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A multi-parameter acquisition device for super high-rise buildings based on model airplanes

A collection device and super-high-level technology, applied in the direction of measuring devices, aircraft parts, aircraft, etc., can solve the problems of unmeasured, complicated operation, and limited number of units, and achieve the effect of avoiding damage to equipment, high degree of intelligence, and simple operation

Active Publication Date: 2015-12-23
HUNAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Methods (1) and (2) have the problem that the measurement points are limited, and it is impossible to measure at any point on the outer surface of a super high-rise building
Method (3) is expensive to use and complicated to operate. The window cleaning machine is used for each measurement, and long-term measurement and collection of parameters will affect the appearance of the building facade
In addition, the cost of window cleaning machines is high, and the number of units is limited, so it cannot be measured at multiple measuring points on the outer surface at the same time

Method used

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  • A multi-parameter acquisition device for super high-rise buildings based on model airplanes
  • A multi-parameter acquisition device for super high-rise buildings based on model airplanes

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0028] refer to figure 1 , this embodiment includes: a heavy-duty model airplane helicopter 1, a titanium alloy measurement pod 2 is arranged under the heavy-duty model airplane helicopter 1, and a take-off bracket is arranged at the bottom of the titanium alloy measurement pod 2;

[0029] One side of the titanium alloy measuring pod 2 is provided with a titanium alloy vacuum suction pipe 16, the titanium alloy vacuum suction pipe 16 passes through the side wall of the pod 2 horizontally and is fixed with the side wall of the pod 2, the titanium alloy vacuum suction pipe 16 The port of the port is provided with a vacuum suction cup 18, and the vacuum suction cup 18 communicates with the titanium alloy vacuum suction pipe 16, and a vacuum breaking electric valve 17 and a swingable measuring rod 27 are provided on the titanium alloy vacuum suction pipe 16 near the vacuum suction cup 18; Destruction electric valve 17 is connected with measurement controller 3, static pressure sen...

Embodiment 2

[0037] The difference between this embodiment and Embodiment 1 is that the titanium alloy vacuum suction pipe 16 is provided with 4 ports, and each port is provided with a vacuum suction cup 18 . All the other are with embodiment 1.

Embodiment 3

[0039] The difference between this embodiment and Embodiment 1 is that the titanium alloy vacuum suction pipe 16 is provided with 5 ports, and each port is provided with a vacuum suction cup 18 . All the other are with embodiment 1.

[0040] In the present invention, the lithium battery 19 is a measurement controller 3, a data acquisition instrument 4, a wireless transmission module 5, a vacuum pump 14, a vacuum pump controller 15, a vacuum breaking electric valve 17, a compressed air bottle deflation electric valve 24, and a parachute release plate electric valve. Opener 26, measuring rod swing actuator 28 power supply; The power supply of rotatable high-definition camera 13 is provided by measurement controller 3; Solar radiation intensity sensor 6, temperature sensor 7, relative humidity sensor 8, air quality sensor 9, acceleration sensor 10, The power supply of the static pressure sensor 11 and the wind speed sensor 12 is provided by the data acquisition instrument 4 .

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Abstract

The invention discloses a model airplane-based super high-rise building multi-parameter acquisition device which comprises a large-load model airplane helicopter, wherein a titanium alloy measurement pod is arranged below the large-load model airplane helicopter; a titanium alloy vacuum suction tube is arranged on one side of the titanium alloy measurement pod; a vacuum chuck is arranged at the port of the titanium alloy vacuum suction tube; a swingable measurement rod is arranged on the titanium alloy vacuum suction tube; a static pressure sensor and an air velocity sensor are arranged on the swingable measurement rod; a measurement controller which is connected with a data acquisition apparatus, the data acquisition apparatus, a wireless transmission module and a vacuum pump are arranged in the titanium alloy measurement pod; the data acquisition apparatus is connected with the measurement controller; the measurement controller is connected with the wireless transmission module; the vacuum pump is connected with the titanium alloy vacuum suction tube;; a solar radiation intensity sensor, a temperature sensor, a relative humidity sensor and an air quality sensor, which are connected with the data acquisition apparatus, are arranged on the outer wall of the titanium alloy measurement pod. According to the model airplane-based super high-rise building multi-parameter acquisition device, the measurement points are not limited, the parameter measurement is comprehensive and the safety is high.

Description

technical field [0001] The invention relates to a multi-parameter acquisition device for a super high-rise building based on an airplane model aircraft. Background technique [0002] my country's "General Rules for Civil Building Design" GB50352-2005 stipulates that when the building height exceeds 100m, both residential and public buildings are super high-rise buildings. Because the glass curtain wall has the advantages of light weight, easy industrial production, beautiful appearance and good lighting, so super high-rise buildings generally adopt a large number of glass curtain wall enclosure structures. Based on considerations of safety, central air-conditioning system design, aesthetic requirements, and the wind field of super high-rise buildings, the glass curtain walls of super high-rise buildings rarely have external windows that can be opened above 100m. [0003] When conducting structural system research, HVAC system research and optimization of super high-rise bui...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02B64D47/00G01D21/02
Inventor 李念平王宽成剑林苏林胡锦华魏小清张旭涵
Owner HUNAN UNIV