Composite frames for opto-mechanical support structures

BACKGROUND 1. Field

The present disclosure relates to opto-mechanical support structures, and more particularly to opto-mechanical support structures with frames of fiber-reinforced composite materials.

2. Description of Related Art

Existing opto-mechanical support structures for optics and mechanical systems such as cameras and like imaging or information transmission systems are metallic based on shell designs with supportive ribs. Substitution of metal by fiber-reinforced polymer-matrix composites provides significant advantages such as lighter weight, corrosion resistance, durability, vibrational damping and more reliable supply chain availability without in advance ordering. Current composite structures usually mimic the existing metallic shell-based designs. However, current composite shell-based designs are limited by, among other things, relatively low stiffness and low strength properties in non-fiber orientations (transversal, shear, interlaminar) requiring their thickness increase with associated extra weight, complexity and cost of fabrication requiring considerable manual labor, additional risk of damage, especially in shell/ribs connections, and expensive quality/service control.

The conventional techniques have been considered satisfactory for their intended purpose. However, there is an ever-present need for improved systems and methods for improved composite components for optics support structures with potential for both design and manufacturing improvement/optimization. This disclosure provides a solution for this need.

SUMMARY

A frame for an opto-mechanical support structure includes an interconnected lattice of frame composite rods defined about an interior space with interstices defined between the frame composite rods.

The lattice of frame composite rods can include a plurality of continuous loop frame composite rods interconnected with the lattice. The lattice of frame composite rods can include a plurality of dis-continuous loop frame composite rods interconnected with the lattice. The frame composite rods can be unidirectionally fiber-reinforced composite elements, e.g. composite tapes or combination of such tapes. Intersections of the frame composite rods can include interlaying of the composite element layers of the respective intersecting frame composite rods.

At least one of the frame composite rods can include a cross-sectional profile selected from the group consisting of: constant thickness, non-constant thickness where one surface of the cross-sectional profile is flat, non-constant thickness where opposed surfaces are both not flat, one rib extending from a base, multiple ribs extending from an external surface, a hollow shape, a hollow shape with an insert inside, multiple different materials in layers varied through thickness of the cross-sectional profile, and multiple different materials in layers varied through thickness and width of the cross-sectional profile.

One of the interstices can define an opto-mechanical aperture therethrough for admittance of optics image data through the lattice and frame. Wall panels can be mounted to an exterior aspect of the lattice for protection of the interior space. At least one of the wall panels can include an aperture therethrough, aligned with the optical aperture of the lattice. An opto-mechanical assembly can be mounted inside the lattice and frame with an objective lens aligned with an optics aperture through one of the interstices in the lattice.

At least one of the frame composite rods can form a continuous loop that extends across more than one surface of the interior space. The interior space can be six-sided and wherein at least one of the frame composite rods forms a continuous loop that extends across all six sides of the interior space. The interior space can be six-sided and wherein at least one of the frame composite rods forms a continuous loop that extends across three different sides of the interior space. The interior space can be six-sided and wherein at least one of the frame composite rods forms a continuous loop that extends across four different sides of the interior space. Two or more frames as described above can be connected together as a three-dimensional gimbal.

A method of making an opto-mechanical frame includes forming a frame of interconnected lattice of frame composite rods using one or more fabrication processes by Automated Fiber Placement (AFP) technique around a mandrel. The method includes removing the mandrel from an interior space of the frame after forming the frame.

The method can include removing the mandrel by dissolving or washing the mandrel away after forming the frame. Forming the frame can include using at least one AFP arm to articulate fibers around the mandrel relative to a fixed frame of reference. Forming the frame can include rotating the mandrel relative to the fixed frame of reference. Forming the frame can include forming interlayered intersections of the frame composite rods in the lattice on a one-layer-at-a-time basis.

These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description of the preferred embodiments taken in conjunction with the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, preferred embodiments thereof will be described in detail herein below with reference to certain figures, wherein:

FIG. 1 is a schematic perspective view of an embodiment of a composite frame constructed in accordance with the present disclosure, showing the frame composite rods and interstices;

FIGS. 2a-2e are schematic perspective views of frame composite rods, showing representative continuous loop frame composite rods crossing different numbers of sides of the mandrel on an exemplary six-sided internal space;

FIG. 3 is a schematic perspective view of a composite frame, showing the optical aperture in the frame;

FIGS. 4a-4b are schematic front two-dimensional views of composite frames, showing examples of two different densities of composite distribution;

FIGS. 5a-5d are schematic perspective views of mandrels for forming composite frames, showing representative examples of different mandrel shapes;

FIGS. 6a-6b are schematic in plane and cross-sectional views of an intersection of frame composite rods of FIG. 1;

FIGS. 7a-7i are schematic cross-sectional views of different examples of cross-sectional profiles for frame composite rods;

FIG. 8 is an exploded perspective view of the composite frame of FIG. 1, showing wall panels for protecting the interior space of the frame; and

FIG. 9 is a schematic perspective view of a gimbal formed of two or more composite frames like the composite frame of FIG. 1.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an embodiment of a frame in accordance with the disclosure is shown in FIG. 1 and is designated generally by reference character 100. Other embodiments of systems in accordance with the disclosure, or aspects thereof, are provided in FIGS. 2-9, as will be described. The systems and methods described herein can be used to form composite frames for optics or opto-mechanical systems.

The frame 100 for an optical or other equipment support structure includes an interconnected lattice 102 of frame composite rods 104 defined about an interior space 106 with interstices 108 defined between the frame composite rods 104. In FIG. 1, not all of the interstices 108 are labeled for sake of clarity. Also shown in FIG. 1 is the mandrel 110 about which the frame composite rods 104 are formed. FIG. 1 shows the beginning of a frame structure, to which additional frame composite rods 104 can be added to form a complete frame 100, for example as shown in FIG. 3.

FIG. 2a shows another beginning stage for forming a frame 100, with an Automated Fiber Placement (AFP) arm 112 forming a continuous, i.e., closed loop frame composite rod 104 about the mandrel 110. The double arrows in FIG. 2a schematically indicate examples of movement orientations of the AFP arm 112, e.g., relative to a stationary frame of reference, that can be used form forming the frame composite rods 104. In other embodiments, using advanced AFP capabilities, the AFP arm 112 can move in all three space directions and similarly rotate in all three angular orientations. The circular arrows in FIG. 2a schematically indicate examples of the movement or rotation of the mandrel 110 itself, relative to the same stationary frame of reference, which can also be used for forming the frame composite rods 104. Depending on the specifics of AFP implementation, the mandrel 110 can move and/or rotate in different directions and orientations. In this example, the frame composite rod 104 in FIG. 2a forms a continuous, i.e., closed, loop on itself and crosses over four faces of the 6-sided mandrel (and corresponding interior space 106, see FIG. 1), e.g., the top, front, bottom, and back surfaces as oriented in FIG. 2a.

FIG. 2b shows another frame continuous, i.e., closed, loop forming a frame composite rod 104 that crosses all six surfaces of the mandrel (and corresponding interior space 106, see FIG. 1), and crosses each of the top and bottom surfaces twice, as oriented in FIG. 2b. FIG. 2c shows another continuous, i.e. closed, loop frame composite rod 104 that crosses the three adjacent sides (top, front, and right sides), and the bottom surface of the mandrel 110, including crossing the bottom surface three times, as oriented in FIG. 2c. FIG. 2d shows another continuous or closed loop frame composite rod 104 that crosses the front, right, back, and left surfaces (the peripheral surfaces) of the mandrel 110, as oriented in FIG. 2d. FIG. 2e shows a similar frame composite rod 104 to that shown in FIG. 2c, but crossing the left surface of the mandrel instead of the right, as oriented in FIG. 2e. Those skilled in the art will readily appreciate that any suitable continuous, i.e., closed, loop pattern can be used for frame composite rods 104 without departing from the scope of this disclosure, i.e., FIGS. 2a-2e show representative examples which can be similarly extended to other mandrel shapes and/or frame rod designs.

With reference now to an example of a composite frame shown in FIG. 3, the lattice 102 of frame composite rods 104 includes a plurality of continuous loop frame composite rods 104, such as those described above with reference to FIGS. 2a-2e, interconnected with the lattice 102. The lattice 102 also includes a plurality of dis-continuous or open loop frame composite rods 105 interconnected with the lattice 102. FIGS. 4a and 4b show two-dimensional side views of two lattices 102, respectively, one with a less dense lattice design, and the other with a more dense lattice design. Number and geometries of frame composite rods 104 can be used to control the lattice density and structural integrity according to specifics of a given application.

Additionally, the lattice 102 needs not to conform to a rectangular mandrel 110 or interior space 106 with rectangular cross-sections (labeled in FIG. 1). FIGS. 5a-5d show frame composite rods 104 being formed on mandrels 110 shaped with a rectangular cross-section (FIG. 5a), with a rounded corner rectangular cross-section (FIG. 5b), with an oval, or more generally, convex cross-section (FIG. 5c), and with an arbitrary cross-section including both convex and concave segments (FIG. 5d). In addition to different two-dimensional geometries of cross-sectional designs, different three-dimensional geometries of mandrels can be similarly applied. Those skilled in the art will readily appreciate that any suitable lattice structure can be used for an opto-mechanical support structure without departing from the scope of this disclosure.

The frame composite rods 104, 105 are unidirectionally reinforced by fibers polymer-matrix composite elements, which can all be formed by an AFP arm 112, as shown in FIG. 2a. Carbon, glass and organic (e.g., Kevlar) fibers or any of their combinations can be used, among others, for the reinforcement. Thermoplastics or thermosets can be used as the polymer matrix. As shown in FIGS. 6a-6b, intersections 114 in the lattice 102 of the frame composite rods 104 include interlaying of the composite layers 116 or groups of layers 116 of the respective intersecting frame composite rods 104, formed by laying the one layer (or group of layers) at a time in the intersection stack, every other layer (or group of layers) belonging to one of the intersecting respective frame composite rods 104. The frame composite rods 104 can be formed layer by layer (or one group of layers by another group of layers), one layer (or one group of layers 116) at a time to have any suitable cross-sectional profile.

The frame composite rods 104 in FIG. 6b have rectangular, constant thickness cross-sections, shown in FIG. 7a. Any other suitable cross-sectional configuration can be used for the frame composite rods 104. FIG. 7b shows a frame composite rod 104 with a non-constant thickness where one surface of the cross-sectional profile is flat, i.e., the bottom layer 116 is flat, and the successive layers 116 upward from the bottom are successively narrower towards the top as oriented in FIG. 7b. FIG. 7c shows a non-constant thickness where opposed surfaces (i.e., the top and bottom layers 116 as oriented in FIG. 7c) are both non-flat. FIG. 7d shows a cross-sectional profile for a frame composite rod 104 with one rib 118 extending from a base, e.g., from the top or bottom layer, and FIG. 7e shows a cross-sectional profile with multiple ribs 118 extending from a base (with the base as the top layer in this example). FIG. 7f shows a cross-sectional frame composite rod profile with a hollow shape, and FIG. 7g shows one with a hollow shape having an insert 120 inside. The inserts 120 can be any suitable light-weight materials, for example, polymeric, foam, elastomeric, honeycomb, among others. The layers 116 can vary in material during the AFP process, giving a frame composite rod 104 with a cross-sectional profile having multiple different composite materials 122/124 in layers 116 varied through thickness of the cross-sectional profile, as shown in FIG. 7h. In FIG. 7i, the multiple different materials 122/124 in layers 116 are varied through thickness and width of the cross-sectional profile, as shown in FIG. 7i.

With reference now to FIG. 8, one of the interstices 108 defines an optics or opto-mechanical aperture 126 therethrough for admittance of image data, e.g., optical or any portion of the electromagnetic spectrum for example, through the frame 100. After forming the lattice 102, the method includes removing the mandrel 110 (labeled in FIG. 1) from an interior space 106 of the frame 100 after forming the frame 100. The mandrel 110 can be removed by dissolving or washing the mandrel 120 away after forming the frame 100. Wall panels 128, e.g., of a composite monolithic or a sandwich design, can optionally be mounted to an exterior aspect of the frame 100 for protection of the interior space 106. Such wall panels 128 can include one or more aperture 130 therethrough, e.g., aligned with the optics aperture 126 of the lattice 102. The wall panels 128 can provide protection for optics/imaging components housed inside the lattice.

An example of usage of composite frames is illustrated in FIG. 9. An optical and/or imaging assembly 132, e.g., including a camera, lens, telescope, or the like, is mounted inside the lattice 102 with an objective lens 134 aligned with the optical aperture 126 through one of the interstices 108 in the lattice 102 (labeled in FIG. 3). Two or more frames 100 constructed as disclosed herein can be connected together as a three-dimensional gimbal 10, where two axes of rotation A and B are indicated in FIG. 9.

The methods and systems of the present disclosure, as described above and shown in the drawings, provide for forming composite frames for optics systems. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.

U.S. Patent Documents Foreign Patent Documents Other references

• Extended European Search Report dated Jul. 14, 2023, issued during the prosecution of European Patent Application No. EP 23157403.9.
• Belnoue et al. “Understanding and predicting defect formation in automated fibre placement pre-preg laminates” Composites Part A: Applied Science and Manufacturing 102 (Nov. 2017) pp. 196-206.

Patent number: 12181098
Type: Grant
Filed: Feb 24, 2022
Date of Patent: Dec 31, 2024
Patent Publication Number: 20230265964
Assignee: GOODRICH CORPORATION (Charlotte, NC)
Inventors: Mark R. Gurvich (Middletown, CT), Brian J. Smith (Maynard, MA)
Primary Examiner: Steven M Marsh
Application Number: 17/679,489

Current U.S. Class: Designated Nonreactive Material (dnrm) Has Numerically Specified Characteristic, E.g., Particle Size, Density, Etc., Other Than Viscosity, M.p., B.p., Molec. Wt., Chemical Composition Or Percentage Range (523/513)
International Classification: F16M 11/00 (20060101); B29C 70/38 (20060101); F16M 11/12 (20060101); B29L 12/00 (20060101); G02B 7/00 (20210101);