selection or design of a vibration/shock isolator, this type of information must be defined as well as possible. Typically, sinusoidal and/or random vibration spectra will be defined for the application. In many installations of military electronics equipment, random vibration tests have become commonplace and primary military specifications for the testing of this type of equipment (such as MIL-STD-810) have placed heavy emphasis on random vibration, tailored to the actual application. Other equipment installations, such as in shipping containers, may require significant amounts of sinusoidal vibration testing.
Shock tests are often required by many types of equipment. Such tests are meant to simulate those operational (e.g., carrier landing of aircraft) or handling (e.g., bench handling or drop) conditions which lead to impact loading of the equipment.
Static Loadings Other than Supported Weight — In addition to the weight and dynamic loadings which isolators must react, there are some static loads which can impact the selection of the isolator. An example of such loading is the load imposed by an aircraft in a high-speed turn. This maneuver loading must be reacted by the isolator and can, if severe enough, necessitate an increase in the isolator size. These loads are often superposed on the dynamic loads.
Allowable System Response — This is another basic piece of information. In order to appropriately isolate a piece of equipment, the response side of the problem must be known. The equipment manufacturer or user should have some knowledge of the fragility of the unit. This fragility, related to the specified dynamic loadings will allow the selection of an appropriate isolator. This may be expressed in terms of the vibration level versus frequency or the maximum shock loading which the equipment can endure without malfunctioning or breaking. If the equipment manufacturer or installer is experienced with vibration/shock isolation, this allowable response may be specified as the allowable natural frequency and maximum transmissibility allowed during a particular test.
The specification of allowable system response should include the maximum allowable motion of the isolated equipment. This is important to the selection of an isolator since it may define some mechanical motion limiting feature which must be incorporated into the isolator design. It is fairly common to have an incompatibility between the allowable “sway space” and the motion necessary for the isolator to perform the desired function. In order to isolate to a certain degree, it is required that a definite amount of motion be allowed. Problems in this area typically arise when isolators are not considered early enough in the process of designing the equipment or the structural location of the equipment.
Ambient Environment — The environment in which the equipment is to be used is very important to the selection of an isolator. Within the topic of environment, temperature is by far the most critical item. Variations in temperature can cause variations in the performance of many typical vibration/shock isolators. Thus, it is quite important to know the temperatures to which the system will be exposed. The majority of common isolators are elastomeric. Elastomers tend to stiffen and gain damping at low temperatures and to soften and lose damping at elevated temperatures. The amount of change depends on the type of elastomer selected for a particular installation.
Other Environmental Effects — Effects from humidity, ozone, atmospheric pressure, altitude, etc. are minimal and may typically be ignored. Some external factors that may not be thought of as environmental may impact on the selection of an isolator. Fluids (oils, fuels, coolants, etc.) which may come in contact with the isolators can cause a change in the material selection or the addition of some form of protection for the isolators. The level of fluid exposure (immersion vs. splash) is a determining factor.
Service Life — The length of time for which an isolator is expected to function effectively is another strong determining factor in the selection or design process. Vibration isolators, like other engineering structures, have finite lives. Those lives depend on the loads imposed on them. The prediction of the life of a vibration/shock isolator depends on the distribution of loads over the typical operating spectrum of the equipment being isolated. Typically, the longer the desired life of the isolator, the larger that isolator must be for a given set of operating parameters. The definition of the isolator operating conditions is important to any reliable prediction of life.
Our engine mounts are a simplified solution to control the motion of an engine. Made up of few parts, they are quick and easy to install. While there is no standard expected life for engine mounts in service, it is vital to understand how to maintain and inspect them in order to maintain optimal conditions.
Our engine mounts are a simplified solution to control the motion of an engine. Made up of few parts, they are quick and easy to install. While there is no standard expected life for engine mounts in service, it is vital to understand how to maintain and inspect them in order to maintain optimal conditions.
Join Emily Mogel, Mechanical Engineer, for a presentation that will cover general aviation engine mounting systems, designs, installations, and maintenance, followed by a discussion of the functionality and technology behind Lord’s unique fluid-free shimmy dampers.
Learn more about the products available for the aerospace market.