一种氢燃料电池无人机石墨板流道
By setting a nanoscale hydrophobic coating and a cross-flow structure inside the graphite plate flow channel of a hydrogen fuel cell drone, combined with elastic buffer pads and bolted connections, the sealing and flow problems of the graphite plate flow channel are solved, improving reaction efficiency and battery stability, and extending the flight time.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- JI YONG QING NENG YUAN KE JI (JIANG SU) YOU XIAN GONG SI
- Filing Date
- 2025-08-20
- Publication Date
- 2026-07-17
AI Technical Summary
The existing graphite plate flow channel design is simple, lacks an efficient collaborative structure between the cathode and anode graphite plates, and the air and hydrogen fuel flow in a single direction, resulting in uneven distribution of reactants and affecting the battery output power; the connection is not stable and is prone to loosening, resulting in poor sealing and posing a safety hazard; moisture easily accumulates on the inner wall of the flow channel, hindering gas flow and affecting battery life.
A nano-level hydrophobic coating is installed inside the graphite plate flow channel of the hydrogen fuel cell drone. A cross-flow structure design is adopted, combined with elastic buffer pads and bolt fixing connections to enhance sealing and stability. Heat dissipation holes and cooling fans are set to prevent moisture accumulation and dissipate heat in a timely manner.
It improves reaction efficiency, ensures smooth gas flow, enhances structural stability and heat dissipation, and extends battery life and range.
Smart Images
Figure CN224519882U_ABST
Abstract
Claims
1. A hydrogen fuel cell drone graphite plate flow channel, comprising a drone battery module body, characterized in that, The UAV battery module body includes end plates (1) disposed on both sides of the UAV battery module body. A multi-layer graphite plate structure (2) is disposed between the two end plates (1). The graphite plate structure (2) includes a cathode graphite plate (3) and an anode graphite plate (4). A connecting insulating plate (5) is disposed on the outside of the graphite plate structure (2). The graphite plate structure (2) is fixed to the two end plates (1) through the connecting insulating plate (5). A hydrogen fuel interface (6) and an air interface (7) are respectively disposed on the upper and lower sides of the end plates (1).
2. The hydrogen fuel cell drone graphite plate flow channel of claim 1, wherein, A membrane electrode (8) is provided between the cathode graphite plate (3) and the anode graphite plate (4). The cathode graphite plate (3) and the anode graphite plate (4) are identical and have a rectangular overall structure. Multiple air channels (9) and hydrogen fuel channels (10) are provided on one side of the graphite plate structure (2). The air flow direction of the air channel (9) is perpendicular to the hydrogen fuel flow direction of the hydrogen fuel channel (10), and a cross-flow structure is adopted.
3. The hydrogen fuel cell drone graphite plate flow channel of claim 2, wherein, The inner walls of the air channel (9) and the hydrogen fuel channel (10) are provided with a nano-scale hydrophobic coating (11).
4. The hydrogen fuel cell drone graphite plate flow channel of claim 1, wherein, The end plate (1) is provided with multiple mounting holes (12), and the connecting insulating plate (5) is fixedly connected to the end plate (1) by bolts passing through the mounting holes (12).
5. The graphite plate flow channel for a hydrogen fuel cell drone according to claim 1, characterized in that, A buffer pad (13) is provided between the connecting insulating plate (5) and the end plate (1). The buffer pad (13) is made of elastic material. The buffer pad (13) is provided with heat dissipation holes (14), which are arranged in multiple rows.
6. The hydrogen fuel cell drone graphite plate flow channel of claim 1, wherein, A smooth plate (15) is provided on the outside of the graphite plate structure (2). The graphite plate structure (2) is fixed to the graphite plate structure (2) by the smooth plate (15). The smooth plate (15) is a flat plate structure that fits tightly with the graphite plate structure (2).
7. The hydrogen fuel cell drone graphite plate flow channel of claim 1, wherein, A protective shell (16) is provided on the outer side of the end plate (1), and a heat dissipation exhaust port (17) is provided on one side of the protective shell (16). A heat dissipation exhaust port (17) is provided with a heat dissipation fan (18) on the protective shell (16).