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Aerial photography mount

a technology for mounting mounts and photography, applied in the field of aerial photography mounts, can solve problems such as degrading the visual quality of images, and achieve the effects of reducing the amount of vibration, improving the degree of vibration reduction, and low friction

Inactive Publication Date: 2014-07-01
WAWRO CHRISTOPHER
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The gimbal unit is designed to be attached to a camera or tripod head, and can be adjusted for height and pitch to ensure smooth image capture. The unit uses gyroscopic stabilizers to keep the camera steady in space, and can counteract movements caused by yaw, roll, and pitch. The gimbal suspension blocks can be adjusted independently for leveling the camera, and the framework can be easily adjusted for different camera placements. The technical effects of the invention include improved stability and control for image capture in an aircraft.

Problems solved by technology

The taking of photographs and video from platforms such as aircraft and other modes of transportation is highly desirable for many applications but is made difficult because of the vibration that is transmitted to the camera causes movements that degrade the visual quality of the images.

Method used

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Examples

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Embodiment Construction

[0019]As shown in FIGS. 1-5, the preferred embodiment of the mount comprises a gimbal unit assembly 51 having a vertical post assembly 55, a central gimbal frame 15, and gimbal end suspension assemblies 8. The vertical gimbal post assembly 55 and the end suspension assemblies 8 are connected to the central gimbal frame 15 in a manner described more specifically below that permits a camera mounted to the vertical post assembly 55 to be moved freely and simultaneously through the yaw, roll, and pitch axes. The gimbal unit assembly 51 is suspended from elastic straps 7 that connect the end suspension assemblies 8 to hooks 11 on post blocks 1 which in turn are connected to a pair of posts 2. This means of suspension dampens the vibrations of the aircraft that would otherwise be transmitted to the gimbal unit assembly 51.

[0020]As shown in FIGS. 1 and 3, the vertical gimbal post assembly 55 comprises a camera mount base 16 for the attachment of a base mount plate 6 and tripod head 5 at th...

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Abstract

An aerial photography mount that features a three-axis gimbal unit that is supported between two posts by elastic straps. Each of the axes rotates within precision bearings that enable smooth operation of a camera secured to the mount. The elastic straps, in conjunction with independently rotating bearings at the end suspension assemblies, provide a enhanced vibration isolation effect. The mount can be further stabilized by the attachment of gyroscopic stabilizers.

Description

CROSS-REFERENCED TO RELATED APPLICATIONS[0001]This application is a reissue application U.S. Pat. No. 8,434,950, the entirety of which is incorporated by reference, which claims the benefit of provisional application 61 / 448,959 which was filed on Mar. 3, 2011.FIELD OF THE INVENTION[0002]The invention relates generally to the field of aerial photography mounts.BACKGROUND OF THE INVENTION[0003]The taking of photographs and video from platforms such as aircraft and other modes of transportation is highly desirable for many applications but is made difficult because of the vibration that is transmitted to the camera causes movements that degrade the visual quality of the images. Compounding the problem is the need by many photographers to be able to selectively aim the imaging device within the confines of a small space. It is especially desirable that an aerial photography mount be portable and capable of being secured to a variety of aircraft, ground vehicles, and watercraft in a mann...

Claims

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Application Information

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Patent Type & Authority Patents(United States)
IPC IPC(8): G03B17/00G03B39/00G03B17/56
CPCF16M11/2092G03B2205/0007G03B17/561F16M11/123G03B17/00F16M13/022G03B15/006F16M11/00F16F7/00F16M2200/041F16F15/04G03B17/56F16M11/24
Inventor WAWRO, CHRISTOPHER
Owner WAWRO CHRISTOPHER
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