Cocking Hammer Launcher Airtight Sealing for Foam Dart Accuracy

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Solution Overview

Problem

Existing toy projectile launchers, particularly those resembling pistols with a cocking hammer, lack sufficient launching force and accuracy for high-performance foam darts.

Innovation Solution

Incorporation of sealing mechanisms to form airtight seals between the air piston mechanism and the launch barrel, along with a simplified construction featuring a cocking hammer mechanism that enhances air pressure launch force and accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If conventional dart guns are designed with metal barrels and small clearance between barrel and dart, then launching velocity and accuracy are improved, but device complexity and manufacturing difficulty increase

Engineering Contradiction:
Improvelaunching velocityVSAvoidbarrel and dart dimensional precision
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The projectile is segmented into two distinct parts: a foam body for safety and a separate cap for aerodynamic performance. This segmentation allows each component to be optimized independently - the foam body can be larger and softer while the cap provides the streamlined shape needed for high velocity, resolving the contradiction between safety and performance without requiring extremely tight tolerances throughout the entire projectile.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The launcher uses a dynamic compression mechanism where the spring-loaded compression member dynamically adjusts to compress the foam body into the cap. This dynamic compression process allows for consistent projectile formation with proper sealing without requiring static precision in the barrel-dart clearance, reducing manufacturing complexity while maintaining launching velocity.

Inventive Principle:
Principle #15Dynamics

2Force

If airtight seals are improved between air piston and launch barrel, then launching force and accuracy are improved, but device complexity increases

Engineering Contradiction:
Improveair pressure launch forceVSAvoidsealing mechanism complexity
Core Design Contradiction:
ForceVSDevice complexity

Solution Approach 1:

The sealing function is merged with the compression mechanism. The compression member that compresses the foam body into the cap also serves as the sealing element against the launch barrel. This merging of functions eliminates the need for separate, complex sealing components while achieving effective airtight sealing for high launching force.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The compression mechanism performs dual functions: it compresses the projectile components together and simultaneously creates the seal against the barrel. The spring-loaded design automatically maintains sealing pressure during the launch cycle without requiring additional sealing components or complex adjustment mechanisms, achieving effective sealing with simpler device architecture.

Inventive Principle:
Principle #25Self-service

3Object-affected harmful factors

If foam darts are used instead of traditional dart caps, then safety is improved, but launching speed and distance are reduced

Engineering Contradiction:
Improveprojectile safetyVSAvoidprojectile launching speed
Core Design Contradiction:
Object-affected harmful factorsVSSpeed

Solution Approach 1:

The projectile is divided into a foam body and a separate cap, allowing the foam to provide safety while the cap provides aerodynamic efficiency. The cap acts as a streamlined shell that reduces air resistance, enabling the foam projectile to achieve high launching speed and distance despite its softer, safer construction.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The dynamic compression process forcefully embeds the foam body into the cap, creating a tightly integrated projectile structure. This dynamic assembly ensures proper sealing and aerodynamic alignment, allowing the safe foam construction to achieve launching performance comparable to traditional hard darts through proper mechanical integration rather than material substitution alone.

Inventive Principle:
Principle #15Dynamics

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 achieves high velocity and accurate projectile launching, improving the performance of toy launchers by enhancing the air pressure launch force and ensuring precise sealing mechanisms.

Implementation Method 1

a compression spring that is compressed when the cocking hammer mechanism is actuated

Methodology Applied
Scientific EffectSpring: Spring

Implementation Method 2

a lever arm that is pivotally attached to the cocking hammer mechanism and that is engaged with the compression spring

Methodology Applied
Scientific EffectMechanical Advantage: Mechanical Advantage

Implementation Method 3

sealing mechanisms to form airtight seals between the air piston mechanism and the launch barrel... enhancing the air pressure launch force

Methodology Applied
Scientific EffectPressure Increase: Pressure Increase

Data Source

PatentUS12553685B2High performance launcher with cocking hammer
Publication Date: 2026.02.17 EASEBON SERVICES
  • US12553685B2 patent drawing
  • US12553685B2 patent drawing
  • US12553685B2 patent drawing

AI summary

A toy projectile launcher including a housing, a launch barrel, an air piston assembly, a trigger, a trigger lever having a distal end portion connected to the launch barrel, a storage cylinder rotatably mounted within the housing and comprising a plurality of projectile holders, wherein each projectile holder is configured to contain a projectile, and a spring that biases the launch barrel away from the storage cylinder. When the trigger is actuated, the trigger lever pulls the launch barrel into engagement with one of the projectile holders of the storage cylinder to form an airtight seal between a rear portion of the launch barrel and the one of the projectile holders.