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TURBINE SERIES PRIMER PUMP KITS

View Parts

  • RKP1912

    DescriptionValue
    PRODUCT TYPE Filter Replacement Parts/kits
    DESCRIPTION Primer Pump Replacement Kit
    USE WITH MODEL 900 & 1000 Turbine Series
    ADDITIONAL DETAIL 12 vdc/Includes Bracket and Bolts
    TRADE/BRAND NAME Racor
    Configurator NO
    CAD Drawing Available NO
  • RKP1924

    DescriptionValue
    PRODUCT TYPE Filter Replacement Parts/kits
    DESCRIPTION Primer Pump Replacement Kit
    USE WITH MODEL 900 & 1000 Turbine Series
    ADDITIONAL DETAIL 24 vdc/Includes Bracket and Bolts
    TRADE/BRAND NAME Racor
    Configurator NO
    CAD Drawing Available NO
 
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SOLENOID DRAIN VALVES

Parker offers Lightning-Safe® and non-lightning safe drain valves for fluids and containers for the aerospace market. Our stainless steel, titanium, aluminum or plastic drain valves are designed with centerline poppets, either manually or electrically actuated. They can be designed with self-closing, locked-open or locked-closed poppets.

 
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SINGLE-POINT NOZZLES

Using our patented Macrospray® macrolaminate technology, the Gas Turbine Fuel Systems Division designs and manufactures single-point nozzles. The nozzles, which produce smaller droplets, repeatable droplet dispersion patterns, and more uniform spray patterns, are designed to replace conventional pressure-swirl design or impact-type nozzles, giving you better performance at lower pressures.

 

Our single-point nozzles are designed for longer life, with larger flow passages to reduce plugging and an integral filter for reduced maintenance. Smaller than a conventional nozzle, it makes replacement easier in hard-to-reach applications.

 

Applications

  • Turbine inlet air cooling (TIAC)
  • Gas conditioning
  • Gas cooling
  • Humidification
  • Moisturizing
  • Odor control

 

Systems and Accessories

  • Manifolds – standard and custom
  • Nozzle and manifold kitting
  • Filtration
  • Mounting bosses

Technical Highlights

  • Maximum operating pressure at ambient temperature: 3000 psi

 

Single-point nozzle capacity, U.S. GPH (water)

Capacity

100 psi

200 psi

300 psi

400 psi

500 psi

750 psi

1000 psi

0.3

0.30

0.42

0.52

0.60

0.67

0.82

0.95

0.5

0.50

0.71

0.87

1.00

1.12

1.37

1.58

0.6

0.60

0.85

1.04

1.20

1.34

1.64

1.90

0.7

0.70

0.99

1.21

1.40

1.57

1.92

2.21

0.8

0.80

1.13

1.39

1.60

1.79

2.19

2.53

1.0

1.0

1.4

1.7

2.0

2.2

2.7

3.2

1.5

1.5

2.1

2.6

3.0

3.4

4.1

4.7

2.0

2.0

2.8

3.5

4.0

4.5

5.4

6.3

2.5

2.5

3.5

4.3

5.0

5.6

6.9

7.9

3.0

3.0

4.2

5.2

6.0

6.7

8.2

9.5

3.5

3.5

5.0

6.1

7.0

7.8

9.6

11.1

Additional capacities available--please contact us.

 
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SPIDER NOZZLES

Using our patented Macrospray® macrolaminate technology, the Gas Turbine Fuel Systems Division designs and manufactures multi-injection point spider nozzles that produce an extremely fine spray with smaller droplets than conventional pressure-swirl design or impact-type nozzles.

 

Utilizing two, four, six, eight, or twelve spray points per assembly, spider nozzles are able to provide a much larger coverage area than conventional pressure-swirl or impact nozzles—ideal for applications where higher volumes of liquid with fine drop sizes are required, such as gas conditioning.

 

Chemically machined geometries provide smooth, efficient flow passages and permit complex or multiple-flow circuits while lower operating pressures reduce erosion and provide for sharper spray startup and shutdown.

 

Applications

  • Turbine inlet air cooling (TIAC)
  • Gas conditioning
  • Gas cooling
  • Fire suppression
  • Odor control
  • Wet compression

 

Systems and Accessories

  • Manifolds – standard and custom
  • Nozzle and manifold kitting
  • Filtration
  • Mounting bosses

 

Technical Highlights

  • Maximum operating pressure at ambient temperature: 3000 psi

 

Spider nozzle capacity per leg, U.S. GPH (water)

Capacity

100 psi

200 psi

300 psi

400 psi

500 psi

750 psi

1000 psi

0.5

0.50

0.71

0.87

1.00

1.12

1.37

1.58

1.0

1.0

1.4

1.7

2.0

2.2

2.7

3.2

1.5

1.5

2.1

2.6

3.0

3.4

4.1

4.7

2.0

2.0

2.8

3.5

4.0

4.5

5.4

6.3

2.5

2.5

3.5

4.3

5.0

5.6

6.9

7.9

3.0

3.0

4.2

5.2

6.0

6.7

8.2

9.5

 
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FUEL AND SPRAY NOZZLES

At the forefront of developments in fuel injection technology, the Gas Turbine Fuel Systems Division designs, manufactures, and services fuel injection nozzles, devices, and systems for the aerospace, marine, and power generation markets. Our products produce spray characteristics to maximize specific fuel consumption, increase combustion efficiency and reduce emissions.

 

With more than five decades of experience developing fuel injection systems for commercial, military, and general aviation aircraft engines, we have the proven reliability of billions of service hours.

 

We also have the power of a significant portfolio of patents. For instance, macrolamination is a novel patented technology that enables us to efficiently manufacture complex internal channels, which are essential for active thermal management in fuel injection systems for multi-staged advanced gas turbine systems.

 

In addition to aircraft engine applications, we apply our aerospace experience and fuel injection technology to land and marine applications, as well as large power generation machines, for which we provide a variety of fuel lances and burners.

 

Products

 

Our nozzle types include:

  • Simplex and duplex
  • Dual orifice
  • Airblast and air-assist
  • Hybrid airblast
  • Spill return

We also provide:

  • Fuel control valves
  • Flow divider valves
  • Flow distribution valves
  • Augmentor spraybars
  • Lances and burners

 

Applications

  • Commercial, military, and general aviation aircraft engines -- more fuel nozzles in service on today’s newer and larger engines than any other manufacturer
  • Military ground vehicles
  • Ships and high-speed ferries
  • Offshore oil platforms
  • Mechanical drives
  • Auxilliary power units
  • Electrical power generation
  • Distributed power generation

 

Technical Highlights

  • Fuel nozzles for low emissions engines
  • NOx level 83 percent below 1996 ICAO standard – NASA development
  • Optimized fuel placement and atomization for ignition and relight performance
  • Active thermal management – liquid fuel circuit may be inactive at temperatures of 1100 degrees F
  • Efficient packaging of multi-circuit, multi-fluid nozzles
  • Patented Macrospray® nozzle technology
 
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