Patent application number | Description | Published |
20090188423 | Securing device - A securing device for securing a flag having a grommet to a cord is provided. Such securing device includes a support member manufactured from a predetermined material and having a first predetermined shape and a first predetermined size. Such support member further having at least one aperture disposed therethrough at a predetermined location. Such aperture has a second predetermined size and is capable of being threaded with a cord for securing such cord to such support member, such cord has a third predetermined size. A securing mechanism is operably connectable to such support member for securing such flag to such support member. | 07-30-2009 |
20100319605 | Securing device - A flag securing assembly includes elongate member formed with an opening, opposed notched ends, and a lug projecting away from the elongate member and which terminates with a free end. A major loop of a line is applied through the opening and is folded over the elongate member forming in the line opposite minor loops applied to the opposed notched ends, a length of the line extending between the minor loops along the elongate member, and standing parts that project outward in opposite directions from the opposed notched ends. A grommet of a flag is applied to the lug between the free end of the lug and the elongate member, and a fastener is applied to the free end of the lug captively retaining the grommet of the flag between the free end of the lug and the elongate member. | 12-23-2010 |
20130055531 | SECURING DEVICE - A flag securing assembly includes elongate member formed with an opening, opposed notched ends, and a lug projecting away from the elongate member and which terminates with a free end. A major loop of a line is applied through the opening and is folded over the elongate member forming in the line opposite minor loops applied to the opposed notched ends, a length of the line extending between the minor loops along the elongate member, and standing parts that project outward in opposite directions from the opposed notched ends. A grommet of a flag is applied to the lug between the free end of the lug and the elongate member, and a fastener is applied to the free end of the lug captively retaining the grommet of the flag between the free end of the lug and the elongate member. | 03-07-2013 |
Patent application number | Description | Published |
20130319002 | NACELLE BIFURCATION FOR GAS TURBINE ENGINE - A nacelle structure for a gas turbine engine includes a core engine nacelle disposed about an engine axis and an outer nacelle disposed about the core engine nacelle. A bifurcation extends between the outer nacelle and the core engine nacelle along a bifurcation axis extending between the outer nacelle and the core engine nacelle. The bifurcation includes at least one mounting surface that is disposed at a non-normal angle relative to the bifurcation axis. | 12-05-2013 |
20140216005 | Gas Turbine Engine Assembly Including A Thrust Reverser - An exemplary gas turbine engine assembly includes a thrust reverser that is selectively moveable between a stowed position and a thrust reversing position. The thrust reverser includes an outer surface having a first outer surface area when the thrust reverser is in the stowed position and a second, smaller outer surface area when the thrust reverser is in the thrust reversing position. | 08-07-2014 |
20140237990 | VARIABLE AREA FAN NOZZLE WITH WALL THICKNESS DISTRIBUTION - A gas turbine engine includes a core engine that has at least a compressor section, a combustor section and a turbine section disposed along a central axis. A fan is coupled to be driven by the turbine section. A fan nacelle is arranged around the fan, and a bypass passage extends between the fan nacelle and the core engine. A variable area fan nozzle (VAFN) extends at least partially around the central axis and defines an exit area of the bypass passage. The VAFN is selectively movable to vary the exit area. The VAFN includes a body that defines an airfoil cross-section shape. The VAFN includes a wall that has a mechanical property distribution in accordance with a computer-simulated vibration profile of a flutter characteristic of the VAFN. | 08-28-2014 |
20140259661 | VARIABLE AREA FAN NOZZLE WITH WALL THICKNESS DISTRIBUTION - A method of controlling flutter of a fan nozzle includes, for a given design of a fan nozzle, determining a vibration mode that causes a flutter characteristic of the fan nozzle and, in response to the determined vibration mode, establishing a wall thickness distribution of at least one wall of the fan nozzle to include local thick portions and local thin portions that alter the flutter characteristic. | 09-18-2014 |
Patent application number | Description | Published |
20130055253 | CLOUD-BASED BUILD SERVICE - Building binary packages for software products, particularly large-scale software products, is a highly computation intensive process. Thus, it is desirable to distribute the workload over a large number of computing nodes so as to have the build process complete in an optimal period of time. One environment providing compute resources that can be utilized for a highly available and dynamically scalable distributed build process is an elastic compute cloud. In such an environment, virtual machines can be instantiated and destroyed as the resource requirements of the build process dictate. This has the advantage that dedicated hardware is unneeded, and excess capacity on the hardware employed can be employed for other computation tasks when the build process is idle. Presented herein are systems, methods and computer storage media for distributing a highly available and scalable build service, suitable for use in an elastic compute environment or other distributed environment. | 02-28-2013 |
20140137116 | CLOUD-BASED BUILD SERVICE - Building binary packages for software products, particularly large-scale software products, is a highly computation intensive process. Thus, it is desirable to distribute the workload over a large number of computing nodes so as to have the build process complete in an optimal period of time. One environment providing compute resources that can be utilized for a highly available and dynamically scalable distributed build process is an elastic compute cloud. In such an environment, virtual machines can be instantiated and destroyed as the resource requirements of the build process dictate. This has the advantage that dedicated hardware is unneeded, and excess capacity on the hardware employed can be employed for other computation tasks when the build process is idle. Presented herein are systems, methods and computer storage media for distributing a highly available and scalable build service, suitable for use in an elastic compute environment or other distributed environment. | 05-15-2014 |
20140282421 | DISTRIBUTED SOFTWARE VALIDATION - A computer-implemented method for validation of a software product via a distributed computing infrastructure includes receiving configuration data for a plurality of validation tasks of the validation, receiving code data representative of the software product, defining a validation pipeline to implement the plurality of validation tasks based on the configuration data, and initiating execution of the plurality of validation tasks on a plurality of virtual machines of the distributed computing infrastructure. Initiating the execution includes sending the code data and data indicative of the defined validation pipeline to configure each virtual machine in accordance with the code data and the defined validation pipeline. | 09-18-2014 |
20140282450 | SOFTWARE BUILD OPTIMIZATION - A method for optimization of a software build includes collecting first data representative of inputs for a build process obtained by a set of data accessing operations implemented during a first execution of the build process, the set including a file accessing operation and a non-file accessing operation. A redirection routine embedded within the build process captures the inputs. The first data is compared with second data representative of the inputs obtained in connection with a second execution of the build process. If the first and second data do not match, the second data is recorded in a data store and output data generated by the second execution of the build process is stored. If the first and second data match, output data generated by the first execution of the build process is used as an output for the second execution of the build process. | 09-18-2014 |