Power lifting rescue platform for pilot in distress

A pilot and power technology, applied in aircraft parts, cranes, ground devices, etc., can solve problems such as poor rescue ability, operator injury, complex mechanical structure of unpowered cranes, etc., to achieve the effect of wide application models and ensuring aircraft safety.

Inactive Publication Date: 2021-09-07
FOURTH MILITARY MEDICAL UNIVERSITY
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Quickly leaving the cockpit for pilots in distress and providing timely treatment is an important link and means to protect the lives of pilots, promote flight safety, and enhance combat effectiveness. The field ambulance team is also equipped with a variety of ambulance devices, including field ambulances, combined life-saving ladders, ambulance stretchers, unpowered cranes and other rescue devices. The failure rate of the sling device is high, and the winch device is easy to cause injury to the operator. The maximum height of the life-saving ladder is 3.2 meters, which can only meet the medical needs of the pilots in the front cabin of the second-generation aircraft and the Su-27 two-seater aircraft, and it is difficult to meet the emergency rescue of the third-generation fighter jets. Requirements, for the pilots in the rear cockpit of Su-27, it is difficult to reach the life-saving ladder, and the life-saving ladder sling device cannot meet the hoisting requirements under the low-angle coverage of the rear seat canopy, and it is impossible to effectively disembark the pilot. The front wing of the aircraft is blocked, and the rescue ladder cannot meet the off-board rescue needs of the pilots in the rear compartment of the two-seater fighter with the front wing. The unpowered crane adopts the form of a trailer, which consists of a QG0.85 trailer chassis, a telescopic boom, a rescue ladder and a hanging plate Composed of slings, it is mainly suitable for rescue on good roads such as runways, taxiways, and contact roads in the flight area. There are unpowered cranes with complex mechanical structures, and all operations are manual operations. The rescue ladder is used together and requires at least 3 people to operate together. The rescue process is relatively cumbersome. It takes a long time for the pilot to leave the cockpit for rescue, and the unpowered crane has poor mobility. It is impossible to safely implement fast maneuvering and cornering, the pilot lacks effective support during the process of leaving the aircraft, and the pilot is prone to rapid rotation when the crane is lowered. The safety is low, and it cannot meet the emergency rescue needs of the third-generation fighters.
[0003] The existing ambulance devices for pilots in distress can no longer meet the emergency rescue needs of three-generation and above fighters. At present, the main problems in the rescue of air force pilots in distress are as follows:
[0004] (1) Rescue capability is poor. Using combined life-saving ladders and rescue equipment for pilots to rescue pre-distressed pilots can only meet the rescue needs of the pilots in the front cabin of the second-generation aircraft and the Su-27 two-seater aircraft, and it is difficult to meet the needs of the rear cabin of the two-seater aircraft and the third-generation new aircraft. The emergency rescue needs of fighter planes;
[0005] (2) The treatment efficiency is low, using the existing emergency rescue equipment, the labor intensity is high, the operation time is long, and the efficiency is low, so it is difficult to carry out rapid rescue of pilots;
[0006] (3) The mode is single and the adaptability is poor. Existing pilots in distress quickly leave the cockpit after an emergency landing.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Power lifting rescue platform for pilot in distress
  • Power lifting rescue platform for pilot in distress
  • Power lifting rescue platform for pilot in distress

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0033] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0034] see Figure 1-Figure 8 , a power hoisting and rescue platform for pilots in distress, including an operation cabin 1, a connecting arm member 2, a hoisting mechanism 3, a forward tilt door 4, a cabin door 5, an operating rod 6, a searchlight 7 and a console 8, the operation cabin 1 An installation chamber 9 is provided on the right side of the upper side, and one end of the connecting arm member 2 is installed in the installation chamber 9. The hoisting...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses a power lifting rescue platform for a pilot in distress, and relates to the technical field of rescue equipment for the pilot in distress. The platform comprises an operation cabin, a connecting arm component, a hoisting mechanism, a forward inclined door, a cabin door, an operation rod, a searchlight and a control console, an installation cavity is formed in the right side of the operation cabin, one end of the connecting arm component is installed in the installation cavity, the hoisting mechanism is installed in the operation cabin, and a linear sliding rail is laid between the bottom of the hoisting mechanism and the inner bottom of the operation cabin; the lifting mechanism is arranged in the operation cabin and is in sliding connection with the operation cabin through a linear sliding rail, a punching plate is laid at the inner bottom of the operation cabin, a quick pressing clamp is installed on the lifting mechanism, and a pressing head part of the quick pressing clamp is pressed into the punching plate. The power lifting rescue platform for the pilot in distress is used for enabling the pilot in distress to quickly leave a cabin after the main battle aircraft of our army lands, has an autonomous power lifting rescue function, can finish the lifting rescue process of the pilot only by one rescue worker, and guarantees the first-line rescue capability of an air force field station hospital.

Description

technical field [0001] The invention relates to the technical field of rescue equipment for pilots in distress, in particular to a power hoisting and rescue platform for pilots in distress. Background technique [0002] Quickly leaving the cockpit for pilots in distress and providing timely treatment is an important link and means to protect the lives of pilots, promote flight safety, and enhance combat effectiveness. The field ambulance team is also equipped with a variety of ambulance devices, including field ambulances, combined life-saving ladders, ambulance stretchers, unpowered cranes and other rescue devices. The failure rate of the sling device is high, and the winch device is easy to cause injury to the operator. The maximum height of the life-saving ladder is 3.2 meters, which can only meet the medical needs of the pilots in the front cabin of the second-generation aircraft and the Su-27 two-seater aircraft, and it is difficult to meet the emergency rescue of the t...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/00B66C23/20B66C23/36B66C23/30
CPCB64F1/00B66C23/202B66C23/36B66C23/30
Inventor 刘天帅孙业勤卢虹冰刘洋燕强杜鹏戎军艳孙珺
Owner FOURTH MILITARY MEDICAL UNIVERSITY
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products