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CN-121982951-A - Real standard system of real fire of integrated aircraft fire rescue

CN121982951ACN 121982951 ACN121982951 ACN 121982951ACN-121982951-A

Abstract

The invention discloses an integrated fire-fighting rescue real-fire training system for an aircraft, which comprises a support frame assembly, a profiling shell assembly, profiling wings, a profiling engine, a profiling wheel carrier, a profiling seat, a central control system and a disaster simulation system. The cooperation setting through support frame assembly, profile modeling shell assembly, profile modeling wing and profile modeling wheel carrier has possessed the effect that the degree of emulation is high, the cooperation setting through profile modeling shell assembly, profile modeling wing, central control system and disaster simulation system has possessed the effect that real standard potential safety hazard is little, the cooperation setting through profile modeling shell assembly, profile modeling engine, profile modeling wheel carrier and central control system and disaster simulation system has possessed the construction cycle short, can avoid on-the-spot environment to disturb construction improvement technological quality, can reduce on-the-spot operation risk, avoid polluting the environment and reduce the effect of construction degree of difficulty.

Inventors

  • JIN ZHEN

Assignees

  • 北京鑫辰时代科技有限公司

Dates

Publication Date
20260505
Application Date
20260226

Claims (8)

  1. 1. The utility model provides an integrative aircraft fire control rescue real fire practical training system, includes support frame assembly (1), profile modeling shell assembly (2), profile modeling wing (3), profile modeling engine (4), profile modeling wheel carrier (5), profile modeling seat (6), central control system (7) and disaster simulation system (8), wherein profile modeling shell assembly (2) include profile modeling aircraft nose (201), preceding cut off between (202), profile modeling fuselage (203), back cut off between (204) and five regions between tail (205), profile modeling shell assembly (2) fixed mounting is in support frame assembly (1) top, profile modeling wing (3) fixed mounting is in profile modeling shell assembly (2) one side, profile modeling engine (4) and profile modeling wheel carrier (5) are installed in profile modeling wing (3) below, profile modeling seat (6) fixed mounting is in the interior bottom surface of profile modeling fuselage (203), central control system (7) set up in tail (205), disaster simulation system (8) are integrated in profile modeling aircraft nose (201) and profile modeling fuselage (203).
  2. 2. The integrated fire rescue training system for the aircraft fire protection is characterized in that the support frame assembly (1) comprises a plurality of upright posts and cross beams forming a rectangular frame, the upright posts are perpendicular to the ground, the rectangular frame formed by the cross beams is parallel to the ground, the width dimension of the rectangular frame is identical to that of the profiling shell assembly (2), and the profiling shell assembly (2) is fixedly arranged on the upper surface of the rectangular frame formed by the cross beams.
  3. 3. The integrated fire-fighting rescue real-fire training system for the aircraft according to claim 1, wherein the frame of the profiling shell assembly (2) is formed by welding rectangular steel pipes, the bottom surface is a steel plate with a flat surface, the profiling nose (201) is formed by shaping the steel plate, and the rest of the outline shell and the partition plates among the five areas are of a composite structure of double-layer steel plate rock wool.
  4. 4. The integrated fire rescue and true fire training system for the aircraft fire protection as claimed in claim 1, wherein a body-side simulation cabin door (2031) is arranged on one side, close to the profiling nose (201), of the profiling fuselage (203), a side emergency door (2032) is arranged on one side, close to the profiling wing (3), of the profiling fuselage (203), a fence (301) is arranged on the upper surface of the profiling wing (3), the body-side simulation cabin door (2031) has an arc-shaped fuselage structure of a real aircraft, and replaceable puncture panels are respectively arranged in the directions of 8 o 'clock and 10 o' clock.
  5. 5. The integrated fire rescue real fire training system for the aircraft fire protection according to claim 1, wherein front partition simulation doors (2021) are arranged on two sides of a front partition room (202), rear partition simulation doors (2041) are arranged on two sides of a rear partition room (204), an openable simple door is arranged between the profiling machine body (203) and the front partition room (202), and a channel capable of directly passing through is arranged between the profiling machine body (203) and the rear partition room (204).
  6. 6. The integrated fire rescue real training system for aircraft fire protection according to claim 1, wherein the disaster simulation system (8) is provided with a middle fuel pipe (801) and side fuel pipes (802), the middle fuel pipe (801) is fixedly installed at a middle position above the profiling nose (201) and the profiling machine body (203), and the side fuel pipes (802) are fixedly installed at two sides above the profiling nose (201) and the profiling machine body (203).
  7. 7. The integrated fire rescue real fire training system for the aircraft according to claim 1, wherein the ladder (9) is arranged at the rear part and the side surface of the tail room (205), and a rear observation window (2051) is arranged at the middle position between the tail room (205) and the rear partition room (204).
  8. 8. The integrated fire-fighting rescue real-fire training system for the aircraft according to claim 1 is characterized in that the lower parts of the profiling engine (4) and the profiling wheel frame (5) are supported in contact with the ground, the upper parts of the profiling engine and the profiling wheel frame are fixedly connected with the profiling wing (3), and one side of the profiling wing (3) is fixedly connected with the profiling shell assembly (2) in a welding mode.

Description

Real standard system of real fire of integrated aircraft fire rescue Technical Field The invention relates to the technical field of fire-fighting rescue practical training equipment, in particular to an integrated fire-fighting rescue practical training system for an aircraft, which is suitable for fire-fighting rescue practical training of various types of civil aviation, military aircraft and the like. Background With the rapid development of the air transportation industry, the emergency rescue requirement of the fire accident of the aircraft is urgent increasingly, because the aircraft has complex structure, airtight cabin space and rapid fire spreading speed, extremely high requirements are put forward on the actual combat ability of fire fighters, in order to improve the emergency rescue ability of fire fighters to the fire accident of the aircraft, the actual fire training of the fire fighters of the aircraft is needed, however, the prior actual fire training system of the fire fighters of the aircraft has some defects in the use process: the simulation degree is low, the existing fire-fighting rescue real-fire training system of the aircraft generally consists of a plurality of independent real-training modules, such as a fuselage fire real-training module, an engine fire real-training module and a nose fire real-training module, but the fire of the aircraft is generally continuous in practice, so that the modularized fire real-training and the real fire scene are greatly different. The potential safety hazard is large, the fire in the airtight profiling machine body is fierce, if errors occur in the training process, people can not timely find and escape, and life threat is easily caused to fire fighters. The construction period is long, each working procedure on site needs to be sequentially advanced, and links such as structure construction, component installation, pipeline laying, system debugging and the like are overlapped, so that the whole construction period is long, and the requirement of quick application of a practical training field cannot be met. The process quality is not easy to control due to strong environment dependence, and site construction is easy to be interfered by weather (high temperature, rain and snow, typhoon), traffic (equipment transportation delay), site limitation (peripheral barriers, insufficient construction space) and other factors. The construction method has the advantages of high risk of field operation, high construction difficulty, more operation links such as field fire welding, gas/waterway pipeline field splicing and the like, high fire safety risk, easiness in noise generation and dust pollution, environment protection failure, lack of large-scale tool equipment such as crane slings for field construction, low continuity of work connection, and increased renting cost and coordinated time cost. Disclosure of Invention (One) solving the technical problems Aiming at the defects of the prior art, the invention provides an integrated real fire training system for fire rescue of an aircraft, which has the advantages of high simulation degree and small potential safety hazard, and solves the problems of low simulation degree and large potential safety hazard. (II) technical scheme The invention provides a technical scheme for realizing the purposes of high simulation degree and small potential safety hazard, which comprises a support frame assembly, a profiling shell assembly, a profiling wing, a profiling engine, a profiling wheel frame, a profiling seat, a central control system and a disaster simulation system, wherein the profiling shell assembly comprises five areas of a profiling machine head, a front partition room, a profiling machine body, a rear partition room and a tail room, the profiling shell assembly is fixedly arranged above the support frame assembly, the profiling wing is fixedly arranged on one side of the profiling shell assembly, the profiling engine and the profiling wheel frame are arranged below the profiling wing, the profiling seat is fixedly arranged on the inner bottom surface of the profiling machine body, the central control system is arranged in the tail room, and the disaster simulation system is integrated in the profiling machine head and the profiling machine body. Preferably, the support frame assembly comprises a plurality of stand columns and cross beams forming a rectangular frame, the stand columns are perpendicular to the ground, the rectangular frame formed by the cross beams is parallel to the ground, the width dimension of the rectangular frame is identical to that of the profiling shell assembly, and the profiling shell assembly is fixedly arranged on the upper surface of the rectangular frame formed by the cross beams. Preferably, the frame of the profiling shell assembly is formed by welding rectangular steel pipes, the bottom surface is a steel plate with a flat surface, the profiling machine head is formed by sh