Honeywell International, Inc. v. Hamilton Sundstrand Corp.

523 F.3d 1304, 86 U.S.P.Q. 2d (BNA) 1718, 2008 U.S. App. LEXIS 8405, 2008 WL 1757667
CourtCourt of Appeals for the Federal Circuit
DecidedApril 18, 2008
Docket2006-1602
StatusPublished
Cited by25 cases

This text of 523 F.3d 1304 (Honeywell International, Inc. v. Hamilton Sundstrand Corp.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Federal Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Honeywell International, Inc. v. Hamilton Sundstrand Corp., 523 F.3d 1304, 86 U.S.P.Q. 2d (BNA) 1718, 2008 U.S. App. LEXIS 8405, 2008 WL 1757667 (Fed. Cir. 2008).

Opinions

RADER, Circuit Judge.

Honeywell International, Inc. and Honeywell Intellectual Properties, Inc. (collectively “Honeywell”) brought suit against Hamilton Sundstrand Corporation (“Sundstrand”) for infringement of claims 8, 10, 11, 19, and 23 of United States Patent No. 4,380,893 (“the '893 patent”) and claim 4 of Patent No. 4,428,194 (“the '194 patent”). Because “rewriting of de[1307]*1307pendent claims into independent form coupled with the cancellation of the original independent claims creates a presumption of prosecution history estoppel,” this court vacated an earlier infringement verdict in favor of Honeywell and remanded to determine whether Honeywell could rebut the presumption of surrender under Festo Corp. v. Shoketsu Kinzoku Kogyo Kabushiki Co., 535 U.S. 722, 122 S.Ct. 1831, 152 L.Ed.2d 944 (2002) (Festo VIII), remanded to 344 F.3d 1359 (Fed.Cir.2003) (en banc) (Festo IX). Honeywell Int’l Inc. v. Hamilton Sundstrand Corp., 370 F.3d 1131, 1134 (Fed.Cir.2004) (en banc) (Honeywell II). On remand, the United States District Court for the District of Delaware barred Honeywell from asserting the doctrine of equivalents. Honeywell Int’l Inc. v. Hamilton Sundstrand Corp., No. 99-309, 2006 WL 2346446, *1, 2006 U.S. Dist. LEXIS 57030, at *2 (D.Del. Aug. 14, 2006) (Honeywell III)- Because Honeywell did not show that the alleged equivalent was unforeseeable at the time of the narrowing amendment or that the narrowing amendment bore no more than a tangential relation to the alleged equivalent, this court affirms.

I

The patents at issue claim technology to control airflow surge in auxiliary power units or “APUs.” An APU is a gas turbine engine often used in the tail end of aircraft. The APU generates electricity for the aircraft and includes a load compressor to supply compressed air for starting the aircraft’s main engines and for controlling the cabin’s environment during flight. Because APUs face rapidly changing demand levels for compressed air during flight, they must control against “surges.” A surge is an aerodynamic phenomenon, which occurs when airflow through the compressor is too low. In a surge condition, the airflow cannot exit the compressor. Instead, the airflow surges back into the compressor, potentially damaging the APU.

A surge control system maintains a minimum level of airflow through the compressor at all times. Conventional systems provided a wide safety margin by drawing more air than required into the compressor’s main air duct and venting the excess through a surge bleed valve. While effective, these prior art systems were inefficient. Honeywell’s patents claim a more efficient APU surge control system. Honeywell’s invention establishes a “set point” that represents the minimum flow to avoid surges. “Ambient air ... is drawn through a set of adjustable inlet guide vanes (TGV’).... ” '893 Patent col.3 11.64-65. The IGVs open and close like Venetian blinds and regulate the amount of ambient air drawn into the load compressor. The value of the set point is “a function of the position of said [IGVs].” Id. col.12 11.11-12. The invention regulates this set point by comparison to a “flow-related parameter” that measures airflow out of the compressor. Id. col.2 11. 48-54. “Thus a comparison is made between the actual flow conditions (represented by the flow-related parameter) and the desired flow conditions (represented by the set point).” Honeywell II, 370 F.3d at 1134. The invention generates an error signal if the airflow through the compressor is too low. In response to this signal, the inventive APU determines the proper setting of the surge bleed valve to prevent a build up of pressure and maintain sufficient airflow. '194 Patent col.2 11.12-20, 55-60.

The '194 patent issued from a divisional of the application that issued as the '893 patent. During prosecution of the '893 patent, to overcome a rejection under 35 U.S.C. § 121, the applicant separated the system claims from the method claims. The system claims issued in the '893 patent, and the method claims issued in the [1308]*1308'194 patent. The independent claims on appeal are claims 8 and 19 of the '893 patent and claim 4 of the '194 patent. Each of these claims requires the APU to include IGVs, which are used by the surge control system. These independent claims were dependent claims 17, 35 and 51 in the original application that ultimately issued as the '863 patent. The original independent claims (application claims 16, 32 and 48) did not contain any reference to IGVs or any use of the position of these guide vanes in the surge control system. The United States Patent and Trademark Office rejected the original independent claims as obvious in light of the prior art, but allowed the dependent claims when rewritten into independent form. Claims 8 and 19 of the '893 patent state:

8. A gas turbine engine accessory power unit having a fluctuating compressed air supply demand, said accessory power unit comprising:
(a) a compressor having adjustable inlet guide vanes;
(b) duct means for receiving compressed air discharged from said compressor and supplying the received air to the pneumatically-powered apparatus;
(c) surge bleed means operable to exhaust from said duct means a selectively variable quantity of air to assure at least a predetermined minimum flow rate through said duct means and thereby prevent surge of said compressor;
(d) sensing means for sensing the value of a predetermined, flow-related parameter within said duct means and generating an output signal indicative of said value, said value of said flow-related parameter being substantially independent of the temperature of the compressed air;
(e) comparator means for receiving said sensing means output signal and generating an error signal representing the difference between the sensed value of said parameter and a desired value thereof, said comparator means having an adjustable control set point representing said desired value of said parameter;
(f) means for transmitting to said comparator means a reset signal for varying said set point as a function of the position of said inlet guide vanes in accordance with a predetermined reset schedule; and
(g) control means for receiving said error signal and transmitting to said surge bleed means a control signal to operate said surge bleed means, the magnitude of said control signal having, relative to the magnitude of said error signal, a proportional component and an integral component, whereby said minimum flow rate through said duct means is essentially constant regardless of the compressed air supply demand of the pneumatically-powered apparatus.

’893 Patent col.ll 1.52-col.l2 1.23 (emphases added).

19. A control system for assuring a substantially constant minimum flow rate through a duct receiving air discharged from a compressor or the like having adjustable inlet guide vanes,

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523 F.3d 1304, 86 U.S.P.Q. 2d (BNA) 1718, 2008 U.S. App. LEXIS 8405, 2008 WL 1757667, Counsel Stack Legal Research, https://law.counselstack.com/opinion/honeywell-international-inc-v-hamilton-sundstrand-corp-cafc-2008.