Daniel Delpuerto Robles

20170057641, Mar 2, 2017

Jan 8, 2016

14/991155

- MORRIS PLAINS NJ, US
Allen MacKnight - Signal Hill CA, US
Siamak Nikbin - Marina Del Rey CA, US
Myron Quan - Cerritos CA, US
Daniel R. Robles - Norwalk CA, US

HONEYWELL INTERNATIONAL INC. - MORRIS PLAINS NJ

B64D 13/06
B64D 37/34

A cooling system in which an ACS (air cycle system) turbine may be driven by high pressure air from a turbo-fan engine and a VCS (vapor cycle system) having an evaporator and a VCS refrigerant compressor may be driven by the ACS turbine. Fluid of the chilled fluid reservoir, which may be chilled fuel, may be circulated through and cooled in the evaporator. In some embodiments, the ACS turbine may be coupled to the VCS refrigerant compressor by a magnetic coupling.

20150090114, Apr 2, 2015

Oct 1, 2013

14/042926

- Morristown NJ, US
Hal J. Strumpf - Rancho Palos Verdes CA, US
Dennis M. Morita - Rancho Palos Verdes CA, US
Daniel R. Robles - Long Beach CA, US

HONEYWELL INTERNATIONAL INC. - Morristown NJ

B03C 3/34

95 8, 96 18, 96 19

An Environmental Control System may use an electronic particle separation system to control humidity in an aircraft. The electronic particle separation system may include a particle separator, a sensor module, and a controller configured to receive signals from the sensor module, and operate the particle separator based on the received sensor signals. In some embodiments, the controller may include a processor which may determine whether the particle separator is being operated under an ozone related condition exceeding a threshold operating condition. If one of the threshold operating conditions is exceeded, the particle separator may be turned off which may control the amount of ozone present in the aircraft.

20150090120, Apr 2, 2015

Oct 1, 2013

14/042883

- Morristown NJ, US
Dennis M. Morita - Rancho Palos Verdes CA, US
Daniel R. Robles - Long Beach CA, US
Hal J. Strumpf - Rancho Palos Verdes CA, US

HONEYWELL INTERNATIONAL INC. - Morristown NJ

B03C 3/017
B01D 45/12

95 70, 96 55

An Environmental Control System may use an electronic particle separation system to control humidity in an aircraft. The electronic particle separation system may include a charging stage and a collecting stage. The charging stage may charge airflow passing through to repel liquid particles away from the airflow. Liquid droplets may be collected by the collecting stage and centrifugally flung toward a periphery of a separator. The liquid particles may be collected outside of the airflow which may be allowed to pass through the separator and out to a destination in the aircraft without the collected liquid.