Separate assembly of a parachute, parachute system for aircraft recovery
A technology for separating components and aircraft, which is applied to the systems of aerospace vehicles returning to the earth's atmosphere, parachutes, and landing devices of aerospace vehicles, etc. It can solve the problems of long launch period, heavy rocket landing impact, and lack of a mature design. The effect of improving the flight safety factor, increasing the exit angle, and eliminating the risk of collision
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0045] The main technical solutions and design ideas of the separation assembly of the present invention are:
[0046] The separation component includes a base, a separation flap, a spring hinge, a rubber spacer, and a partition. The rubber spacer and the separation flap are bonded to form a flap assembly. The separation flap and the spring hinge are connected by screws, and the spring hinge is made of Screws are connected to the base, that is, the flap assembly is fixed by a spring hinge; the partition divides the opening of the base into multiple rope slots, and the paracord or sling is separated by the partition in the rope slot to ensure that different paracords Or the slings will not interfere with each other when pulled out. The two ends of the separation flap are designed with guide angles to ensure that when the paracord or sling is pulled out from any direction at both ends, it will move toward the center line under the guidance of the separation flap and come out fro...
Embodiment 2
[0052] The main technical solutions and design ideas of the parachute system of the present invention are:
[0053] The parachute system of the present invention includes a deceleration parachute, a deceleration parachute strap, a deceleration parachute front suspension point support, a deceleration parachute rear suspension point support, a conversion suspender, a deceleration parachute rear suspension point unlocking bolt, a main parachute, a main parachute suspension strap (three), a main The front suspension point support of the canopy, the rear suspension point support of the main canopy (two), the main canopy cover, the unlocking bolt of the main canopy cover, and the separation assembly.
[0054] The drogue parachute strap is used to connect the drogue parachute and the drogue parachute rear suspension point support; the drogue parachute rear suspension point support is located behind the center of mass of the aircraft, used to fix the drogue parachute strap and conversi...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com