GB/T 38924.6-2020Environmental test methods for civil small and light unmanned aircraft system—Part 6: Vibration test (English PDF)
民用轻小型无人机系统环境试验方法 第6部分：振动试验
This is a limited preview
Buy now to download the full PDF (15 pages)
Need quotation for your management?
Get a formal quotation for GB/T 38924.6-2020 in 30 minutes.
Issued by
SAMR; SAC
Level / Type
National · Recommended
Issue date
July 21, 2020
Implementation date
February 1, 2021
Scope
GB/T 38924.6-2020 is the English-translated version of 民用轻小型无人机系统环境试验方法 第6部分：振动试验.
GB/T 38924.6-2020 is the Chinese standard "Environmental test methods for civil small and light unmanned aircraft system—Part 6: Vibration test".
Its scope clause reads: This part of GB/T 38924 specifies the civil light and small unmanned aerial vehicle (take-off weight 0.25kg~150kg) system (including aircraft and Ground station) vibration test requirements and methods, including test conditions, test equipment and instruments, test process, test interruption and recovery, test results Evaluation and test reports, etc. This part is applicable to light and small civilian use (maximum take-off weight greater than 0.25kg) that may experience a vibration environment during transportation and use, and not more than 150kg) multi-rotor UAV system, fixed-wing UAV system, unmanned helicopter system and vehicle-mounted ground station to determine Whether the civil light and small UAV system can withstand the impact of the vibration environment. Its clauses include test conditions.
Found what you need?
Document preview — GB/T 38924.6-2020
National Standard of the People's Republic of China
- ICS
- 49.020
- Classification
- V 35
Issued by: State Administration for Market Regulation; Standardization Administration of the PRC
Contents
- Foreword
- 1 Scope
- 2 Normative references
- 3 Test conditions
- 3.1 Device under test
- 3.2 Vibration test category
- 3.3 Standard vibration test conditions
- 3.4 Transport vibration test conditions
- 4 Test equipment and instruments
- 4.1 General requirements
- 4.2 Control tolerance requirements
- 5 Test process
- 5.1 Random vibration test process
- 5.2 Sinusoidal vibration test process
- 5.3 Sine superposition random vibration test process
- 6 Test interruption and resumption
- 6.1 Interruption and recovery of undertest
- 6.2 Interruption and recovery after the test
- 7 Evaluation of test results
- 8 Test report
- Appendix A (Normative Appendix) Vibration Test Conditions
1 Scope
This part of GB/T 38924 specifies the civil light and small unmanned aerial vehicle (take-off weight 0.25kg~150kg) system (including aircraft and
Ground station) vibration test requirements and methods, including test conditions, test equipment and instruments, test process, test interruption and recovery, test results
Evaluation and test reports, etc.
This part is applicable to light and small civilian use (maximum take-off weight greater than 0.25kg) that may experience a vibration environment during transportation and use.
And not more than 150kg) multi-rotor UAV system, fixed-wing UAV system, unmanned helicopter system and vehicle-mounted ground station to determine
Whether the civil light and small UAV system can withstand the impact of the vibration environment.
2 Normative references
The following documents are indispensable for the application of this document. For dated reference documents, only the dated version applies to this article
Pieces. For undated references, the latest version (including all amendments) applies to this document.
GB/T 35018 Classification and classification of civil unmanned aircraft systems
3 Test conditions
3.1 Device under test
3.1.1 Requirements for the equipment under test
The equipment under test shall meet the following requirements.
a) The technical status of the tested equipment should be consistent with the content of the submitted product information;
b) The number of tested equipment should meet the test requirements, and the number of tested equipment should be at least one set;
c) The tested equipment should have quality inspection certificates such as enterprise qualification certificates.
3.1.2 Equipment classification
According to the requirements in GB/T 35018, the test equipment is divided into the following categories according to the configuration.
a) The multi-rotor UAV system is determined to be a Class A equipment;
b) The fixed-wing UAV system is determined to be a Class B equipment;
c) The unmanned helicopter system is determined to be a Class C equipment;
d) The ground station (vehicle) is determined as a Class D equipment.
3.2 Vibration test category
The vibration test categories of different equipment categories and power forms of UAV systems are shown in Table 1.
......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 15 pages — is available in the English PDF.
Referenced standards
Similar standards
How to Download GB/T 38924.6-2020
- 1
Add to cart
Click "Download PDF" on this page and choose "Buy this standard". You can add more standards before checkout.
- 2
Checkout
Enter your email and billing details. Payment is processed securely by Stripe (cards or bank transfer). Prefer bank details? Request a quotation (min. order $300).
- 3
Instant delivery (0–9 sec)
Delivery is automatic: within seconds of payment you'll receive an email with a secure download link. The link stays valid for 72 hours.
- 4
Invoice included
A tax invoice is attached to the confirmation email. Need a custom invoice? Contact us.
Related Standards
GB/T 38924.1-2020 — Environmental test methods for civil small and light unmanned aircraft system—Part 1: General principles
GB/T 38924.10-2020 — Environmental test methods for civil small and light unmanned aircraft system - Part 10: Sand and dust test
GB/T 38924.11-2023 — Environmental test methods for civil small and light unmanned aircraft system—Part 11: Fungus test
Secure payment via Stripe
Payments accepted
GB/T 38924.6-2020
$195.00