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Frame shafting support system for three-shaft inertially stabilized platform

A technology for stabilizing the platform and supporting system, which is applied in the field of aerial remote sensing, can solve the problems of increased mechanical bearing support friction, larger shafting structure size, and increased control difficulty, so as to reduce friction, increase load capacity, and improve structure simple compact effect

Active Publication Date: 2015-06-17
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the design of aviation inertial stabilized platforms, the existing support methods for the rotary shaft system of the frame use traditional mechanical supports to realize the swing of the roll frame and the pitch frame. If a larger load is to be achieved, a larger mechanical bearing is required. , which leads to an increase in the overall size of the shafting structure and a complex structure
When the load is large, the frictional force of the mechanical bearing support will also increase accordingly, which will increase the requirements for the drive torque of the platform and increase the difficulty of control

Method used

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  • Frame shafting support system for three-shaft inertially stabilized platform
  • Frame shafting support system for three-shaft inertially stabilized platform
  • Frame shafting support system for three-shaft inertially stabilized platform

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Embodiment Construction

[0019] Such as figure 1 As shown, a three-axis inertial stable platform frame shaft support system in the present invention consists of a rotary shaft 1, a shaft end nut 2, a sleeve 3, a bolt 4, a retaining ring 5, a mechanical bearing 6, an outer end cover 7, an outer end Cover screw 8, inner end cover screw 9, inner end cover 10, outer steel ring 11, rotor mounting ring 12, magnetic bearing support 13, outer cover screw 14, stator magnetic steel 15, rotor magnetic steel 16, outer cover 17, Stator fixing ring 18, rotor fixing ring 19, rotor hoop 20, stator lining block 21, lining block screw 22, support screw 23; stator magnetic steel 15, rotor magnetic steel 16, outer steel ring 9, stator lining block 21 The magnetic bearing structure is adopted; the frame structure 102 is installed on the base 101 through this support system; the outer diameter of one side of the rotary shaft 1 is covered with a sleeve 3, and the sleeve 3 is installed in the base 101 through the bolt 4 and ...

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Abstract

A frame shafting support system for a three-shaft inertially stabilized platform is suitable for the support of shaftings of a rolling frame and a pitching frame of a three-shaft inertially stabilized platform; the support system of the invention adopts a double-support mechanism of a mechanical bearing and a driven magnetic bearing, which is different from a traditional mechanical bearing support mode. The support system mainly comprises a revolving shaft, a mechanical bearing, a magnetic bearing, and the like. The structure of the system has the advantages of less friction and great load bearing, when compared with a traditional mechanical support mode. The support system of the invention is suitable for the support of frame shaftings of inertially stabilized and photoelectric servo platforms for aviation remote sensing, target tracking, and the like.

Description

technical field [0001] The invention belongs to the technical field of aviation remote sensing, and relates to the support of the roll and pitch frame shaft system of a three-axis inertial stabilization platform, which is suitable for the aerial remote sensing three-axis inertial stabilization platform system with a large load and a small self-weight, and can also be used in a vehicle , shipboard, radar and target surveillance and other servo tracking and stabilization platform systems. Background technique [0002] The aerial remote sensing three-axis inertial stabilization platform is one of the key equipment for airborne earth observation. Its function is to support the imaging load and isolate the attitude angle movement and external disturbance of the flight carrier in three directions, so that the visual axis of the imaging load can always track in the inertial space. And perpendicular to the local level, improving imaging resolution. However, due to the limitation of...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C21/18F16M11/00F16C32/04F16C3/02
Inventor 周向阳房建成张钰王春娥李贝
Owner BEIHANG UNIV