Non-blocking landing system for shipboard aircraft of aircraft carrier
By setting up a landing runway with rolling strong round steel bodies on the deck of the aircraft carrier, the carrier-based aircraft automatically stops through inertia taxiing, which solves the damage problem of the blocking cables to carrier-based aircraft and pilots in the prior art, reduces maintenance costs and complexity, and improves the wartime navigation capacity.
Patent Information
- Application Number
- CN202510131596.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-02-06
- Publication Date
- 2025-05-13
AI Technical Summary
In the existing aircraft carrier-based aircraft landing system, the blocking cable causes physical damage to the carrier-based aircraft structure, affects its life, and causes hidden damage to the pilots. At the same time, the blocking cable is costly, easy to lose, complex construction and maintenance, and low safety.
The unobstructed landing system is adopted. By setting up a landing runway with strong round steel bodies on the deck of the aircraft carrier, the carrier-based aircraft will glide through inertia after landing. The rolling runway forms a relative rolling with the carrier-based aircraft wheels, and the carrier-based aircraft will automatically stop using inertia friction.
The damage problem of the blocking cable to carrier-based aircraft and pilots has been completely solved, the maintenance cost and complexity has been reduced, and the wartime navigation capacity of carrier-based aircraft has been improved without the need for high-cost blocking cables.
Smart Images

Figure CN119975818A_ABST
Abstract
Description
Technical Field
[0001] The present invention belongs to the technical field of aircraft carrier landing, and in particular relates to an unobstructed landing system for aircraft carrier landing. Background Art
[0002] At present, the landing of aircraft carriers relies on the aircraft to accelerate into the landing area and be stopped by the arresting cable. The reaction force causes great physical damage to the structure of the aircraft carrier, affecting the life of the aircraft carrier. At the same time, it causes hidden damage to the pilot's lumbar spine, cervical spine and eyes. The pilots take off and land less frequently, which cannot meet the needs of wartime and weakens the combat capability. The arresting cable is expensive and easy to wear. The construction of the arresting cable system is technically complex, with a long cycle, high maintenance cost, low safety, and easy to break. Occasionally, the hook cannot hook the arresting cable, resulting in a go-around or a safety accident. The amount of ammunition carried by the carrier-based aircraft is closely related to the combat effectiveness of the carrier-based aircraft, and the weight affects the arresting cable landing method and the landing of the carrier-based aircraft. Summary of the invention
[0003] The purpose of the present invention is to change the carrier-based aircraft landing system and provide an unobstructed landing system for carrier-based aircraft on an aircraft carrier, so as to completely solve the problems existing in the above-mentioned prior art. BRIEF DESCRIPTION OF THE DRAWINGS
[0004] Attached Figure 1 The structure diagram of the unobstructed landing system for aircraft carriers of the present invention is shown in FIG. The aircraft carrier landing aircraft touches down at the landing point (2), and its inertia glides to the rolling runway (1) of the aircraft carrier. The wheels of the aircraft carrier roll relative to the rolling runway, and the inertia force is unloaded, and the friction force is lost, so that the aircraft carrier stops. DETAILED DESCRIPTION
[0005] As shown in the figure, the unobstructed landing system for aircraft carriers of the present invention includes a set of unobstructed carrier landing runways of rolling strong round steel bodies arranged along the original runway. The length and width of the runway are set comprehensively according to objective factors such as different types of carrier aircraft. Each rolling round steel body is set on the carrier body, flush with the deck, and has special rolling bearings or needle bearings at both ends, and each end is provided with a solid lubricant oiling nozzle. When the carrier aircraft lands, it slides into the rolling runway, and the rolling strong round steel cylinder of the runway and the wheels of the carrier aircraft form relative rolling, with extremely small rolling force. The inertial friction of the carrier aircraft is unloaded on the rolling runway, and the carrier aircraft can automatically stop landing without being blocked.
[0006] The above invention is based on the principles of physics, but the invention is not limited to the contents disclosed in the invention, so all modifications similar to or expanded upon the disclosure of the invention are within the protection scope of the invention.
Claims
1. An unobstructed landing system for aircraft on an aircraft carrier, characterized in that: The carrier aircraft unobstructed landing system for carrier aircraft includes (1) a rolling runway for unobstructed carrier aircraft landing, which is arranged along the original runway position. The length and width of the runway are comprehensively set according to objective factors such as different types of carrier aircraft. Each rolling round steel cylinder is arranged on a carrier body, flush with the deck, and has special rolling bearings or needle bearings at both ends. Each end is provided with a solid lubricant injection nozzle. When the carrier aircraft lands (2) and slides into the rolling runway (1), the rolling strong steel cylinder forms relative rolling friction with the wheels of the carrier aircraft, so that the carrier aircraft loses friction and unloads inertia, and the rolling landing stops.
2. The unobstructed landing system for aircraft carriers according to claim 1, characterized in that: The wheels of the carrier-based aircraft and the rolling body of the unobstructed landing system roll relative to each other, unloading the inertial force and stopping naturally.
3. The unobstructed landing system for aircraft carriers according to 2 is characterized by: The principle of relative rolling friction is applicable to military airports on artificial reclaimed islands.
4. The unobstructed landing system for aircraft carriers according to 2 is characterized by: The principle of relative rolling friction is suitable for temporary landing airports during wartime.
5. The unobstructed landing system for aircraft carriers according to 2 is characterized by: The principle of relative rolling friction can be used to build a mobile landing airport in wartime, that is, a vehicle-mounted mobile airport.