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pressure control system terminal pressure ≤0.385mpa pressure control system aircraft hydrant dispenser introduction interpretation differential pressure gauge accuracy ≤0.2 level api water hammer pressure ≤0.84mpa api main quality class non-alloy steels lignin water pressure pulsation
MH/T 6100-2013 in English

MH/T 6100-2013 in English

VALID

Aircraft hydrant dispenser

  • Issued on:2013-09-27
  • Implemented on:2014-01-01
  • File Format:PDF
  • Delivery:Via email within 2~4 business days
Price(USD): $399.00
$388.00
Standard No: MH/T 6100-2013
Document status: VALID
Title in English: Aircraft hydrant dispenser
Title in Chinese: 飞机管线加油车
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 2~4 business days
Issued on: 2013-09-27
Implemented on: 2014-01-01
ICS Classification: 49.100-Ground service and maintenance equipment
Chinese Classification: V57-Special vehicles
Professional Classification: MH-Civil Aviation
Related Keywords: pressure control system terminal pressure ≤0.385mpa
pressure control system
aircraft hydrant dispenser introduction interpretation
differential pressure gauge accuracy ≤0.2 level api
water hammer pressure ≤0.84mpa api


Introduction

Interpretation of the core content of the standard

Technical module Key indicators International benchmarking
Filter separator In compliance with GB/T 21358 or API 1581, differential pressure gauge accuracy ≤0.2 level API 1581 Class 3
Pressure control system Terminal pressure ≤0.385MPa, water hammer pressure ≤0.84MPa API 1540 Annex B
Static conductivity system Pipeline resistance ≤5Ω, hose resistance ≤1MΩ NFPA 407 Chapter 5

Analysis of key technical requirements

Clause 4.8.5.10 stipulates that the pressure control system must achieve dual adjustment:
1) Ground well connector Venturi controls the main flow (10-15s open/3-5s closed)
2) Pressure refueling connector regulator performs terminal fine adjustment


Safety interlock mechanism

Standard Clause 4.8.7 requires 11 interlock states to trigger vehicle braking, including:
• The platform is raised but not reset (forced braking when the height is ≥2.7m)
• The static conductive device is not connected (locked when the resistance value exceeds the standard)
• The power take-off engagement state is abnormal

Implementation suggestions

1. The filter separator should be tested for differential pressure every 500 hours. When the pressure difference is greater than 0.1MPa, the filter element needs to be replaced
2. The pressure test should use 1.25 times the rated pressure to maintain the pressure for 5 minutes, and focus on checking the welded joints
3. If the static conductive drag zone is worn by more than 30%, it should be replaced immediately (refer to JT 230)

Sample only — not a preview of MH/T 6100-2013
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