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CN-224225297-U - Aircraft battery fixing device

CN224225297UCN 224225297 UCN224225297 UCN 224225297UCN-224225297-U

Abstract

The utility model relates to the technical field of machinery, in particular to an aircraft battery fixing device which comprises a base and a structural component, wherein the structural component comprises a limiting block, an inserting rod, an inserting frame, a pressing plate, a fixing rod, a fixing frame, a driving member and a power member, wherein the inserting frame is slidably arranged on one side of the base, the inserting rod is slidably connected with the inserting frame and is slidably connected with the base, the driving member is connected with the inserting frame, the limiting block is fixedly connected with the inserting rod and is connected with the driving member, the fixing frame is slidably connected with the base and is positioned on one side of the base away from the limiting block, the fixing rod is slidably connected with the base and is slidably connected with the fixing frame, the pressing plate is fixedly connected with the fixing rod and is positioned on one side of the fixing rod away from the fixing frame, and the power member is connected with the fixing frame and is connected with the pressing plate, so that aircraft batteries with different specifications and sizes can be conveniently fixed.

Inventors

  • HE BO
  • HAN TAO

Assignees

  • 麦航(郑州)新能源有限公司

Dates

Publication Date
20260512
Application Date
20241230

Claims (5)

  1. 1. An aircraft battery fixing device, includes base, its characterized in that: also comprises a structural component; The structure assembly comprises a limiting block, an inserting rod, an inserting frame, a pressing plate, a fixed rod, a fixed frame, a driving member and a power member, wherein the inserting frame is slidably installed on one side of the base, the inserting rod is slidably connected with the inserting frame and is slidably connected with the base, the driving member is connected with the inserting frame, the limiting block is fixedly connected with the inserting rod and is connected with the driving member, the fixed rod is slidably connected with the base and is located on one side of the base away from the limiting block, the fixed rod is slidably connected with the base and is slidably connected with the fixed frame, the pressing plate is fixedly connected with the fixed rod and is located on one side of the fixed rod away from the fixed frame, and the power member is fixedly connected with the fixed frame and is connected with the pressing plate.
  2. 2. The aircraft battery holder according to claim 1, wherein: the driving member comprises a driving rod and a driving spring, wherein the driving rod is in sliding connection with the plug frame and is fixedly connected with the limiting block, one end of the driving spring is connected with the plug frame, and the other end of the driving spring is connected with the driving rod.
  3. 3. The aircraft battery holder according to claim 1, wherein: The power component comprises a power rod and a power spring, wherein the power rod is in sliding connection with the fixed frame and is fixedly connected with the pressing plate, one end of the power spring is connected with the fixed frame, and the other end of the power spring is connected with the power rod.
  4. 4. The aircraft battery holder according to claim 1, wherein: The base is provided with a first through hole, the first through hole is positioned on one side of the base, close to the inserted link, and is matched with the inserted link, and the inserting frame is provided with an inserting hole, and the inserting hole is positioned on one side of the inserting frame, close to the inserted link, and is matched with the inserted link.
  5. 5. The aircraft battery holder according to claim 1, wherein: The base is provided with a second port, the second port is positioned on one side of the base, which is close to the fixed rod, and is matched with the fixed rod, and the fixed frame is provided with a positioning hole, and the positioning hole is positioned on one side of the fixed frame, which is close to the inserted rod, and is matched with the fixed rod.

Description

Aircraft battery fixing device Technical Field The utility model relates to the technical field of machinery, in particular to an aircraft battery fixing device. Background The main function of the aircraft battery is to provide a power source for the aircraft, ensure that the aircraft battery can normally fly and execute tasks, and simultaneously can be used as a standby power supply for supplying power to key equipment of the aircraft under emergency conditions, so that the flight safety is ensured, the common device can only fix the aircraft battery with the same specification and size, and when the device needs to fix the aircraft battery with different specification and size, the device can not install the aircraft battery with different specification and size, thereby influencing the use effect of the device. Prior art CN208053660U an aircraft battery fixing device and aircraft, including bolt, clamp plate, fuselage, stopper, baffle and baffle spring, adjusting bolt can adjust the position of stopper on the fuselage and the position of clamp plate on the stopper to make stopper and clamp plate laminate respectively with the side and the bottom surface of battery, the baffle receives baffle spring's pulling force effect can laminate with the side of battery, makes the aircraft battery of different specification sizes install, thereby improves the result of use of device. In normal use, the fixed mode of prior art is according to the aircraft battery of different specification sizes, when adjusting the position of stopper and clamp plate, wastes time and energy, and is mostly inconvenient to cause the inconvenience to fix the aircraft battery of different specification sizes. Disclosure of utility model The utility model aims to provide an aircraft battery fixing device, which solves the problems that the fixing mode in the prior art is time-consuming and labor-consuming and inconvenient to fix aircraft batteries with different specifications and sizes when the positions of a limiting block and a pressing plate are adjusted according to the aircraft batteries with different specifications and sizes. The utility model provides an aircraft battery fixing device which comprises a base and a structural component, wherein the structural component comprises a limiting block, an inserting rod, an inserting frame, a pressing plate, a fixed rod, a fixed frame, a driving member and a power member, the inserting frame is slidably arranged on one side of the base, the inserting rod is slidably connected with the inserting frame and is slidably connected with the base, the driving member is connected with the inserting frame, the limiting block is fixedly connected with the inserting rod and is connected with the driving member, the fixed frame is slidably connected with the base and is positioned on one side of the base far away from the limiting block, the fixed rod is slidably connected with the base and is slidably connected with the fixed frame, the pressing plate is fixedly connected with the fixed rod and is positioned on one side of the fixed rod far away from the fixed frame, and the power member is connected with the fixed frame and is connected with the pressing plate. The driving member comprises a driving rod and a driving spring, wherein the driving rod is in sliding connection with the inserting frame and is fixedly connected with the limiting block, one end of the driving spring is connected with the inserting frame, and the other end of the driving spring is connected with the driving rod. The power component comprises a power rod and a power spring, wherein the power rod is in sliding connection with the fixed frame and is fixedly connected with the pressing plate, one end of the power spring is connected with the fixed frame, and the other end of the power spring is connected with the power rod. The base is provided with a first through hole, the first through hole is positioned on one side of the base, close to the inserted link, and is matched with the inserted link, and the inserted frame is provided with an inserting hole, and the inserting hole is positioned on one side of the inserted frame, close to the inserted link, and is matched with the inserted link. The base is provided with a second port, the second port is positioned on one side of the base, which is close to the fixed rod, and is matched with the fixed rod, the fixed frame is provided with a positioning hole, and the positioning hole is positioned on one side of the fixed frame, which is close to the inserted rod, and is matched with the fixed rod. According to the aircraft battery fixing device, the limiting block is pulled to drive the inserting rod to be separated from the inserting frame, the limiting block drives the driving rod to move on the inserting frame, the driving spring is compressed under the movement of the driving rod to push the inserting frame to move on the base, after moving in place, the limiting block is rel