Evidence map›Paper›PMID 30585229›Full record

ArticleSensors (Basel, Switzerland)2018

Sensitivity-Compensated Micro-Pressure Flexible Sensor for Aerospace Vehicle.

Xiaozhou Lü, Jianan Jiang, Hui Wang, Qiaobo Gao, Shaobo Zhao, Ning Li, Jiayi Yang, Songlin Wang, Weimin Bao, Renjie Chen

Abstract read
In one paragraph

Article in Sensors (Basel, Switzerland), 2018. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 7 papers.

0numbers the graph read from it
0cells of the map it votes in
7citing papers in PubMed
–field-weighted citation impact
1 · What the graph read from it

What it found

Each row is one number read from the abstract, on the scale the paper reported it, with its interval. Left of the dashed line favours the treatment, right favours the comparator. Under each row is the sentence it came from. New to these charts? A ten-minute tutorial.

The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.

2 · The registry

The trial behind it

Trials whose registry record cites this paper, or whose number appears in the abstract. A trial that started after this paper was published is citing it as background, not reporting it.

Neither the registry nor the abstract names a trial number. If this is a trial report, that itself is worth knowing.

3 · Its place in the literature

Who cites it

7 citing papers in PubMed.

  1. Article
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  4. Review
  5. Process method of SiFrontiers in chemistry · 2022
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4 · The record

Corrections and comments

PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.

5 · Who and what money

Authors and funding

10 authors.

Xiaozhou LüThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. lxz@uw.edu.ORCID 0000-0003-3545-3280
Jianan JiangThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. jiangjianan4213@126.com.
Hui WangThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. whui94@126.com.
Qiaobo GaoThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. 15991262350@sina.cn.
Shaobo ZhaoThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. imnazi@163.com.
Ning LiThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. lining408060@163.com.
Jiayi YangThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. yang.jiayi@stu.xidian.edu.cn.
Songlin WangThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. slwang@mail.xidian.edu.cn.
Weimin BaoThe School of Aerospace Science and Technology, Xidian University, Xi'an 710071, China. baoweimin@cashq.ac.cn.
Renjie ChenBeijing Key Laboratory of Environmental Science and Engineering, School of Chemical Engineering and the Environment, Beijing Institute of Technology, Beijing 100081, China. chenrj@bit.edu.cn.

Funding

National Key Research and Development Program of China 2016YFB0100204National Natural Science Foundation of China 51772030National Natural Science Foundation of China 61601342Natural Science Basic Research Plan in Shaanxi Province of China 2016ZDJC-07Shaanxi Postdoctoral Science Foundation funded project 2017BSHYDZZ36
6 · The paper itself

Abstract

When flight vehicles (e.g., aerospace vehicles, Low Earth Orbit (LEO) satellites, near-space aircrafts, Unmanned Aerial Vehicles (UAVs) and drones) fly at high speed, their surfaces suffer the micro-pressure from high-altitude thin air. The long-term effect of this pressure causes the surface components of flight vehicle to deform or fall off, which can lead to a serious accident. To solve this problem, this paper proposes a sensitivity-compensated micro-pressure flexible sensor based on hyper-elastic plastic material and plate parallel capacitance. The sensor is able to measure a range of 0⁻6 kPa micro-pressure suffered by the flight vehicle's surface with high sensitivity and flexible devices. In this paper, we propose the principle, structure design and fabrication of the sensitivity-compensated micro-pressure flexible sensor. We carried out experiments to obtain the static characteristic curve between micro-pressure and the output capacitance of the sensor devices, and investigated the relationship between sensitivity and geometric parameters. We also compared the performance of the flexible sensor before and after sensitivity compensation. The result shows that the sensor can measure a range of 0⁻2 kPa and 2⁻6 kPa with a sensitivity of 0.27 kPa

Indexed as

aerospaceflexible sensormicro-pressure measurementsensitivity compensation

Identifiers

PMID30585229
PMCPMC6338916

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Registered trials

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Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the OpenQuestion graph.