Large amphibious aircraft hull watertight detection system and method

An amphibious aircraft and detection system technology, which is applied in the direction of using liquid/vacuum degree for liquid tightness measurement and measuring the acceleration and deceleration rate of fluid, etc., can solve the difficulty of leakage point detection, large volume, and the need for space for spray devices. and other problems, to achieve the effect of easy production and application, huge economic benefits, and simple production

Active Publication Date: 2021-03-09
中航通飞华南飞机工业有限公司
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AI Technical Summary

Problems solved by technology

The spraying device requires a site and is large in size, and cannot be flexibly carried out in the field, so it is suitable for use in the manufacturing stage; when static water immersion and external vacuuming are used to conduct watertight tests on the hull, it cannot truly reflect the water pressure on the hull during sliding
During the outfield water test flight of a large amphibious aircraft, none of the above watertight test methods can meet the watertight test requirements of the outfield water test flight, which brings many difficulties to the detection of leakage points

Method used

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  • Large amphibious aircraft hull watertight detection system and method
  • Large amphibious aircraft hull watertight detection system and method
  • Large amphibious aircraft hull watertight detection system and method

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Embodiment Construction

[0018] The purpose of the invention is to quickly, conveniently and accurately detect the leakage point of the hull in the outfield when the aircraft finds hull leakage during the water test flight in the outfield, so as to help eliminate hidden dangers of the aircraft and reduce the risk of subsequent flight tests. In order to achieve the above object, the present invention provides a large-scale amphibious aircraft hull watertight detection system and method, the following in conjunction with the attached Figure 1 to Figure 4 The present invention will be described in detail.

[0019] Such as figure 1 Shown:

[0020] The implementation of the present invention provides a large-scale amphibious aircraft hull watertight detection system, including a pool 3, a water pump 4, a leak detection plate 5, a vent valve 8, a pressure gauge 7, a manual overflow valve 6, and a water pipe 9; wherein the pool 3, The water pump 4, the manual overflow valve 6 and the water pipe 9 constitu...

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Abstract

The invention belongs to the field of amphibious aircraft hull watertight detection process methods, and particularly relates to a large amphibious aircraft hull watertight detection system and method. The watertight detection system comprises a water pool (3), a water pump (4), a leakage detection disc (5), a vent valve (8), a pressure gauge (7), a manual adjustment type overflow valve (6) and awater pipe (9). By means of the detection system and method, leakage points can be rapidly detected. The method is a positive-pressure watertight detection method, the detection pressure is adjustable, and the stress condition of an airplane during underwater gliding can be actually and truly restored. The detection system device is simple in structure, small in size, easy to manufacture, very convenient and flexible to use when used for outfield overwater test flight and easy to produce and apply, an airplane manufacturer can deliver the detection system device to a client as a random tool, and huge economic benefits are brought.

Description

technical field [0001] The patent of the present invention belongs to the field of amphibious aircraft hull watertight detection process method, in particular to a large-scale amphibious aircraft hull watertight detection system and method. Background technique [0002] During the manufacturing process of large-scale amphibious aircraft, watertightness tests are carried out on the fuselage of the aircraft, and sealing test methods such as spraying devices, static immersion, and external vacuuming methods are often used. When a large amphibious aircraft is flying on the water in the outfield, the leakage of the hull is unavoidable, and leakage often occurs at the rivet holes and the joints of the fuselage. Finding and repairing the leak quickly and accurately can stop the leak from getting worse. The spraying device requires a site and is large in size, and cannot be flexibly carried out in the field. It is suitable for use in the manufacturing stage; static water immersion ...

Claims

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Application Information

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IPC IPC(8): G01M3/26
CPCG01M3/26
Inventor 杨敏范文康罗海勇马笑天苑春华
Owner 中航通飞华南飞机工业有限公司
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