select adjustable trigger system

38
Central Washington University ScholarWorks@CWU All Undergraduate Projects Undergraduate Student Projects Spring 2017 Select Adjustable Trigger System Seth Rich Central Washington University, [email protected] Follow this and additional works at: hp://digitalcommons.cwu.edu/undergradproj Part of the Mechanical Engineering Commons is Undergraduate Project is brought to you for free and open access by the Undergraduate Student Projects at ScholarWorks@CWU. It has been accepted for inclusion in All Undergraduate Projects by an authorized administrator of ScholarWorks@CWU. For more information, please contact [email protected]. Recommended Citation Rich, Seth, "Select Adjustable Trigger System" (2017). All Undergraduate Projects. 38. hp://digitalcommons.cwu.edu/undergradproj/38

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Page 1: Select Adjustable Trigger System

Central Washington UniversityScholarWorks@CWU

All Undergraduate Projects Undergraduate Student Projects

Spring 2017

Select Adjustable Trigger SystemSeth RichCentral Washington University, [email protected]

Follow this and additional works at: http://digitalcommons.cwu.edu/undergradproj

Part of the Mechanical Engineering Commons

This Undergraduate Project is brought to you for free and open access by the Undergraduate Student Projects at ScholarWorks@CWU. It has beenaccepted for inclusion in All Undergraduate Projects by an authorized administrator of ScholarWorks@CWU. For more information, please [email protected].

Recommended CitationRich, Seth, "Select Adjustable Trigger System" (2017). All Undergraduate Projects. 38.http://digitalcommons.cwu.edu/undergradproj/38

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Select Adjustable Trigger System

Seth Rich

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Table of Contents ......................................................................................................................................................... 0

1. ABSTRACT ............................................................................................................................ 3

2. INTRODUCTION ................................................................................................................... 4

2A: Description ........................................................................................................................... 4

2B: Motivation ............................................................................................................................ 4

2C: Function Statement ............................................................................................................... 4

2D: Requirements ........................................................................................................................ 4

2E: Engineering Merit ................................................................................................................. 5

2F: Scope of Effort ...................................................................................................................... 5

2G: Success Criteria .................................................................................................................... 5

3. DESIGN AND ANALYSIS .................................................................................................... 6

3A: Approach .............................................................................................................................. 6

3B: Design Proposal .................................................................................................................... 6

3C: Benchmark ............................................................................................................................ 7

3D: Performance Predictions ...................................................................................................... 9

4. METHODS AND CONSTRUCTION .................................................................................. 11

4A: Description ......................................................................................................................... 11

4B: Manufacturing Issues.......................................................................................................... 11

5. TESTING METHOD ............................................................................................................ 12

5A: Introduction ........................................................................................................................ 12

5B: Method/Approach ............................................................................................................... 12

5C: Test Procedure .................................................................................................................... 12

6. BUDGET AND SCHEDULE ............................................................................................... 17

6A: Purchasing .......................................................................................................................... 17

6B: Labor................................................................................................................................... 17

6C: Funding ............................................................................................................................... 17

6D: Schedule ............................................................................................................................. 18

7. DISCUSSION ........................................................................................................................ 19

8. CONCLUSION ..................................................................................................................... 20

9. ACKNOLEDGEMENTS ...................................................................................................... 21

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APPENDIX A – Analysis ............................................................................................................. 22

A-1 Hammer Spring .................................................................................................................. 22

A-2 Trigger Spring .................................................................................................................... 23

A-3 Disconnector Spring ........................................................................................................... 24

A-4 Trigger Force Mil-Spec ...................................................................................................... 25

A-5 Trigger Force SSA ............................................................................................................. 27

A-6 Center of Percussion Mil-Spec .......................................................................................... 29

A-7 Center of Percussion SSA .................................................................................................. 30

APPENDIX B – Drawings............................................................................................................ 31

APPENDIX C – Budget................................................................................................................ 34

APPENDIX D – Schedule ............................................................................................................ 35

APPENDIX E – Resume .............................................................................................................. 36

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1. ABSTRACT

There is an increasing need for singular weapon systems to fill multiple roles. A fire control

group system is needed which provides a trigger that is adaptable for different uses on command

by way of the safety selector. The device needs to be non-intrusive to normal function and

operation of the firearm requiring no specialized training in its use. It should provide with a

setting for a general combat use and a secondary setting for a designated marksman role. The

proposed system interfaces with existing trigger groups by using a self-contained drop in module

that counteracts the primary trigger spring while set to the second fire mode. By using a

secondary spring to counteract the primary spring the end result is essentially a lower k value on

trigger movement reducing the trigger pull weight. A survey of commonly available triggers

shows a range of trigger pull values for combat triggers to be 5-7 lbf and marksman triggers to be

3.5-5 lbf. From this data it is concluded that the module should provide a 1.5 lbf reduction in

trigger pull force when engaged in the second fire position. This provides a singular fire control

group system that has the ability to serve in both a general combat and designated marksman

role. The characteristics of the entire system may still be tailored to personal preference by the

selection of the trigger group the device interfaces with.

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2. INTRODUCTION

2A: Description

A fire control group (FCG) system providing two selectable modes with different pull weights

for general and precision use.

2B: Motivation

There is an increasing need for singular weapon systems to fill multiple roles. From the

military side operations have trended towards smaller fire teams relying on force multiplier

strategies rather than employing larger quantities of troops. This has driven demand for in-field

adaptability of the weapon platform, primarily for use in a designated marksman role, while still

being useful in a typical support role. The primary user-weapon interaction point is the trigger

which has remained relatively unchanged in function since the M16A1. The 3rd selector position

or AUTO function has steadily been falling out of favor, particularly with Special Forces groups

who operate most often in small fire teams. A fire control group is needed which provides a user-

weapon interaction with a setting for a general combat use and a secondary setting for a

designated marksman role.

2C: Function Statement

A device is needed which must:

• Provide normal trigger operation

• Have distinctly different user-selectable firing modes

o Firing position 1 for general use

o Firing position 2 for precision use

2D: Requirements

The requirements for the device are:

• Reduce trigger break force by 1-1.5 lbf

• No reduction in hammer energy

• No reduction in hammer lock time

• Minimum cycle life of 10,000 rounds with M855 62gr ammunition without part

breakage

• Fit mil spec AR15 trigger pocket dimensions (excluding Colts with Auto-Sear

block or similar)

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• For use with mil spec small pin (0.154 in) receivers

• Require no permanent modifications to the firearm

• Max cost $75 at production volume (target msrp $295) if self-contained system

• Max cost $20 at production volume (target msrp $80) if add on to existing trigger

2E: Engineering Merit

This project will require the calculation of hammer energy and dynamics, multiple force

calculations, stress calculations for material selection, and confirmation of results through

testing.

2F: Scope of Effort

The scope of this project will be limited to the trigger system only. While accuracy and

usability could be improved in other areas of the weapon platform that is outside the scope of

this exploration.

2G: Success Criteria

A successful device will conform within the defined range of values given in the primary

requirements. It will also be given merit on subjective “feel” on a pass/fail basis. Secondary

requirements are not necessary for a successful solution however are useful options if feasible.

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3. DESIGN AND ANALYSIS

3A: Approach

The primary analysis and testing of this device can be broken into two primary areas. The

first being trigger pull weight and the second being hammer energy. The primary attribute of

total pull force is the break weight which can be defined as the force required on the trigger face

to cause the sear to release the hammer. This problem can be viewed as a statics problem at the

point in motion just before the release. The second point of analysis is hammer energy. This

problem must be solved as a dynamics problem and shall be taken just before the point of impact

with the striker. The torque from the spring and inertia of the hammer are the driving factors in

this calculation.

3B: Design Proposal

The proposed design consists of a standalone module that would interact with existing

fire control groups as shown in Figure 3-1. This unit functions by engaging or disengaging a

spring which provides upward force on the back of the trigger bar. This cancels out part of the

force of the prep spring resulting in a lighter trigger weight as shown in Figure 3-2.

Figure 3-1 Drop In Module

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Figure 3-2 Primary Forces

3C: Benchmark

Two existing components will be used for benchmarking. The first being a standard mil

spec trigger having a single stage operation. It provides a benchmark as a poor yet functional

device. The second component used for benchmarking will be a Geissele Super Semi-Automatic

(SSA®) having a two stage operation. It provides a benchmark as a high end device. Both

devices are widely adopted at opposite ends of the cost spectrum and provide a useful range of

benchmarks.

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Figure 3-3 Mil Spec Trigger Group

Figure 3-4 Geissele Super Semi-Automatic (SSA®) Trigger Group

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Figure 3-5 Trigger Pull Weight Comparison Graph

Manufacturer advertised trigger specifications are referenced above. Max values are confirmed

through our own analysis. The calculated value for a stock milspec trigger was 7.66lb and the

Geissele SSA is 4.53lb. This can be referenced in Appendix A-4 & A-5. This will be used as the

primary benchmark for how the trigger feels.

3D: Performance Predictions

The calculated reduction from stock the module provides as a function of degrees of

rotation is shown in the Table 3-1. Important points of Break and Over-travel are denoted. At

break there should be a 1lb reduction and 1.25lb at over-travel.

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Table 3-1 Module Force Reduction

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4. METHODS AND CONSTRUCTION

4A: Description

The drop in module consists of four proprietary components: Module Housing, Transfer

Bar, Selector Paddle, and Safety Selector. Additional COTS components consist of the

following: Transfer Bar Spring, Selector Paddle Spring, Selector Paddle Pin, and Transfer Bar

Pin. The exploded assembly can be seen in Figure 4-1.

Figure 4-1 Exploded Drop In Module Assembly

Construction of the Module Housing and Selector Paddle are designed around a die cast

or plastic injection molded component. For prototyping purposes functional assemblies may be

made using additive manufacturing. The Transfer Bar is a bent sheet metal component.

4B: Manufacturing Issues

The design of components based on a die cast or injection molded process lends itself

well to the use of additive manufacturing. This drastically simplifies the construction of

prototypes as well as iterative design revisions. The primary concern with this method of

construction will be the ability to maintain acceptable tolerancing of critical features.

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5. TESTING METHOD

5A: Introduction

There are two primary requirements in this test to verify the analysis. The first being a

function test and the second a measurement of trigger break weights. This will be a

straightforward test using commercially available and inexpensive equipment. The desired

requirement for trigger weight reduction is between 1lbf and 1.5lbf.

5B: Method/Approach

Function: After installation the device must be verified to be unfireable in the safe

selector position as well as being capable of firing in both of the fire positions.

Break Weight: Using a commercially available trigger pull gauge a series of samples will

be taken of both the Mil Spec and SSA Triggers. These samples will be overlaid with the

advertised break force graph and calculated theoretical value. This will provide a three

point technical baseline giving a high degree of precision. This will then be performed for

both modes of the new trigger design and will also be compared to the calculated

theoretical values.

5C: Test Procedure

Summary/overview

This test is to evaluate the effectiveness of the drop in module at reducing the trigger pull of a

standard AR15 trigger. Both a Mil Spec (Single Stage) and Geissele SSA (Two Stage) trigger will

be used.

Resources

This test will require the following pieces of equipment

• Lyman Trigger Pull Gauge (Model #7832248)

• AR15 Lower or Strike Industries AR Trigger Hammer Jig

• Mil Spec Trigger Group

• Geissele SSA Trigger Group

• Drop In Trigger Module and Safety Selector

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Procedure

Preface

Process will be repeated with both Mil Spec and SSA trigger groups installed in AR15 lower or

Trigger Jig. Follow standard trigger installation procedures.

Benchmarking

Step 1: Mark trigger at a point 1 inch away from the center of the trigger pin as shown in Figure

5-1.

Figure 5-1

Step 2: Hook trigger pull gauge on trigger at the point that was marked.

Step 3: Pull trigger gauge rearward keeping parallel to bore axis until the trigger breaks as shown

in Figure 5-2.

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Figure 5-2

Step 4: Record reading on gauge.

Step 5: Repeat process for a total of 10 times. Calculate an average value.

Safe Position/Module Installation

Step 1: With Safety Selector removed install Drop In Module by setting it into the cavity of the

trigger pocket that is behind the Safety Selector as shown in Figure 5-3. The Transfer Bar should

be hooked under the rear portion of the Trigger Bar as shown in Figure 5-4.

Figure 5-3 Figure 5-4

Step 2: Install Drop In Module specific Safety Selector following standard installation procedure.

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Step 3: Set Safety Selector to the “SAFE” position and confirm the firearm won’t fire. Result is

pass/fail.

Fire Position 1

Step 1: Set Safety Selector to “FIRE” position and repeat steps 2 through 5 from Benchmarking.

Fire Position 2

Step 1: Set Safety Selector to “FIRE 2” position and repeat steps 2 through 5 from

Benchmarking.

Discussion

Results should be compared to manufacturer advertised specifications and calculated values.

Non-scientific notes may be recorded on how the trigger “feels” on any pull as a point of

reference if it is unusual or substantially different in function.

The results from the initial test show a variance from the calculated values due to a high friction

coefficient between sliding components. The initial calculations were assumed frictionless.

Follow-up includes experimentally determined friction coefficient to adjust calculations.

Results:

The average reduction in trigger pull was about 0.5lb, half of the calculated value. This is

mostly due to unaccounted for friction. The moved average force lines are shown in

Figure 5-5.

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Figure 5-5 Trigger Reduction

The MilSpec trigger saw a slightly higher reduction in trigger pull weight than the SSA.

The complete test results for each trigger can be seen in Table 5-1 and 5-2.

Table 5-1 Mil Spec Table 5-2 SSA

Test # MilSpec Stock lbf MilSpec Module lbf

1 7.6 7

2 7.8 6.9

3 7.4 7.2

4 7.5 7

5 7.6 7.1

6 7.4 7.2

7 7.5 6.9

8 7.6 7.1

9 7.8 7.2

10 7.6 7.3 Reduction

Average 7.58 7.09 0.49

Test # SSA Stock lbf SSA Module lbf

1 4.6 4.2

2 4.4 3.9

3 4.5 4.1

4 4.4 4

5 4.3 4.1

6 4.4 3.8

7 4.5 3.9

8 4.5 4.1

9 4.3 4

10 4.4 4.1 Reduction

Average 4.43 4.02 0.41

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6. BUDGET AND SCHEDULE

6A: Purchasing

Purchased components can be separated into three main categories. Raw materials will be

anything requiring processing to become a usable part in the assembly; this will be denoted with

blue. COTS are any standardly stocked component which may be purchased for direct use in the

assembly; this will be denoted with grey. Jigs and Tooling will be any additional materials or

components which must be purchased to aid in manufacture/assembly but will not be a part of

the final product; this category being denoted with green.

6B: Labor

Labor may be broken into two categories; however, all labor will be denoted in yellow. Internal

labor will primarily consist of my own time involved in the project but may include faculty

assistance as well. The cost of this labor is reference only and is not included in the actual

expenditure for the project. External labor will be for any outside assistance which must be hired.

This could include outside machinists or finishing processes. This is a real cost and will be

included in the actual expenditure for the project.

6C: Funding

This project will be completely self-funded. The max allowable personal expenditure will be set

at $500 including testing materials which will drive the scope of the development. Sources for

donated materials or services will be evaluated throughout the project to alleviate associated

costs where possible.

TYPE NAME PART # DESCRIPTION SOURCE UNIT PRICE QUANTITY TOTAL COST

RAW MATERIALS A2 TOOL STEEL 9019K76 1"X 6" X 3/4" MCMASTERCARR $31.07 1 $31.07

SUB TOTAL $31.07

COTS TRIGGER SPRING 078-101-136WB MIL SPEC TRIGGER SPRING BROWNELLS $1.99 1 $3.00

SECONDARY TRIGGER SPRING TBD NA TBD $15.00 MAX 1 $15.00

DISCONNECTOR SPRING 078-101-120WB MIL SPEC DISCONNECTOR SPRING BROWNELLS $1.29 1 $1.29

HAMMER SPRING F1003069 MIL SPEC HAMMER SPRING BROWNELLS $1.79 1 $1.79

HAMMER SPRING ALTERNATE 30093 PLUS POWER HAMMER SPRING BROWNELLS $4.99 1 $4.99

TRIGGER PIN 231-000-103WB MIL SPEC TRGGER PIN (.154) BROWNELLS $2.43 2 $4.86

SUB TOTAL $30.93

JIGS AND TOOLING STRIKE INDUSTRIES TRIGGER JIG SIARTHJ AR15 TRIGGER ASSEMBLY JIG BROWNELLS $36.95 1 $36.95

SUB TOTAL $36.95

TOTAL $98.95

TYPE NAME DESCRIPTION SOURCE COST/HR HOURS TOTAL COST

LABOR INTERNAL ENGINEERING, DEVELOPMENT, MANUFACTURING $50.00 100 $5,000.00

EXTERNAL FINISHING AND EXTERNAL PROCESSING $100.00 1.5 $150.00

SUB TOTAL $5,150.00

PROJECT TOTAL $5,186.95

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6D: Schedule

The proposed high level schedule is as follows. See Appendix E for in depth schedule of each

weeks tasks.

Task # Task 1/4/2017 1/9/2017 1/16/2017 1/23/2017 1/23/2017 1/30/2017 2/6/2017 2/13/2017 2/20/2017 2/27/2017 3/6/2017 3/13/2017 Task Total Project Total Status

1 Design Module x x x x x 15 11 26

2 Source Material 0.5 5.5 6

3 Program Machining 2 4 6

4 Machine Components 3 7 5 15

5 Test Assemble 2 2

6 Revisions 0

55

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7. DISCUSSION

The Fire Control Group (FCG) operates on a rather simplistic principle. The hammer is

mechanically locked in a rearward position until user input releases it. This is not much different

than the mechanism used on flintlock firearms. Where it differs is that rather than needing to be

manually recocked it uses a disconnector to catch the hammer on the way back from cycling the

action. While that feature in its self is not technologically complicated, it does create more

complexity to the system. With this added complexity, more components must occupy a

similarly sized space.

This project aims to add more functionality to that existing design. While again these

changes aren’t technologically complicated they do place in increase in demand for components

to occupy the same space. Multi-break weight functionality can be designed rather simply using

cams, different springs and sear geometry. The challenge in this project is packaging that

functionality in the limited space provided by an existing receiver. The vast majority of

challenges in this endeavor will be in creating a smart design that is both space efficient as well

as easy to assemble.

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8. CONCLUSION

A successful conclusion to this project will result in a device which provides the two

distinct modes of operation outlined in the requirements. Success can be assured by

following a few simple guidelines. Successful benchmarking is critical to good design work.

Benchmarking should be calculated and verified through testing to ensure the design process

is accurate before dedicating too much effort into manufacturing a flawed device. Iterative

design should be an ongoing process through calculation and testing until confidence is

achieved to move forward with production. Once in production project management will be

crucial to ensure materials and components are received or completed in a timely manner

with room for unforeseen complications. Lastly judicious documentation will lead to a

successful and repeatable project.

The final iteration of the project met the design goals. Initially friction was ignored as an

experimentally determined coefficient could be easily added in later to adjust the design.

After initial testing a change in spring rates was used to compensate for unaccounted for

friction to bring the project into the values specified in the requiring for trigger force

reduction.

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9. ACKNOLEDGEMENTS

This project could not be completed without the support of the faculty and other advisers

to this project. Any industry contacts providing expertise, donated materials, or other forms

of support are greatly appreciated. While this is a mostly individual project the collaboration

between other students is an important part of the development process.

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APPENDIX A – Analysis

A-1 Hammer Spring

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A-2 Trigger Spring

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A-3 Disconnector Spring

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A-4 Trigger Force Mil-Spec

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A-5 Trigger Force SSA

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A-6 Center of Percussion Mil-Spec

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A-7 Center of Percussion SSA

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APPENDIX B – Drawings

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APPENDIX C – Budget

TYPE

NA

ME

PA

RT #

DESC

RIP

TION

SOU

RC

EU

NIT P

RIC

EQ

UA

NTITY

TOTA

L CO

ST

RA

W M

ATER

IALS

A2 TO

OL STEEL

9019K76

1"X 6" X

3/4"M

CM

ASTER

CA

RR

$31.071

$31.07

SUB

TOTA

L$31.07

CO

TSTR

IGG

ER SP

RIN

G078-101-136W

BM

IL SPEC

TRIG

GER

SPR

ING

BR

OW

NELLS

$1.991

$3.00

SECO

ND

AR

Y TRIG

GER

SPR

ING

TBD

NA

TBD

$15.00 MA

X1

$15.00

DISC

ON

NEC

TOR

SPR

ING

078-101-120WB

MIL SP

EC D

ISCO

NN

ECTO

R SP

RIN

GB

RO

WN

ELLS$1.29

1$1.29

HA

MM

ER SP

RIN

GF1003069

MIL SP

EC H

AM

MER

SPR

ING

BR

OW

NELLS

$1.791

$1.79

HA

MM

ER SP

RIN

G A

LTERN

ATE

30093P

LUS P

OW

ER H

AM

MER

SPR

ING

BR

OW

NELLS

$4.991

$4.99

TRIG

GER

PIN

231-000-103WB

MIL SP

EC TR

GG

ER P

IN (.154)

BR

OW

NELLS

$2.432

$4.86

SUB

TOTA

L$30.93

JIGS A

ND

TOO

LING

STRIK

E IND

USTR

IES TRIG

GER

JIGSIA

RTH

JA

R15 TR

IGG

ER A

SSEMB

LY JIGB

RO

WN

ELLS$36.95

1$36.95

SUB

TOTA

L$36.95

TOTA

L$98.95

TYPE

NA

ME

DESC

RIP

TION

SOU

RC

EC

OST/H

RH

OU

RS

TOTA

L CO

ST

LAB

OR

INTER

NA

LEN

GIN

EERIN

G, D

EVELO

PM

ENT, M

AN

UFA

CTU

RIN

G$50.00

100$5,000.00

EXTER

NA

LFIN

ISHIN

G A

ND

EXTER

NA

L PR

OC

ESSING

$100.001.5

$150.00

SUB

TOTA

L$5,150.00

PR

OJEC

T TOTA

L$5,186.95

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APPENDIX D – Schedule

Sub

Task #Su

b Task

2/27/20172/28/2017

3/1/20173/2/2017

3/3/20173/4/2017

3/5/2017Su

b Task To

talW

ee

k Total

Status

4EM

achin

e Flip

pe

r2

13

4FM

ake Tran

sfer B

ar2

25

5AFirst A

ssem

bly

22

27

Sub

Task #Su

b Task

2/20/20172/21/2017

2/22/20172/23/2017

2/24/20172/25/2017

2/26/2017Su

b Task To

talW

ee

k Total

Status

4BSe

tup

for H

ou

sing M

achin

e2

2

4CM

achin

e H

ou

sing

33

4DSe

tup

for M

achin

e Flip

pe

r2

2

7

Sub

Task #Su

b Task

2/13/20172/14/2017

2/15/20172/16/2017

2/17/20172/18/2017

2/19/2017Su

b Task To

talW

ee

k Total

Status

3AH

ou

sing C

AM

Pro

gram2

13

3BFlip

pe

r CA

M P

rogram

11

4

4AM

od

ify Sele

ctor

33

37

Sub

Task #Su

b Task

2/6/20172/7/2017

2/8/20172/9/2017

2/10/20172/11/2017

2/12/2017Su

b Task To

talW

ee

k Total

Status

1AD

ete

rmin

e Sp

ring C

haracte

ristics2

13

1BFin

alize H

ou

sing fo

r Sprin

gs2

24

1CEn

gine

erin

g Draw

ings

22

411

2BSo

urce

Alu

min

um

0.50.5

2CSo

urce

Sprin

gs3

3

2DSo

urce

CO

TS2

25.5

3AH

ou

sing C

AM

Pro

gram2

22

18.5

Sub

Task #Su

b Task

1/30/20171/31/2017

2/1/20172/2/2017

2/3/20172/4/2017

2/5/2017Su

b Task To

talW

ee

k Total

Status

1AD

esign

Basic H

ou

sing Sh

ape

21

3

1BD

esign

Basic In

tern

al Fun

ction

12

23

8

1CD

ete

rmin

e Sp

ring C

haracte

ristics2

24

15

2ASo

urce

Stee

l She

et

0.50.5

0.5

15.5

Task #Task

1/4/20171/9/2017

1/16/20171/23/2017

1/23/20171/30/2017

2/6/20172/13/2017

2/20/20172/27/2017

3/6/20173/13/2017

Task Total

Pro

ject To

talStatu

s

1D

esign

Mo

du

lex

xx

xx

1511

26

2So

urce

Mate

rial0.5

5.56

3P

rogram

Mach

inin

g2

46

4M

achin

e C

om

po

ne

nts

37

515

5Te

st Asse

mb

le2

2

6R

evisio

ns

0

55

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APPENDIX E – Resume