SOW H2WM06 v2_17Feb2022.pdf

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Attached to
Coordinate Measuring Machine system Federal contract opportunity
Solicitation number
FA8126-22-R-0004
Issued by
Department of the Air Force Materiel Command Air Force Sustainment Center

About this file

This Statement of Work details requirements for furnishing, shipping, installing, calibrating, and testing a new Coordinate Measuring Machine (CMM) system to replace an existing Zeiss Prismo 9-12-7 CMM at Tinker Air Force Base in Oklahoma. The CMM must have a minimum 900mm x 1200mm x 650mm measurement envelope, be inch/metric switchable, and include a fixed probe head, probe styli kit, reference sphere, air filter/regulator, and vibration dampening system. The system must also include a granite inspection table capable of supporting up to 1300kg, integrated rotary table capable of supporting up to 600kg, AC or DC servo drive motors, and linear measurement scales with 0.08um resolution. Additional requirements include manuals, electrical specifications, nameplate information, and on-site installation, calibration, verification and testing by the vendor. The contract will be awarded by the Air Force Sustainment Center and includes a one-year warranty on hardware, software, and operating system.

The related federal contract opportunity is solicitation number FA8126-22-R-0004 for a CMM system to meet the requirements in the Statement of Work, including shipping, installation, and certification.

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CSS_FA812622R0004_15Mar2022.pdf PDF
Technical Proposal Evaluation v2.pdf PDF

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Text version

Statement of Work

(SOW)

QVC Coordinate Measuring Machine (CMM)

Zeiss Prismo 9-12-7 Replacement

1.0. Scope – This purchase description details the requirements for furnishing, shipping, installing, assembling, and verification/calibration of a commercially available Coordinate

Measuring Machine (CMM) to replace the Zeiss Prismo 9-12-7 CMM in the B2210 QVC

Lab. The CMM shall be utilized to verify the dimensional integrity of weapon systems and component parts that are repaired and/or manufactured as well as inspection of the necessary tooling and fixturing required to produce the weapon systems and component parts.

Contractor shall provide all labor, tools, equipment, materials, parts, personal protective equipment (PPE), transportation and any other incidentals to travel to Tinker AFB OK.

Offloading and placement of CMM will be provided by Tinker AFB personnel at the guidance of contractor technical personnel.

2.0. Requirements and Specifications

2.1. Design – The CMM shall be one of the manufacturer’s current production models;

new and unused. The CMM related components and accessories shall meet or exceed the minimum requirements for design, construction, functional capability, size and performance as specified herein. All parts subject to wear, breakage or distortion shall be readily accessible for adjustment, replacement and repair.

2.2. Measuring System – Either the U. S. Customary System of Units (US) or the

International System of Units (SI) may be used in the design and manufacture of the

CMM. The CMM shall be inch/metric switchable with automatic conversion by the system between the two systems of measurement.

2.3. Construction – All parts and materials used in the construction of the CMM shall be new. The quality of construction shall be provided to meet the strength, rigidity and wear resistance characteristics necessary to meet the standards for accuracy, performance and safety specified herein. All parts and mechanisms requiring adjustment, replacement or servicing shall be readily accessible. The CMM shall be complete so that when installed and connected to the proper utilities it shall be ready for use. The construction of the CMM shall be free from any defects; primarily, but not only, those which would affect the operation of the CMM.

2.4. Maintenance – Test procedures and instructions shall be provided for identification, location and repair of mechanical, electrical and electronic failures. Parts lists/drawings, circuit diagrams and electrical/electronic schematic shall be provided for both preventative and remedial maintenance.

2.5. Lubrication – All parts of the CMM requiring continuous lubrication shall be automatically lubricated by a system that will ensure adequate lubrication of parts.

Parts or mechanisms requiring periodic lubrication shall be provided with adequate means for grease or oil lubrication. Systems using recirculated oil shall be equipped with a replaceable or washable filter element. Each oil reservoir shall have an oil level gage. Automatic processes of lubrication shall have a warning device to indicate when lube oil is low or system failure.

2.6. Bearings – All moving components of the CMM requiring bearings shall be equipped with anti-friction, free-floating air or mechanical bearings. All mechanical bearings should be precision ground, honed and/or lapped and be constructed to withstand the applicable axial and radial loads. All bearings will be adequately marked for replacement purposes. Each measurement axis of the CMM will be supported by air bearings, with means for adjustment provided to facilitate alignment and calibration. All sliding surfaces of the CMM that are subject to wear shall have provisions for lubrication and have replaceable bearing surfaces. Air bearings will be of open orifice type to prevent clogging due to the collection of extremely fine particle matter which may be allowed to pass through the filtering system.

2.7. Bearing Surfaces – All bearing surfaces shall be designed and constructed to eliminate inaccuracies caused by deflections of machine components and to prevent applicable load factors from adding to the total error.

2.8. Plates – All instruction plates and identification plates attached to the CMM shall be of a corrosion resistant material. Wording shall be in the English language using plain bold-face letters and shall be made legible and permanent on a contrasting non-glare background.

2.9. Safety and Health – Covers, guards, bellows, or other safety devices will be provided for all parts of the CMM that present potential safety hazards. Safety devices shall not interfere with the operation of the CMM. The safety devices will prevent unintentional contact with the guarded part(s) and will be removable to facilitate inspection, maintenance and replacement of the part(s). All parts, components, mechanisms and assemblies furnished with the CMM shall comply with applicable requirements of OSHA. Additional safety and health requirements will be as specified herein.

2.10. Mercury Restriction – The CMM must meet or exceed RoHS 2017 requirements for mercury contamination.

2.11. Asbestos Restriction – Asbestos and materials containing asbestos will not be used on or in the CMM and are strictly forbidden.

2.12. Lead Restriction – The CMM must meet or exceed RoHS 2017 requirements for lead contamination.

2.13. Ozone Depleting Substances - All class 1 ozone depleting substances (ODSs) are strictly forbidden.

2.14. Environmental Protection – Under the operating, service, transportation and storage conditions described herein, the CMM will not emit materials or radiation hazardous to the operator or ecological system as prohibited by Federal, State or Local statutes in effect at the time of installation.

2.15. Affirmative Procurement Determination - Green/Affirmative Procurement has been determined not to be applicable to this procurement.

3.0. Components

3.1. CMM – The CMM shall consist of a moving bridge system including a fixed granite table as the base of the machine. The measuring machine shall be of sufficient size and stability to provide full measurement capabilities within a minimum 900mm (X) x minimum 1200mm (Y) x minimum 650mm (Z) measurement envelope with all necessary clearances needed for adequate measurement approach. CMM overall height cannot exceed 11’ (3,353mm).

3.2. Inspection Table – The fixed inspection table of the CMM shall be made from granite of sufficient size to accomodate all capacities and the working inspection volume of the CMM as specified herein. The inspection table must be able to support parts weighing up to 1300kg (2,866 lbf) without degrading the measurement performance accuracy of the CMM or table flatness. The inspection table will have the manufacturer’s standard number of threaded inserts with center-to-center distances and diameter common for work-holding devices or fixturing.

3.3. Integrated Rotary Table – A rotary table will be integrated into the granite of the inspection table, with the face of the rotary table beneath the surface of the inspection table to allow for unobstructed use of a fixturing plate attached using the aforementioned threaded inserts. The rotary table must be able to support workpieces and fixturing weighing at least 600kg (1,333 lbf) without a degradation in performance. The face plate of he rotary table must be at least 400mm in diameter and include M8 threaded holes to facilitate the mounting of jaw chucks for part stability during measurement. The rotary table must not have an axial runout greater than 0.1µm and a radial runout greater than 0.2µm.

3.4. Bridge Structure – The moving bridge structure supporting the probe system will conform to standard industry practices and will be supported by air bearings for stability. The bridge structure shall be designed and constructed to achieve maximum stability while at the same time minimizing any induced error resulting from temperature changes and particulate infiltration. The bridge structure will be made of the same material to minimize thermal expansion that would adversely affect the accuracy of the CMM.

3.5. Drive System – The bridge structure, carriage crosslide and ram shall be driven by variable speed, high torque AC or DC servo motors. Linear scales shall be integrated with the servo drive systems to form a closed loop feedback system with both computer directed and manually directed by means of remote. The motion system shall have means for backlash compensation and provisions for halting movement of the entire bridge structure should the air supply be interrupted. The servo drive/motion control system shall monitor manual CMM operations, respond to instruction entered into the remote and execute the inspection routines according to inspection programs entered into the computer control of the CMM. The drive system shall be coordinated by the computer control of point-to point, two and three dimensional contouring motion(s). The motion control drive system shall have three-axis vectoring capabilities so as to allow approach and probing at any vector normal to a feature.

3.6. Linear Measurement Devices (scales) – Linear measurement scales shall be constructed of wear resistant materials and shielded to prevent damage and contamination. The scales shall have a uniform coefficient of thermal expansion in relation to the mounting structure and have a resolution of 0.08µm or better.

3.7. Articulating Probe System – An articulating CMM head is not required for this

CMM. However, the CMM must be capable of switching between a fixed head probe system and an articulating head probe system from the factory, in case future workload dictates the purchase of this additional head. The CMM must allow this probe head change by the end user (QVC) as workload demands.

3.8. Fixed Head Probe System – The CMM will be provided with a fixed, active scanning probe head. This probe head must be capable of handling assembled probes weighing at least 650g and measuring at least 800mm long. The fixed probe system must be manufactured and qualified in accordance with ISO-10360-2, having an

MPE(E0)≤0.9+L/350µm and an MPE(E150)≤0.9+L/350µm at the ambient lab temperature of 20°C.

3.9. Probe Styli Kit – The contractor will furnish a probe styli kit designed specifically for the probe combinations as described in 3.7 and 3.8, consisting of the standard minimum items or components commonly used in CMM measurement.

3.10. Reference Sphere – A reference sphere will be provided for the qualification of each of the sensors included with the CMM.

3.11. CMM Control Computer – The following minimum hardware and software capabilities/functions will be required (items may be exact or equivalent to):

3.11.1. Hardware

3.11.1.1. High End Workstation Computer System

3.11.1.1.1. Minimum one (1) Workstation-grade quad-core CPU or better

3.11.1.1.2. 64-bit Windows operating system

3.11.1.1.3. Minimum one (1) Discrete Workstation-grade GPU

with 4GB VRAM or better

3.11.1.1.4. Minimum 64GB RAM

3.11.1.1.5. DVD+RW compatible internal optical drive

3.11.1.1.6. Sufficient RJ45 Gigabit LAN Ethernet ports for

machine-computer communication and connection of the computer to our lab printer network.

3.11.1.2. (2) 27” 16:9 LCD Monitors with cables

3.11.1.3. US QWERTY Keyboard, wired

3.11.1.4. Mouse, wired

3.11.1.5. CMM Control Joystick Box, wired

3.11.2. Software

3.11.2.1. Windows-based Operating System

3.11.2.2. Geometric Dimensioning and Tolerancing per ASME

Y14.5M

3.11.2.3. Selection of geometric alogorithms per ASME Y14.5M

3.11.2.4. Probe calibration routines

3.11.2.5. Part programming routines

3.11.2.6. Measurement and analysis of complex curves and surfaces

3.11.2.7. Measurement and analysis of blade profiles

3.11.2.8. Measurement and analysis of involute gear profiles

3.11.2.9. STEP import/export compatibility

3.11.2.10. Graphical presentation of results in part drawing format

3.11.2.11. Printing capabilities to network printer

4.0. Peripheral Devices

4.1. Probe Rack and Storage Sockets – A probe rack and stylus system holders shall be provided to house all items not in use. This rack should be able to accommodate probe head(s), holders for nine (9) articulating head adapter plates, and any other items needed for storage of probe head/stylus systems.

5.0. Additional Equipment

5.1. Air Filter / Regulator – The CMM will utilize the current 100 psi shop air supply in the existing area. The contractor shall supply a means to remove contaminants and regulate the pressurized air entering into the CMM.

5.2. Vibration Dampening System – The contractor shall supply some means to reduce measurement error from vibrations not associated with the CMM. Anti-vibration isolation pads are acceptable.

5.3. Machine Manuals – Two (2) complete hard copies of technical data (or a single electronic file of all manuals) will be submitted upon contract approval prior to delivery to ensure proper shop footprint specifications and familiarity with the CMM before delivery. This technical data will include items such as operating manuals, maintenance manuals, parts catalogs, parts lists, wiring schematics, lubrication charts, machine accuracy and alignment test results and shall be written in the

English language.

6.0. Environmental Tolerance – The CMM will be located in a controlled environment wherein the temperature will be maintained at 68 degrees +/- 1 degree Fahrenheit over a 24 hour period with the humidity controlled to 30 – 50% non-condensing. The contractor shall state before contract approval whether the conditions will adversely affect the operation of the

CMM.

7.0. Electrical Equipment – The electrical system of the CMM and all electrical components thereof, will conform to the requirements of NEC and operate on 115 VAC +/- 10% utilizing standard NEMA 5-15 Duplex Receptacles. The contractor will provide full documentation of the electrical requirements and any power conditioning requirements before contract approval. All electrical equipment design and documentation is subject to final approval by the Government.

8.0. Nameplate – A corrosion resistant nameplate identifying the CMM shall be securely attached to the granite inspection table. The nameplate should contain the information listed below. The captions may be shortened or abbreviated, provided the entry for each is clear to its identity:

Manufacturer’s Name

Manufacturer’s Model Designation

Manufacturer’s Serial Number

Power Input (volts, total full load amps, phase, frequency)

Date of Manufacture

9.0. On-Site Installation, Calibration, Verification and Testing - The vendor shall provide on-site installation, calibration, verification, and testing demonstrating that the instrument is in working order and meets the requirements of this SOW. The installation, calibration, verification, and testing shall be accomplished during normal operating hours of Monday –

Friday 6:00 am – 3:00 pm.

10.0. Contract Monitor Provisions

10.1. Responsibility for Inspection – Unless otherwise directed by the contracting officer, the contractor is responsible for performance of all inspection requirements herein. Except as otherwise directed by the contracting officer, the contractor may use their own or any other facilities suitable for the performance of inspection requirements specified herein, unless overruled by the Government. The Government reserves the right to perform any of the inspections set forth in the specification when such inspections are deemed necessary to ensure supplies and services conform to prescribed requirements.

10.2. Quality Conformance Inspection – Quality conformance inspection shall be applied to each item prior to being offered for acceptance under the contract.

Preliminary quality conformance inspection prior to shipment will be conducted at the facility chosen by the contractor. Final quality conformance inspection shall be conducted at the Government installation site, after installation, standard checkouts and calibration have been completed, and will consist of the examination in 10.3. and the tests in 10.4. under supervision of Government representatives appointed by the contract administrator. The calibration data obtained in the preliminary and the final quality conformance checks shall be furnished with the machine in a standard certificate format. Failure of any item to pass any examination or test shall be cause for rejection. The CMM and all equipment associated with this purchase will remain the property of the contractor until all items of this quality conformance inspection have been passed and accepted by all government representatives.

10.3. Examination – The CMM and all associated equipment shall be examined for compliance with design, construction, materials, components, electrical equipment and workmanship requirements specified herein.

10.4. Tests – The contractor shall demonstrate that the CMM performs as required herein using accepted industry standards for testing and calibration, provided these tests demonstrate all performance requirements stated in this purchase description.

Failure of any test to demonstrate that the CMM and related equipment meet the minimum requirements as specified herein, will be cause for rejection.

11.0. Warranty – All components of this purchase will come with a 1 year warranty over hardware, software and computer operating system. This warranty will not be required to include normal wear on styli or collision damage of probe system. The warranty period will begin once installation, inspection, all testing and government acceptance has been approved by the contract monitor and representatives of the government.

12.0. Software Support – Vendor will supply all software updates and/or patches free of charge for 1 year after acceptance. This software support will include 1 year of telephone support associated with all functions of the operation of the CMM.

13.0. Shipping – The contractor shall include all costs associated with shipping or transport of all items associated with this purchase description to the final destination of Tinker AFB, OK. Upon delivery, Tinker AFB personnel will offload the equipment to a staging area until representatives of the contractor can be on site for final installation. Any special accommodations will be noted by the vendor prior to receipt of equipment. Staging of equipment will not exceed 14 calendar days upon receipt of equipment, unless negotiated and agreed upon by the vendor and contracting officer if changes from the original contract are deemed necessary.

File details come from the government source that posted it. Updated .