| Literature DB >> 35806917 |
Johannes Zipperle1, Bernhard Ziegler2,3, Herbert Schöchl1,4, Wolfgang Voelckel3,4, Christoph J Schlimp1,3,5, Daniel Oberladstätter1,3,4.
Abstract
Trauma and bleeding are associated with a high mortality, and most of these deaths occur early after injury. Viscoelastic haemostatic tests have gained increasing importance in goal-directed transfusion and bleeding management. A new generation of small-sized and thus portable ultrasound-based viscoelastic analysers have been introduced in clinical practice. We questioned whether a promising candidate can be used in emergency helicopters, with a focus on the susceptibility to vibration stress. We investigated whether the high vibration environment of an emergency helicopter would affect the operability of an ultrasound-based viscoelastic analyser and would yield reproducible results in flight and on the ground. We drew blood from 27 healthy volunteers and performed simultaneous analyses on two TEG 6s. Each measurement was performed in-flight on board an Airbus H135 emergency helicopter and was repeated on the ground, close to the flight area. Results from both measurements were compared, and the recorded tracings and numeric results were analysed for artifacts. Vibratometric measurements were performed throughout the flight in order to quantify changes in the magnitude and character of vibrations in different phases of helicopter operation. The high vibration environment was associated with the presence of artifacts in all recorded tracings. There were significant differences in citrated Kaolin + Heparinase measurements in-flight and on the ground. All other assays increased in variability but did not show significant differences between the two time points. We observed numerous artifacts in viscoelastic measurements that were performed in flight. Some parameters that were obtained from the same sample showed significant differences between in-flight and on-ground measurements. Performing resonance-based viscoelastic tests in helicopter medical service is prone to artifacts. However, a 10 min delay between initiation of measurement and take-off might produce more reliable results.Entities:
Keywords: emergency helicopter; haemostasis; point-of-care; trauma-induced coagulopathy; viscoelastic tests
Year: 2022 PMID: 35806917 PMCID: PMC9267152 DOI: 10.3390/jcm11133630
Source DB: PubMed Journal: J Clin Med ISSN: 2077-0383 Impact factor: 4.964
Figure 1TEG6s devices mounted on the helicopter floor. In contrast to the picture, the device for vibratometric measurement was fixed to the floor for study measurements.
Figure 2Viscoelastic haemostatic measurements from healthy volunteers on the ground and in-flight. Corresponding results from the same donor are connected with a line. Paired t-tests were performed to assess differences between both measurement conditions. Note that in many cases, statistical analysis returned no significant differences between time points. However, when looking on individual data points, measurements yielded different results in-flight and on the ground. CK, Citrated Kaolin; CRT, Citrated Rapid TEG; CKH, Citrated Kaolin + Heparinase; CFF, Citrated Functional Fibrinogen; * p < 0.05; ** p < 0.01; *** p < 0.005; ns, not significant.
Figure 3(A) Frequency of occurrence of artifacts in the tracings of TEG6s measurements. Unlabelled curves were inspected by an operator, who was blinded to the experiment. Data were then stratified by the time from beginning of measurement until the engine was started (“delay < 10 min vs. >10 min”). No artifacts were found in any of the ground measurements. When the measurement was started within 10 min prior to starting the engine, a high number of artifacts were present. In case a certain clot firmness was reached when the engine was started (delay > 10 min), susceptibility of the measurement to artifacts was reduced. Depicted p-values are derived from the applied Chi-square test (B). Representative tracings of measurements on the ground and in-flight (engine on). Multiple inflections and artifacts are visible in measurements that were started immediately (delay < 10 min).
Figure 4(A−C) Representative vibratometric measurement within the high-vibration environment of air medical transport. A smartphone with an accelometric sensor and a respective mobile application was directly attached to the same surface on which both viscoelastic analysers were placed. Vibration is given as acceleration in m/s2. Alignment of the phone and arising axes with regard to both VHAs is illustrated in the insert. Measurement was initiated when the engine of the aircraft was started. Time of take-off is marked with a dashed line. Vibratometric measurements indicate that the devices are already exposed to a high-vibration environment prior to take-off as soon as the engine is started, and that the majority of vibrations occur on the Z-axis. (A) Vibration at X-axis, (B) Vibration at Y-axis and (C) Vibration at Z-axis.