JEFFREY MICHAEL HEIN
Pilots at Carver Rd, Tempe, AZ

7210652, May 1, 2007

Dec 8, 2005

11/299116

Jeffrey M. Hein - Tempe AZ, US
Nicholas A. Williams - Phoenix AZ, US
Yogendra Y. Sheoran - Scottsdale AZ, US
Cecilia S. Lam - Scottsdale AZ, US
Ora Morency Cowans - Los Angeles CA, US
Benjamen Kurt Higuera - Oracle AZ, US
Andrew Stephen Peduchi - Tucson AZ, US
Ravisha Pramod Sellahewa - Los Gatos CA, US
Daniel Brown - Surprise AZ, US

Honeywell International, Inc. - Morristown NJ

B64D 33/02

244 53B

An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.

2013021, Aug 22, 2013

Feb 20, 2012

13/400432

Adam Kowal - Phoenix AZ, US
Jeffrey Hein - Tempe AZ, US
David E. Wilcox - Gilbert AZ, US

HONEYWELL INTERNATIONAL INC. - Morristown NJ

G10K 11/00, B32B 37/14, B32B 37/00

181175, 156 60

Monolithic acoustically-treated composite structures and methods for fabricating the same are provided. A monolithic acoustically-treated composite structure comprises an internal frame assembly comprising a unitary composite frame structure and at least one acoustic panel assembly. The unitary composite frame structure defines a shape of the monolithic acoustically-treated composite structure to be fabricated. A composite overlay covers the internal frame assembly. The method for fabricating the monolithic acoustically-treated composite structure comprises forming the unitary composite frame structure, including the at least one acoustic panel in the unitary composite frame structure, and covering the internal frame assembly with the composite overlay.

7014144, Mar 21, 2006

Feb 27, 2004

10/789827

Jeffrey M. Hein - Tempe AZ, US
Nicholas A. Williams - Phoenix AZ, US
Yogendra Y. Sheoran - Scottsdale AZ, US
Cecilia S. Lam - Scottsdale AZ, US
Ora M. Cowans - Los Angeles CA, US
Benjamen K. Higuera - Oracle AZ, US
Andrew S. Peduchi - Tucson AZ, US
Ravisha P. Sellahewa - Los Gatos CA, US
Daniel Brown - Suonse AZ, US

Honeywell International, Inc. - Morristown NJ

B64D 33/02

244 53B

An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.

7448656, Nov 11, 2008

Apr 30, 2007

11/741872

Jeffrey M. Hein - Tempe AZ, US
Nicholas A. Williams - Phoenix AZ, US

Honeywell International Inc. - Morristown NJ

E05C 5/02

292113, 2441294

A dual action structural latch () is provided for securing hinged access doors to a frame. The latch () comprises a latching member () secured to the frame and defining a first aperture (). A hook member () engages the latching member () to resist a tensile force when the latch () is in a closed position, and disengages the latching member () when the latch () is in the open position. A shear pin () extends so as to engage within the first aperture () to resist a shear force when the latch () is in the closed position and to disengage the first aperture () when the latch () is in the open position. A handle (), when moved from the closed position to the open position, sequentially withdraws the shear pin () from the first aperture () and disengages the hook member () from the latching member (), and when moved from the open position to the closed position, sequentially engages the hook member () with the latching member () and inserts the shear pin () in the first aperture ().

7461814, Dec 9, 2008

Dec 8, 2005

11/299147

Jeffrey M. Hein - Tempe AZ, US
Nicholas A. Williams - Phoenix AZ, US
Yogendra Y. Sheoran - Scottsdale AZ, US
Cecilia S. Lam - Scottsdale AZ, US
Ora Morency Cowans - Los Angeles CA, US
Benjamen Kurt Higuera - Oracle AZ, US
Andrew Stephen Peduchi - Tucson AZ, US
Ravisha Pramod Sellahewa - Los Gatos CA, US
Daniel Brown - Surprise AZ, US

Honeywell International Inc. - Morristown NJ

B64D 27/00

244 53B, 244 58

An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.

7600713, Oct 13, 2009

Mar 4, 2005

11/072467

Jeffrey M. Hein - Tempe AZ, US
Nicholas A. Williams - Phoeniz AZ, US

Honeywell International Inc. - Morristown NJ

B64D 33/02

244 53B

A pre-hung air inlet door assembly comprises an inlet door, a door box frame, and an actuation system. The door box frame is fastened to the support structure of an aircraft. The inlet door is operationally connected to the actuation system. The entire pre-hung air inlet door assembly can be pre-assembled for quick installation into an aircraft. Pre-assembly eliminates trimming operations and rigging and misalignment issues. The pivot shafts and bearing housings of the pre-hung air inlet door assembly can be accessed from outside the aircraft when repairs and/or replacement components are needed.

7665694, Feb 23, 2010

Mar 27, 2007

11/691679

Jeffrey M. Hein - Tempe AZ, US
Nicholas A. Williams - Phoenix AZ, US
Yogendra Y. Sheoran - Scottsdale AZ, US
Cecilia S. Lam - Scottsdale AZ, US
Ora Morency Cowans - Los Angeles CA, US
Benjamen Kurt Higuera - Oracle AZ, US
Andrew Stephen Peduchi - Tucson AZ, US
Ravisha Pramod Sellahewa - Los Gatos CA, US
Daniel Brown - Surprise AZ, US

Honeywell International Inc. - Morristown NJ

B64D 33/02, B64C 1/14

2441295, 244 53 B

An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.