SKID type landing gear for helicopters
The skid type landing gear for helicopters addresses load distribution and impact absorption issues by incorporating an energy-absorbing leaf spring and compressive bearing housings, ensuring safe landings on diverse terrains.
WO2026117205A1PCT designated stage Publication Date: 2026-06-04KARPAT FATIH +1
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Patent Information
- Application Number
- PCT/TR2025/050871
- Authority / Receiving Office
- WO · WO
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2025-07-31
- Publication Date
- 2026-06-04
AI Technical Summary
Technical Problem
Existing skid type landing gears for helicopters fail to evenly distribute load and absorb impact effectively during landings on different surfaces and in cases of falling, lacking essential components like main springs, bearing housing structures, and retainer parts.
Method used
A skid type landing gear with a composite structure featuring an energy-absorbing leaf spring, compressive bearing housings, carrier beams, and retainer parts that distribute load evenly and absorb impact through flexible components.
Benefits of technology
The gear provides high strength and longevity by minimizing impact effects on varied surfaces and in falling scenarios, offering protection against ground reaction forces and allowing safe landings on soft and rough terrains.
✦ Generated by Eureka AI based on patent content.
Smart Images
Figure TR2025050871_04062026_PF_FP_ABST
Abstract
The invention relates to a skid type landing system for helicopters with a composite structure, which has an energy absorbing leaf spring and a compressive bearing housing structure, comprises carrier beams and retainer elements, and minimizes the impact effect in landings on different surfaces and in cases such as falling.
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