Marine Rocket Erection Device Guide Member Mechanism

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing marine rocket launch systems fail to achieve stable and effective hot launches due to the damage caused by high-temperature flames on the erection device and wire ropes, which are not suitable for marine hot launches.

Innovation Solution

An erection device for marine hot launches, comprising a launch vessel with a guide member, driving cylinder, sliding member, and connecting member, which allows for synchronized movement and orientation of the rocket, avoiding side loads and high temperatures, ensuring stability and preventing hydraulic seal damage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a hydraulic cylinder with soft rubber sealing is used to erect the rocket, then the erection function is achieved, but the rubber sealing is damaged by side loads from ship movement causing hydraulic oil leakage

Engineering Contradiction:
Improveerection functionVSAvoidhydraulic seal reliability
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

A guide member is introduced as an intermediary component between the sliding member and the driving cylinder. The guide member constrains the sliding member to move only along its longitudinal direction, preventing side loads from transmitting to the driving cylinder. This mediator protects the hydraulic seal from damage while maintaining the erection function.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The erection system is segmented into distinct functional components: the driving cylinder provides driving force, the sliding member translates this force, and the guide member constrains the motion path. This segmentation isolates the hydraulic cylinder from side loads by separating the driving function from the guiding function.

Inventive Principle:
Principle #1Segmentation

2Reliability

If a backup hydraulic system is set up to ensure launch quality, then the reliability is improved, but the space requirement exceeds the limited space on the launch vessel

Engineering Contradiction:
Improvelaunch qualityVSAvoidspace on launch vessel
Core Design Contradiction:
ReliabilityVSVolume of moving object

Solution Approach 1:

The guide member is installed beforehand to prevent side loads from affecting the driving cylinder during operation. This prior protective measure eliminates the need for backup hydraulic systems while maintaining launch quality, as the single hydraulic system operates without side load contamination.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

3Productivity

If the driving cylinder is positioned close to the rocket for efficient erection, then the erection efficiency is improved, but the high-temperature flame damages the hydraulic system

Engineering Contradiction:
Improveerection efficiencyVSAvoidhigh-temperature flame damage
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The driving cylinder is extracted from the high-temperature zone near the rocket and positioned at a safe distance. The connecting member (sliding member and connecting rod) acts as an extended mechanism to transmit the driving force from the remote cylinder to the rocket, maintaining erection efficiency while protecting the hydraulic system from thermal damage.

Inventive Principle:
Principle #2Taking out (Extraction)

4Adaptability or versatility

If the ship moves at sea with horizontal acceleration and tilting, then the marine launch capability is achieved, but side forces are generated on the erection device

Engineering Contradiction:
Improvemarine launch capabilityVSAvoidside force on erection device
Core Design Contradiction:
Adaptability or versatilityVSForce

Solution Approach 1:

The guide member changes the dimension of motion constraint by allowing movement only along its longitudinal axis while preventing movement in perpendicular directions. This dimensional constraint isolates the driving cylinder from side forces generated by ship motion, enabling marine launch capability without transmitting harmful forces to the hydraulic system.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The solution enables effective and stable rocket erection during marine hot launches by preventing hydraulic seal damage and reducing the impact of high temperatures on the driving cylinder, ensuring the rocket's safety and successful launch.

Implementation Method 1

a driving cylinder fixedly connected to the deck of the launch vessel and configured to provide a driving force for erecting the rocket

Methodology Applied
Scientific EffectHydraulic pressure: Hydraulic Press

Implementation Method 2

a sliding member adapted to and slidable along the guide cavity and connected to a moving end of the driving cylinder

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 3

a connecting member provided with one end hinged to the erection assembly and the other end hinged to the sliding member

Methodology Applied
Scientific EffectHinge mechanism: Hinge

Data Source

PatentUS11732999B2Erection device and method for marine hot launch of rocket
Publication Date: 2023.08.22 LUDONG UNIVERSITY
  • US11732999B2 patent drawing

AI summary

An erection device and method for the marine hot launch of a rocket are provided. The erection device includes a launch vessel, a launch pad, an erection assembly, a guide member, a driving cylinder, a sliding member, and a connecting member. The sliding member cooperates with the guide member and is driven by the driving cylinder to move linearly. The connecting member has one end hinged to the erection assembly at a certain angle and the other end connected to the sliding member and is configured to move with the sliding member to drive the erection assembly to be erected on the launch pad. The erection device and method can achieve an effective erection of the rocket for marine hot launch with a desired erection effect and high stability.